{"meta":{"page":1,"per_page":50,"max_per_page":100,"total":267,"total_is_capped":false,"direct_labels_cover":1,"predictions_cover":267,"direct_label_status":"direct model label, unvalidated","prediction_status":"machine_predicted_unvalidated (Codex and Gemma teacher distillation)","score_status":"score_only:v0-immature-baseline (scores rank; they never assert a category)","snapshot":{"source":"OpenAlex, pinned release, all 482 partitions","release":"2026-06-24","frame_built":"2026-07-12","author_layer_release":"2026-06-26"},"query_hash":"179b19826f74","filters":{"topic":"Spacecraft Dynamics and Control"}},"results":[{"id":"W2034217323","doi":"10.1016/j.ast.2014.12.031","title":"Tracking control of spacecraft formation flying with collision avoidance","year":2015,"lang":"en","type":"article","venue":"Aerospace Science and Technology","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":133,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Concordia University","funders":"Specialized Research Fund for the Doctoral Program of Higher Education of China; Program for New Century Excellent Talents in University; National Natural Science Foundation of China; Heilongjiang Youth Development Foundation","keywords":"Collision avoidance; Spacecraft; Control theory (sociology); Obstacle avoidance; Lyapunov function; Parametric statistics; Tracking (education); Obstacle; Computer science; Nonlinear system; Control engineering; Control (management); Collision; Engineering; Aerospace engineering; Mathematics; Artificial intelligence; Mobile robot; Physics; Robot","authors":[{"name":"Qinglei Hu","is_ca":false},{"name":"Hongyang Dong","is_ca":false},{"name":"Youmin Zhang","is_ca":true},{"name":"Guangfu Ma","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.00621323682029414,"gpt":0.1937701431819612,"spread":0.1875569063616671,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002446166,0.0003056955,0.0002974308,0.0002309907,0.0004752784,0.0005531578,0.0004630031,0.000290547,0.001317322],"category_scores_gemma":[0.0005982381,0.0001505516,0.0001961273,0.000292301,0.0003912279,0.0002767575,0.0006306153,0.0003253022,0.0001627049],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0003363318,"about_ca_system_score_gemma":0.000593464,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.007841334,"about_ca_topic_score_gemma":0.004574438,"domain_scores_codex":[0.9999021,0.00001949789,0.000003241842,0.00001994353,0.00003601058,0.00001925657],"domain_scores_gemma":[0.999887,0.00003417291,0.00002665753,0.00000913395,0.00003289632,0.00001004246],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.0001909806,0.00004924121,0.0005749291,0.00007100886,0.00003738152,0.0000794899,0.0001665336,0.8962744,0.009559657,0.0235357,0.0009577625,0.06850288],"study_design_scores_gemma":[0.00001834385,0.00008002094,0.0002938744,0.000003672274,0.000006433448,0.00001328323,0.00001201869,0.9951563,0.0008682725,0.00288079,0.0006624713,0.000004527359],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.1334592,0.000406265,0.8518435,0.0002104381,0.0001480295,0.00005223279,0.00004033424,0.0002056773,0.01363436],"genre_scores_gemma":[0.9871451,0.0000969554,0.009846158,0.00002164721,0.00002034123,0.00002686455,0.00001767276,0.000008119874,0.002817144],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.007841334,"threshold_uncertainty_score":0.01559144,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2070003902","doi":"10.1142/s0218127407018671","title":"ELEMENTAL PERIODIC ORBITS ASSOCIATED WITH THE LIBRATION POINTS IN THE CIRCULAR RESTRICTED 3-BODY PROBLEM","year":2007,"lang":"en","type":"article","venue":"International Journal of Bifurcation and Chaos","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":131,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Concordia University","funders":"National Science Foundation","keywords":"Continuation; Bifurcation; Periodic orbits; Three-body problem; Mathematics; Lagrangian point; Numerical continuation; Boundary (topology); Libration (molecule); Numerical analysis; Mathematical analysis; Boundary value problem; Geometry; Computer science; Classical mechanics; Point (geometry); Physics; Nonlinear system","authors":[{"name":"Eusebius J. Doedel","is_ca":true},{"name":"Volodymyr A. Romanov","is_ca":true},{"name":"Randy Paffenroth","is_ca":false},{"name":"Herbert B. Keller","is_ca":false},{"name":"Donald J. Dichmann","is_ca":false},{"name":"J. Galán","is_ca":false},{"name":"André Vanderbauwhede","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.003823604189728892,"gpt":0.2036360954253354,"spread":0.1998124912356065,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002416974,0.0003083822,0.0004902689,0.0005159867,0.0008434308,0.0006603933,0.0004780181,0.0008333804,0.005935853],"category_scores_gemma":[0.00122547,0.0002120665,0.0006198301,0.0004089429,0.0007173175,0.0006640916,0.0007916141,0.0004339547,0.0005146541],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0002524584,"about_ca_system_score_gemma":0.000397925,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.002075205,"about_ca_topic_score_gemma":0.001668002,"domain_scores_codex":[0.9999344,0.00001577034,0.000004277803,0.00001043896,0.00002104667,0.00001399404],"domain_scores_gemma":[0.9997359,0.000144708,0.00004487374,0.00002942479,0.00002412449,0.00002101644],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.00008688202,0.00002681066,0.002928852,0.0001561949,0.00002581279,0.0003593523,0.0001999355,0.883576,0.001882649,0.09557655,0.001152816,0.01402812],"study_design_scores_gemma":[0.0000194739,0.00002095338,0.0008170294,0.00003009631,0.000009341034,0.0001482021,0.0001235995,0.9572511,0.0009427675,0.03890622,0.001717458,0.00001372546],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.656635,0.0008013519,0.3029078,0.0004054562,0.00005792318,0.00009414772,0.0005870333,0.0001949851,0.03831621],"genre_scores_gemma":[0.9129937,0.0004702384,0.08055269,0.00006226609,0.00002805375,0.0001507165,0.000564435,0.0001305004,0.005047488],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.005935853,"threshold_uncertainty_score":0.01985741,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2029050532","doi":"10.1088/0067-0049/199/1/9","title":"A RADIATION TRANSFER SOLVER FOR ATHENA USING SHORT CHARACTERISTICS","year":2012,"lang":"en","type":"article","venue":"The Astrophysical Journal Supplement Series","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":118,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Canadian Institute for Theoretical Astrophysics","funders":"","keywords":"Solver; Radiative transfer; Magnetohydrodynamics; Tensor (intrinsic definition); Scattering; Integrator; Operator (biology); Code (set theory)","authors":[],"retraction":null,"screen_n_in":null,"score":{"opus":0.01078493738657875,"gpt":0.2242283090598661,"spread":0.2134433716732873,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004517574,0.0007032373,0.0005712773,0.0005678415,0.0006544509,0.0009756418,0.001679387,0.0008575999,0.01559446],"category_scores_gemma":[0.001571162,0.0004637188,0.0009666235,0.0006151625,0.0004164151,0.001195194,0.001873074,0.001209124,0.004688231],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0007009733,"about_ca_system_score_gemma":0.001604279,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.002882235,"about_ca_topic_score_gemma":0.002327673,"domain_scores_codex":[0.9996333,0.00005978892,0.00003419877,0.00005460082,0.000173946,0.00004412079],"domain_scores_gemma":[0.9995717,0.0001265719,0.00004485478,0.00007903779,0.0001396565,0.00003822437],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.0003389828,0.0001784618,0.004121008,0.0007348772,0.0001995145,0.00066298,0.0005927224,0.4547789,0.05395972,0.2010864,0.07169345,0.2116531],"study_design_scores_gemma":[0.0001247304,0.00006721193,0.0007329552,0.00005265076,0.00002408753,0.0003209666,0.0000552593,0.7902483,0.01308355,0.03136356,0.1638781,0.00004855595],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.02256364,0.0003480317,0.9149575,0.0003663882,0.0002853656,0.0002200473,0.002195701,0.0136967,0.04536663],"genre_scores_gemma":[0.1634815,0.0003572509,0.7924088,0.0004348093,0.0001416504,0.001246265,0.005764129,0.005823652,0.0303419],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.01559446,"threshold_uncertainty_score":0.05216867,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2066850947","doi":"10.2514/1.38580","title":"Fault Tolerant Reconfigurable Satellite Formations Using Adaptive Variable Structure Techniques","year":2010,"lang":"en","type":"article","venue":"Journal of Guidance Control and Dynamics","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":102,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Control theory (sociology); Spacecraft; Control reconfiguration; Fault tolerance; Robustness (evolution); Nonlinear system; Sliding mode control; Computer science; Reaction wheel; Engineering; Aerospace engineering; Control (management); Physics","authors":[{"name":"Godard","is_ca":true},{"name":"Krishna Dev Kumar","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.003795491317063494,"gpt":0.196793574314044,"spread":0.1929980829969805,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001698426,0.0002944595,0.0002339682,0.000189604,0.0001963947,0.0002499011,0.000498691,0.0002727599,0.000373039],"category_scores_gemma":[0.0004042508,0.0001293503,0.0002743558,0.0001063537,0.0003218515,0.0002719409,0.0003489293,0.0003276683,0.00006913858],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0002448904,"about_ca_system_score_gemma":0.0002422449,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.001565988,"about_ca_topic_score_gemma":0.001266849,"domain_scores_codex":[0.9999139,0.00001610232,0.000004059882,0.00002207974,0.00003201569,0.00001177267],"domain_scores_gemma":[0.9998589,0.0000393819,0.00004642596,0.00002325414,0.00002253858,0.000009504569],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.00007987393,0.00004155543,0.0006760404,0.00005704697,0.00003520812,0.0001159681,0.0001975906,0.8003858,0.03612982,0.01119395,0.0003637964,0.1507234],"study_design_scores_gemma":[0.00001843608,0.000116476,0.0001905815,0.000004041851,0.000006961356,0.00003841873,0.00001097481,0.994048,0.003292635,0.001334273,0.0009332094,0.000005977526],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.06493308,0.0002220119,0.9328935,0.00006746849,0.00003941163,0.00001824193,0.000005790298,0.0002622954,0.001558172],"genre_scores_gemma":[0.8960744,0.0001272278,0.1024831,0.00003096602,0.00002248889,0.00004048973,0.00001510182,0.00001204277,0.001194123],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.001565988,"threshold_uncertainty_score":0.003113747,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2047828854","doi":"10.2514/1.56387","title":"Particle Swarm Optimization Applied to Spacecraft Reentry Trajectory","year":2012,"lang":"en","type":"article","venue":"Journal of Guidance Control and Dynamics","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":88,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Aerospace; Trajectory optimization; Computer science; Missile guidance; Aeronautics; Operations research; Aerospace engineering; Engineering; Optimal control; Mathematics; Mathematical optimization","authors":[{"name":"Afshin Rahimi","is_ca":true},{"name":"Krishna Dev Kumar","is_ca":true},{"name":"Hekmat Alighanbari","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.003518474042284823,"gpt":0.1873773403057785,"spread":0.1838588662634937,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007180414,0.0006408478,0.0009954714,0.0005765453,0.0005986591,0.0006853081,0.000522883,0.0008651731,0.001294426],"category_scores_gemma":[0.002361132,0.0005252996,0.0005388599,0.0007093266,0.0004689088,0.0005494362,0.0005689727,0.0008597669,0.000223329],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0007174453,"about_ca_system_score_gemma":0.001054721,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.0255258,"about_ca_topic_score_gemma":0.0103115,"domain_scores_codex":[0.9998389,0.0000742811,0.000009356876,0.00002238789,0.00004019875,0.00001479606],"domain_scores_gemma":[0.9996147,0.0002065559,0.00002747349,0.00002832695,0.0001026034,0.00002025726],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.00002805273,0.00001367891,0.0001968991,0.00001985289,0.0000166803,0.00002090747,0.00002857173,0.9807237,0.0005002863,0.003295779,0.0004080333,0.0147477],"study_design_scores_gemma":[0.000001550419,0.00000288651,0.00003264617,7.611367e-7,0.00000101762,8.846855e-7,0.000001344087,0.9995161,0.00004730217,0.0003213343,0.00007342972,7.067616e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.03071874,0.0003873887,0.9645022,0.000225754,0.0002100485,0.00005289431,0.00002853905,0.0002521421,0.00362233],"genre_scores_gemma":[0.7531952,0.0006699775,0.2385253,0.00006392381,0.0001403198,0.0001651041,0.0001058076,0.0001799748,0.006954343],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.0255258,"threshold_uncertainty_score":0.05075449,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2190128130","doi":"10.1007/s11071-015-2479-1","title":"Robust adaptive terminal sliding mode control on SE(3) for autonomous spacecraft rendezvous and docking","year":2015,"lang":"en","type":"article","venue":"Nonlinear Dynamics","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":86,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"York University","funders":"","keywords":"Control theory (sociology); Spacecraft; Rendezvous; Terminal sliding mode; Lyapunov function; Sliding mode control; Robustness (evolution); Lyapunov stability; Robust control; Mathematics; Computer science; Engineering; Physics; Control system; Artificial intelligence; Aerospace engineering","authors":[{"name":"Daero Lee","is_ca":true},{"name":"George Vukovich","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.02863938010311932,"gpt":0.2434321827838287,"spread":0.2147928026807094,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002473965,0.0005141263,0.0004423918,0.0002129048,0.0003119471,0.000505685,0.0005151478,0.0005428329,0.00193857],"category_scores_gemma":[0.0005267885,0.0001395663,0.000435944,0.0002009507,0.0004468262,0.0003663146,0.0008781826,0.0004681002,0.0001896925],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0002344244,"about_ca_system_score_gemma":0.0003299765,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.004035329,"about_ca_topic_score_gemma":0.002618477,"domain_scores_codex":[0.9999083,0.0000202057,0.000004997172,0.00002518989,0.00002316626,0.00001809563],"domain_scores_gemma":[0.9998865,0.00003287858,0.00002299153,0.00001239723,0.00003640441,0.00000880535],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.0003902266,0.00005944099,0.0007204247,0.0001151229,0.00005610093,0.0002092012,0.0001903073,0.9022843,0.02307794,0.01640201,0.001293081,0.05520181],"study_design_scores_gemma":[0.000009510141,0.00008616968,0.000168386,0.000003062474,0.000004313051,0.000007841989,0.000009441083,0.9974947,0.0007489086,0.001240978,0.0002230159,0.00000372614],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.1414785,0.0001738106,0.8517057,0.0001000572,0.0001024459,0.00003194444,0.000036396,0.0002586682,0.006112426],"genre_scores_gemma":[0.9904383,0.00004975839,0.006957278,0.00001878832,0.000008955933,0.00002817063,0.00002886008,0.00001064913,0.002459293],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.004035329,"threshold_uncertainty_score":0.008023679,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W3093458920","doi":"10.1016/j.actaastro.2020.10.016","title":"Adaptive extended Kalman filtering strategies for spacecraft formation relative navigation","year":2020,"lang":"en","type":"article","venue":"Acta Astronautica","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":84,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"Carleton University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Control theory (sociology); Kalman filter; Spacecraft; Invariant extended Kalman filter; Extended Kalman filter; Fast Kalman filter; Orbit determination; Adaptive filter; Computer science; Alpha beta filter; Kernel adaptive filter; Filter (signal processing); Initialization; Smoothing; Algorithm; Filter design; Engineering; Artificial intelligence; Computer vision; Aerospace engineering; Global Positioning System","authors":[{"name":"Cory T. Fraser","is_ca":true},{"name":"Steve Ulrich","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.01459880787303913,"gpt":0.2201210418295319,"spread":0.2055222339564928,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000542807,0.0006079566,0.0007428161,0.0003459464,0.0003915279,0.0006339871,0.0009049821,0.0006924209,0.001903772],"category_scores_gemma":[0.002215944,0.0003850822,0.0004553478,0.0005448317,0.0004649861,0.001027191,0.001047381,0.0009529918,0.0004817289],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0003674428,"about_ca_system_score_gemma":0.0006438592,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.007742499,"about_ca_topic_score_gemma":0.005726968,"domain_scores_codex":[0.9997042,0.00008646405,0.00001950579,0.00005955114,0.00009934617,0.00003089555],"domain_scores_gemma":[0.9995716,0.0001957585,0.00005775968,0.00003922315,0.0001224499,0.0000131626],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.0001651156,0.0000566493,0.0003895802,0.0001541203,0.0000907305,0.00006697005,0.0002398199,0.7483659,0.007096766,0.02881141,0.00236365,0.2121994],"study_design_scores_gemma":[0.00001349485,0.00005688223,0.0001718316,0.000008693474,0.00001164561,0.00001234682,0.00001303187,0.9926392,0.0006590534,0.005215485,0.001188626,0.000009752835],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"methods","genre_scores_codex":[0.007784961,0.0004503564,0.9901779,0.0000720031,0.00008030496,0.00001109076,0.00002126196,0.0001149547,0.001287185],"genre_scores_gemma":[0.8070754,0.001113093,0.1780413,0.0001388888,0.0001955759,0.0001477214,0.0002231094,0.00009347517,0.01297146],"genre_candidate":"methods","genre_consensus":"methods","teacher_disagreement_score":0.007742499,"threshold_uncertainty_score":0.01539487,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2081155235","doi":"10.2514/1.52395","title":"Multiple Satellite Formation Flying Using Differential Aerodynamic Drag","year":2012,"lang":"en","type":"article","venue":"Journal of Spacecraft and Rockets","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":67,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"Toronto Metropolitan University","funders":"Canada Research Chairs","keywords":"Aerospace engineering; Spacecraft; Aerodynamics; Spacecraft design; Satellite; Missile; Space vehicle; Drag; Space (punctuation); Differential (mechanical device); Space technology; Aerodynamic drag; Aeronautics; Computer science; Systems engineering; Engineering","authors":[{"name":"Surjit Varma","is_ca":true},{"name":"Krishna Dev Kumar","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.009405502939031122,"gpt":0.2031544133834264,"spread":0.1937489104443952,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001450683,0.0004759814,0.0005309443,0.0003406092,0.0004762702,0.000408899,0.0004071636,0.0002792325,0.002383579],"category_scores_gemma":[0.000338542,0.0001988224,0.0004635109,0.0003236808,0.0002775339,0.0004703054,0.0006705783,0.0004708731,0.0003486167],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0004594011,"about_ca_system_score_gemma":0.0004298238,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.003782716,"about_ca_topic_score_gemma":0.005803008,"domain_scores_codex":[0.9998931,0.00001419998,0.00000335475,0.00002086158,0.00005345797,0.00001516573],"domain_scores_gemma":[0.9998943,0.00003399899,0.0000111666,0.00002062503,0.00002537292,0.00001454298],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.00006512456,0.0000453285,0.001761909,0.00008456204,0.00006502576,0.0001510401,0.00006530953,0.848269,0.01329642,0.03135994,0.003178604,0.1016577],"study_design_scores_gemma":[0.000003500355,0.00002819513,0.0003487048,0.000005968159,0.000005907224,0.00004666144,0.000006679516,0.9949155,0.0007552491,0.001963882,0.001913388,0.000006392095],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.05084397,0.00139303,0.9216902,0.0002228745,0.00058282,0.00004759681,0.0001073074,0.0004372678,0.02467485],"genre_scores_gemma":[0.8503945,0.001442243,0.1252041,0.00008423132,0.0002745389,0.00006149708,0.0002349188,0.0001694857,0.02213449],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.003782716,"threshold_uncertainty_score":0.007973909,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2158869043","doi":"10.2514/1.29438","title":"Linearized Dynamics of Formation Flying Spacecraft on a J2-Perturbed Elliptical Orbit","year":2007,"lang":"en","type":"article","venue":"Journal of Guidance Control and Dynamics","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":67,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Spacecraft; Elliptic orbit; Orbit (dynamics); Physics; Aerospace engineering; Orbital mechanics; Orbit determination; Classical mechanics; Control theory (sociology); Computer science; Astronomy; Satellite; Engineering","authors":[{"name":"Jean‐François Hamel","is_ca":true},{"name":"Jean de Lafontaine","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.004221957918848681,"gpt":0.2074031629968061,"spread":0.2031812050779574,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000143579,0.0004223144,0.0004231276,0.0002156391,0.0003471602,0.0006560186,0.0004781183,0.0005642021,0.001711614],"category_scores_gemma":[0.0003910366,0.0002456963,0.0003855121,0.0002045264,0.0005544802,0.000591383,0.0006917689,0.0005859067,0.0003319112],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0004781421,"about_ca_system_score_gemma":0.0005234224,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.0135332,"about_ca_topic_score_gemma":0.005477454,"domain_scores_codex":[0.9999177,0.00001810538,0.000002837955,0.00001436375,0.00003678807,0.00001012927],"domain_scores_gemma":[0.9999039,0.00002248761,0.00003060874,0.000008504767,0.00002396763,0.00001050576],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.00002852457,0.00001162442,0.0007365387,0.00002460783,0.00001452231,0.0001098627,0.0001134779,0.9752544,0.003792667,0.01599153,0.0004821047,0.00344011],"study_design_scores_gemma":[0.000005270883,0.00002344124,0.0002904616,0.000002363407,0.000003945673,0.00002639901,0.00001998211,0.9973295,0.0003744327,0.001472118,0.000444959,0.000007093566],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.3090157,0.0003515284,0.6541594,0.0006352704,0.00006782256,0.0000752035,0.0005044712,0.0005808985,0.03460975],"genre_scores_gemma":[0.9768992,0.0002180664,0.01056135,0.0000694959,0.00001604285,0.0000520018,0.0002442577,0.00003984729,0.01189978],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.0135332,"threshold_uncertainty_score":0.02690887,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2110610429","doi":"10.2514/1.62154","title":"Optimal Control of Nanosatellite Fast Deorbit Using Electrodynamic Tether","year":2014,"lang":"en","type":"article","venue":"Journal of Guidance Control and Dynamics","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":57,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"York University","funders":"","keywords":"Control theory (sociology); Optimal control; Discretization; Trajectory; Piecewise; Trajectory optimization; Orbit (dynamics); Collocation (remote sensing); Physics; Computer science; Mathematics; Mathematical optimization; Control (management); Engineering; Aerospace engineering; Mathematical analysis","authors":[{"name":"Rui Zhong","is_ca":true},{"name":"Zheng Zhu","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.002502561285818197,"gpt":0.1866223596817416,"spread":0.1841197983959234,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001907286,0.0003448542,0.0003840603,0.0001621184,0.0002559657,0.0004062814,0.0003945512,0.0003360148,0.0008584064],"category_scores_gemma":[0.000282012,0.0001956432,0.0001965464,0.0001216032,0.0004452437,0.000330909,0.0006486189,0.000349681,0.00008104296],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0003007823,"about_ca_system_score_gemma":0.0004063741,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.001990296,"about_ca_topic_score_gemma":0.001447683,"domain_scores_codex":[0.999935,0.00001344775,0.00000304222,0.00001354914,0.0000240333,0.00001082701],"domain_scores_gemma":[0.9999083,0.00003104148,0.00002514846,0.000009211317,0.00001648209,0.000009804479],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.0001047758,0.00001931783,0.0002861481,0.00004275812,0.000009922867,0.00005288793,0.00005977,0.9558228,0.01298706,0.01011625,0.000313239,0.02018514],"study_design_scores_gemma":[0.000006946725,0.00003151282,0.0000699676,0.000001839237,0.000001487858,0.000005436404,0.000007362908,0.9981116,0.0007351997,0.0006236784,0.0004023492,0.000002642149],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.09472954,0.0002001559,0.8993018,0.0001354851,0.00005237776,0.00002490654,0.00002021505,0.0001290016,0.005406542],"genre_scores_gemma":[0.9641023,0.0001277284,0.03317634,0.00002582315,0.0000125986,0.00004383835,0.00002097326,0.00001814472,0.002472216],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.001990296,"threshold_uncertainty_score":0.00395745,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2150615212","doi":"10.1090/s0002-9947-2010-05251-1","title":"On the singularities of the curved 𝑛-body problem","year":2010,"lang":"en","type":"article","venue":"Transactions of the American Mathematical Society","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":54,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Pacific Institute for the Mathematical Sciences; University of Victoria","funders":"","keywords":"Mathematics; Mathematical proof; Gravitational singularity; Curvature; Property (philosophy); Projection (relational algebra); Constant (computer programming); Constant curvature; Pure mathematics; Mathematical analysis; Geometry; Algorithm","authors":[{"name":"Florin Diacu","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.004140655321624442,"gpt":0.1945167135666369,"spread":0.1903760582450124,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00118441,0.0008194998,0.0007996663,0.001218716,0.001671419,0.001448686,0.001308852,0.001923269,0.005971009],"category_scores_gemma":[0.006873269,0.0003431577,0.0008733498,0.0005413835,0.003368365,0.002809696,0.003519068,0.002198093,0.0007756135],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.001001605,"about_ca_system_score_gemma":0.0007948939,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.001996574,"about_ca_topic_score_gemma":0.0007909348,"domain_scores_codex":[0.9995211,0.0001608508,0.00001884025,0.0000664339,0.0001340515,0.00009868498],"domain_scores_gemma":[0.9988831,0.0004605877,0.0001732829,0.0001015353,0.0001869506,0.000194621],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"theoretical_or_conceptual","study_design_scores_codex":[0.00003516061,0.00001969589,0.0004132928,0.00007161628,0.00001127024,0.0003110956,0.0002809035,0.01165669,0.0006508451,0.9803764,0.00242361,0.003749417],"study_design_scores_gemma":[0.00003741988,0.00004788861,0.0004082015,0.00005537688,0.000009749548,0.0002287457,0.0002783021,0.09257362,0.0003876073,0.902052,0.003897579,0.00002356547],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":"theoretical_or_conceptual","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.421547,0.003105959,0.4153178,0.009490638,0.0007302154,0.0001625102,0.0002383585,0.0003484542,0.149059],"genre_scores_gemma":[0.9421438,0.001078314,0.0284474,0.0006222686,0.0002953408,0.00009694148,0.0001946979,0.0001592931,0.02696189],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.005971009,"threshold_uncertainty_score":0.01997501,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W3155137447","doi":"10.1016/j.ast.2021.106739","title":"Adaptive saturated control for spacecraft rendezvous and docking under motion constraints","year":2021,"lang":"en","type":"article","venue":"Aerospace Science and Technology","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":54,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":false,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"","funders":"China Scholarship Council; University of Toronto","keywords":"Rendezvous; Spacecraft; Control theory (sociology); Aerospace engineering; Docking (animal); Adaptive control; Motion control; Computer science; Control engineering; Control (management); Engineering; Artificial intelligence; Robot","authors":[{"name":"Xiangtian Zhao","is_ca":false},{"name":"Shijie Zhang","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.005397587027568872,"gpt":0.2024097780405234,"spread":0.1970121910129546,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002057785,0.0005393701,0.0005180089,0.0003211884,0.0004527505,0.0006724717,0.0005695897,0.0004589173,0.002567333],"category_scores_gemma":[0.001115659,0.0002392341,0.000203853,0.0004152564,0.0007230685,0.000658052,0.00140127,0.0005000169,0.0002036709],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0004863036,"about_ca_system_score_gemma":0.0006271199,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.01055545,"about_ca_topic_score_gemma":0.007748733,"domain_scores_codex":[0.9998435,0.00003402938,0.000006910936,0.00003431328,0.00003858159,0.00004258311],"domain_scores_gemma":[0.9996878,0.0001364484,0.00003485047,0.00001782524,0.0001053533,0.00001785736],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.0004396286,0.00008473783,0.0005807332,0.0002455309,0.00006267446,0.0001443015,0.000258573,0.8847246,0.01849622,0.03121353,0.002102346,0.06164714],"study_design_scores_gemma":[0.00001237308,0.00005391108,0.0002013983,0.000004562201,0.000004393983,0.000009985006,0.00002098388,0.9939068,0.0007251739,0.004709304,0.0003460888,0.000005078138],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.1277296,0.0003526503,0.856728,0.0002859962,0.0001370245,0.00004641435,0.00008949979,0.0003715675,0.0142593],"genre_scores_gemma":[0.9931794,0.00006179506,0.003043582,0.00003825368,0.00001487301,0.00002652556,0.00002952724,0.00001282942,0.003593234],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.01055545,"threshold_uncertainty_score":0.02098799,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2051436583","doi":"10.1007/s10509-012-1085-7","title":"On the restricted three body problem with oblate primaries","year":2012,"lang":"en","type":"article","venue":"Astrophysics and Space Science","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":52,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"Wilfrid Laurier University","funders":"Natural Sciences and Engineering Research Council of Canada; Wilfrid Laurier University","keywords":"Physics; Bounded function; Uniqueness; Three-body problem; Symmetry (geometry); Reflection symmetry; Circular symmetry; Oblate spheroid; Classical mechanics; Lagrangian point; Surface (topology); Domain (mathematical analysis); Motion (physics); Stability (learning theory); Space (punctuation); Mathematical analysis; Geometry; Mathematics","authors":[{"name":"John A. Arredondo","is_ca":false},{"name":"Jianguang Guo","is_ca":true},{"name":"Cristina Stoica","is_ca":true},{"name":"Claudia Tamayo","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.003187040398005403,"gpt":0.1631824329149029,"spread":0.1599953925168975,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008853877,0.001049724,0.002024657,0.0009322127,0.001412891,0.001920831,0.001587632,0.002972684,0.007576983],"category_scores_gemma":[0.005402778,0.0006176623,0.0007947379,0.0007142859,0.003381039,0.003108351,0.003345257,0.002596084,0.0006727509],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0007285227,"about_ca_system_score_gemma":0.0008098396,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.003960761,"about_ca_topic_score_gemma":0.00221847,"domain_scores_codex":[0.9996543,0.000148983,0.00001170455,0.00005301442,0.00006715201,0.00006484842],"domain_scores_gemma":[0.9981772,0.001210026,0.0001947987,0.00007730634,0.0000910471,0.0002497186],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"theoretical_or_conceptual","study_design_scores_codex":[0.0003181782,0.00009319613,0.0008215582,0.0002666517,0.00008098959,0.0005432367,0.0001841822,0.3018716,0.0007626229,0.67773,0.008721545,0.008606161],"study_design_scores_gemma":[0.00009722242,0.00003166175,0.0003887299,0.00003292722,0.00001016128,0.00008265911,0.0001167213,0.3916089,0.0001133619,0.6055192,0.001968647,0.00002971114],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":"theoretical_or_conceptual","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.4040217,0.005268653,0.4163477,0.02017606,0.001481822,0.0001482632,0.0009237036,0.0003284506,0.1513036],"genre_scores_gemma":[0.921193,0.001975313,0.03670748,0.001178484,0.001180248,0.0001863578,0.0007411871,0.0002468406,0.036591],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.007576983,"threshold_uncertainty_score":0.02534747,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2080618918","doi":"10.1007/s00205-006-0047-z","title":"Convex Four-Body Central Configurations with Some Equal Masses","year":2007,"lang":"en","type":"article","venue":"Archive for Rational Mechanics and Analysis","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":49,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Wilfrid Laurier University","funders":"","keywords":"Quadrilateral; Regular polygon; Symmetry (geometry); Line (geometry); Planar; Convex polytope; Line segment; Newtonian fluid","authors":[],"retraction":null,"screen_n_in":null,"score":{"opus":0.006340960885194462,"gpt":0.2051616454779257,"spread":0.1988206845927312,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005435904,0.001494469,0.001224113,0.001725204,0.002067292,0.002224891,0.001378985,0.001350091,0.01200405],"category_scores_gemma":[0.001884906,0.0006299075,0.00082214,0.001056513,0.003201302,0.001899412,0.003148195,0.002073503,0.001513215],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0009965203,"about_ca_system_score_gemma":0.0005529238,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.001030573,"about_ca_topic_score_gemma":0.001033518,"domain_scores_codex":[0.9996151,0.0001031368,0.00001691709,0.00006569672,0.0000979774,0.0001011749],"domain_scores_gemma":[0.9994895,0.000126294,0.00007944524,0.00007633022,0.0001100224,0.0001183958],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"theoretical_or_conceptual","study_design_scores_codex":[0.0001963966,0.00002375055,0.0001597645,0.00004697924,0.0000190266,0.0002277578,0.0001397118,0.01878485,0.002336488,0.9692613,0.00206886,0.006734981],"study_design_scores_gemma":[0.00008808526,0.00009223609,0.0005436667,0.00002788945,0.00001987429,0.0003185541,0.0002661373,0.08483727,0.003157452,0.9060206,0.004580264,0.00004805651],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":"theoretical_or_conceptual","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.3466959,0.0006026299,0.4959331,0.001409297,0.0004358323,0.0001380469,0.0007891878,0.0004337475,0.1535622],"genre_scores_gemma":[0.9321581,0.0002133702,0.03858814,0.0001939021,0.0001032698,0.0001259495,0.0004127793,0.0001828613,0.02802178],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.01200405,"threshold_uncertainty_score":0.04015756,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2029529399","doi":"10.1115/1.2719772","title":"Adaptive Synchronization Control of Multiple Spacecraft Formation Flying","year":2006,"lang":"en","type":"article","venue":"Journal of Dynamic Systems Measurement and Control","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":47,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"York University; University of Toronto","funders":"","keywords":"Spacecraft; Synchronization (alternating current); Control theory (sociology); Computer science; Nonlinear system; Adaptive control; Control (management); Tracking (education); Aerospace engineering; Engineering; Physics; Artificial intelligence; Telecommunications","authors":[{"name":"Hongtao Liu","is_ca":true},{"name":"Jinjun Shan","is_ca":true},{"name":"Dong Sun","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.006331921667650406,"gpt":0.1662297015343118,"spread":0.1598977798666614,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001836639,0.000250297,0.0002241942,0.0001353699,0.0002246885,0.0002426122,0.0003673708,0.0002187373,0.0007450869],"category_scores_gemma":[0.0004740626,0.00007508757,0.0001527466,0.0001687705,0.0002619939,0.0002071328,0.0004593586,0.0002752364,0.00007468909],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0002284544,"about_ca_system_score_gemma":0.0002665142,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.003145955,"about_ca_topic_score_gemma":0.001996439,"domain_scores_codex":[0.9998993,0.00002041517,0.000004394139,0.00002645994,0.00003526009,0.00001415077],"domain_scores_gemma":[0.9998918,0.00002825177,0.00002895268,0.000008165622,0.00003464653,0.000008116136],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.000115514,0.00003123836,0.0006058849,0.0001191206,0.00003870099,0.0002030742,0.0001831118,0.8208862,0.03300762,0.02426281,0.001153187,0.1193935],"study_design_scores_gemma":[0.00002310468,0.00008952952,0.0003252729,0.000004642164,0.000006819219,0.00002143557,0.00001165848,0.9944847,0.001715973,0.002055673,0.001255522,0.000005639713],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.1025407,0.0004971704,0.8897852,0.0001556421,0.0001619882,0.00003574169,0.00002164278,0.0002894888,0.006512359],"genre_scores_gemma":[0.9861135,0.0001473659,0.0120244,0.000023943,0.00003306101,0.00003096318,0.00001675468,0.000006752879,0.001603354],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.003145955,"threshold_uncertainty_score":0.006255329,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2326945679","doi":"10.2514/6.2008-6469","title":"A Bang-Bang Control Approach to Maneuver Spacecraft in a Formation with Differential Drag","year":2008,"lang":"en","type":"article","venue":"AIAA Guidance, Navigation and Control Conference and Exhibit","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":43,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Canadian Space Agency","funders":"","keywords":"Spacecraft; Drag; Control theory (sociology); Differential (mechanical device); Aerospace engineering; Computer science; Control (management); Physics; Aeronautics; Engineering; Artificial intelligence","authors":[{"name":"Balaji Shankar Kumar","is_ca":true},{"name":"Alfred Ng","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.006739779483541572,"gpt":0.1791969519984535,"spread":0.1724571725149119,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001727255,0.0005371921,0.0002810658,0.0002359852,0.0003132501,0.0004984824,0.0006809602,0.0003704076,0.001557808],"category_scores_gemma":[0.0002117503,0.0002192294,0.000322085,0.0002135424,0.0006418035,0.0003126844,0.0005053041,0.0006014538,0.000277829],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0002870987,"about_ca_system_score_gemma":0.0004234235,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.003248289,"about_ca_topic_score_gemma":0.002493148,"domain_scores_codex":[0.9999373,0.00001217941,0.000003810026,0.00001501852,0.00002198444,0.000009793102],"domain_scores_gemma":[0.9999523,0.00001458411,0.000007778471,0.00000492636,0.00001236093,0.000008062408],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.0001576729,0.000113394,0.0006345346,0.0004090098,0.00007938134,0.0004357916,0.000549874,0.5991734,0.04134424,0.1854467,0.003586766,0.1680693],"study_design_scores_gemma":[0.00003827216,0.0003028494,0.0002025837,0.00001919556,0.00001826144,0.00006616192,0.00003477801,0.9704134,0.002611199,0.01676841,0.009504982,0.00001986393],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.01107221,0.0005662311,0.9750615,0.0001768667,0.000124772,0.00004724212,0.00001857561,0.0002830354,0.01264964],"genre_scores_gemma":[0.8212399,0.001191673,0.1568259,0.0002382249,0.0001179278,0.0002083581,0.0000568393,0.00006079444,0.0200604],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.003248289,"threshold_uncertainty_score":0.006458759,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W1994489158","doi":"10.1016/j.jde.2012.01.002","title":"An intrinsic approach in the curved n-body problem: The negative curvature case","year":2012,"lang":"en","type":"article","venue":"Journal of Differential Equations","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":43,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Pacific Institute for the Mathematical Sciences; University of Victoria","funders":"","keywords":"Stereographic projection; Mathematics; Gaussian curvature; Hyperbolic geometry; Mathematical analysis; Motion (physics); Curvature; Geometry; Constant curvature; Classical mechanics; Physics; Differential geometry","authors":[{"name":"Florin Diacu","is_ca":true},{"name":"Ernesto Pérez-Chavela","is_ca":false},{"name":"J. Guadalupe Reyes Victoria","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.01325450356884313,"gpt":0.2399207333099425,"spread":0.2266662297410993,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.001036657,0.0009583036,0.0008273015,0.001096416,0.001064687,0.001477311,0.002048757,0.002154434,0.004738314],"category_scores_gemma":[0.003216312,0.0004676609,0.001056337,0.0005218613,0.002636344,0.003144966,0.003149587,0.002345838,0.0004797781],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.001013074,"about_ca_system_score_gemma":0.0009436764,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.00240763,"about_ca_topic_score_gemma":0.002897491,"domain_scores_codex":[0.9996195,0.0001565845,0.0000144828,0.00007285192,0.0001003845,0.00003619898],"domain_scores_gemma":[0.99919,0.0002448201,0.0001349091,0.00008908616,0.0001748224,0.0001662566],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"theoretical_or_conceptual","study_design_scores_codex":[0.0000148073,0.00002146755,0.0002183594,0.00005055655,0.00001257314,0.0001048472,0.00009092085,0.02195233,0.0007129872,0.9722271,0.001486831,0.003107184],"study_design_scores_gemma":[0.00001338176,0.00003872378,0.0004041995,0.0000307801,0.000008180537,0.0001315647,0.0001099789,0.2995456,0.0001964998,0.6942492,0.005244597,0.00002722325],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":"theoretical_or_conceptual","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.08947786,0.001621107,0.8224313,0.005212542,0.0005858547,0.00005636063,0.0002170308,0.0001319391,0.08026601],"genre_scores_gemma":[0.7924278,0.00211816,0.1491122,0.001063136,0.001139492,0.000140001,0.0003337483,0.0003255572,0.05333992],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.004738314,"threshold_uncertainty_score":0.0158512,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2068310052","doi":"10.1007/s00332-013-9184-3","title":"Relative Equilibria in the Four-Vortex Problem with Two Pairs of Equal Vorticities","year":2013,"lang":"en","type":"article","venue":"Journal of Nonlinear Science","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":41,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Wilfrid Laurier University","funders":"","keywords":"Rhombus; Mathematics; Vortex; Regular polygon; Isosceles triangle; Combinatorics; Equivalence (formal languages); Symmetry (geometry); Algebraic number; Hamiltonian (control theory); Pure mathematics; Mathematical analysis; Geometry; Physics","authors":[{"name":"Marshall Hampton","is_ca":false},{"name":"Gareth E. Roberts","is_ca":false},{"name":"Manuele Santoprete","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.00982860135392271,"gpt":0.2213819940724282,"spread":0.2115533927185055,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.001401007,0.0008835004,0.001304079,0.001639558,0.001404403,0.003701989,0.001381696,0.002875186,0.006708027],"category_scores_gemma":[0.00546095,0.000776185,0.000616408,0.0005398052,0.00284504,0.004111606,0.003938983,0.001865691,0.0005355061],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.001028865,"about_ca_system_score_gemma":0.0008619559,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.002006575,"about_ca_topic_score_gemma":0.001129528,"domain_scores_codex":[0.9995549,0.0001868184,0.00001978187,0.00006136405,0.00008290733,0.00009416365],"domain_scores_gemma":[0.9984968,0.0007810477,0.0002582792,0.00004059504,0.0001379462,0.0002852952],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"theoretical_or_conceptual","study_design_scores_codex":[0.0007357167,0.0002222792,0.00167592,0.000181374,0.00009623684,0.001109699,0.0004979005,0.2789635,0.00368715,0.69949,0.002095596,0.01124461],"study_design_scores_gemma":[0.0003119984,0.0002485502,0.0004402712,0.00006096459,0.00003224896,0.0002056972,0.000740131,0.7895322,0.001161806,0.2056115,0.001591393,0.00006313865],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":"theoretical_or_conceptual","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.7100918,0.0005638571,0.2393317,0.002783387,0.0002370571,0.0001750976,0.0002112739,0.0001658391,0.04644006],"genre_scores_gemma":[0.9705259,0.0001510193,0.01887624,0.000129355,0.00005705187,0.0001094093,0.0001040831,0.00005159646,0.009995341],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.006708027,"threshold_uncertainty_score":0.02244055,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W1561283670","doi":"","title":"Precision Formation Flight: The Can X-4 and Can X -5 Dual Nanosatellite Mission","year":2007,"lang":"en","type":"article","venue":"Digital Commons - USU (Utah State University)","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":41,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":false,"ca_fund":true,"ca_venue":false,"about_ca":true},"ca_institutions":"","funders":"University of Toronto","keywords":"Aerospace engineering; Separation (statistics); Remote sensing; Aerospace; Propulsion; Aeronautics; Position (finance); Satellite; Computer science; Engineering; Geology","authors":[{"name":"Nathan Orr","is_ca":false},{"name":"Jesse Eyer","is_ca":false},{"name":"Benoit P. Larouche","is_ca":false},{"name":"Robert Zee","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.006111698530080125,"gpt":0.172371722029584,"spread":0.1662600234995039,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006184221,0.0003042772,0.0001785798,0.0003515494,0.0007515226,0.0007069359,0.000552172,0.0005577636,0.001852172],"category_scores_gemma":[0.000293611,0.0001112322,0.0001790006,0.0002307442,0.0005872673,0.0004785629,0.001365682,0.0008424095,0.0003778873],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.00132752,"about_ca_system_score_gemma":0.001750251,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.01121112,"about_ca_topic_score_gemma":0.02373026,"domain_scores_codex":[0.9995491,0.00002801822,0.00000609445,0.00004658141,0.0002631834,0.0001069863],"domain_scores_gemma":[0.9998384,0.000008558168,0.00001435259,0.00002079438,0.00003917058,0.00007875921],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","study_design_scores_codex":[0.006899818,0.001667958,0.05908923,0.0004738778,0.000236414,0.003194361,0.002665197,0.06230481,0.3829857,0.05416374,0.05011754,0.3762015],"study_design_scores_gemma":[0.00198422,0.009389872,0.1193644,0.0001727223,0.0001710539,0.002697234,0.001873476,0.178386,0.2596383,0.008681139,0.4173975,0.0002440751],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.8334935,0.0009173728,0.01868397,0.001590067,0.0003470825,0.0004456863,0.001138341,0.001534789,0.1418492],"genre_scores_gemma":[0.9505015,0.0001999353,0.02493294,0.0003087152,0.00003660789,0.000106169,0.002433688,0.00006837604,0.02141205],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.01121112,"threshold_uncertainty_score":0.02229172,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W1970061659","doi":"10.1103/physrevlett.88.241101","title":"Stability and Bifurcations of the Figure-8 Solution of the Three-Body Problem","year":2002,"lang":"en","type":"article","venue":"Physical Review Letters","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":40,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Concordia University","funders":"","keywords":"Homotopy; Three-body problem; Stability (learning theory); Physics; Continuation; Class (philosophy); Mathematics; Mathematical analysis; Classical mechanics; Pure mathematics; Computer science","authors":[{"name":"J. Galán","is_ca":false},{"name":"Francisco Javier Muñoz–Almaraz","is_ca":false},{"name":"E. Freire","is_ca":false},{"name":"Eusebius J. Doedel","is_ca":true},{"name":"André Vanderbauwhede","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.01113048683284689,"gpt":0.211069122157601,"spread":0.1999386353247541,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002783081,0.0002004604,0.0003180284,0.0004430317,0.0005766736,0.000617524,0.0003362122,0.001121336,0.002403083],"category_scores_gemma":[0.001325473,0.0001877283,0.0004369763,0.0001897576,0.0009544416,0.0003781113,0.0005381282,0.0004338089,0.0003148606],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.000503124,"about_ca_system_score_gemma":0.0003326661,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.0009374713,"about_ca_topic_score_gemma":0.0004316551,"domain_scores_codex":[0.9999259,0.00002075863,0.000002867233,0.00001301393,0.0000193726,0.00001807953],"domain_scores_gemma":[0.9997936,0.00006313452,0.0000577908,0.00001676591,0.00003629766,0.00003232318],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"theoretical_or_conceptual","study_design_scores_codex":[0.0005597167,0.0001130392,0.006066036,0.0001615488,0.0001055927,0.001319407,0.001394691,0.4142132,0.126181,0.4233699,0.002646453,0.0238695],"study_design_scores_gemma":[0.0001079105,0.00009473651,0.002581462,0.0000371242,0.00001855685,0.0003507273,0.0002156348,0.9269778,0.009416535,0.05849047,0.001674004,0.00003515941],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":"theoretical_or_conceptual","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.9441475,0.000167928,0.04334879,0.0003882885,0.00003665749,0.00001999186,0.00003747619,0.000094308,0.01175909],"genre_scores_gemma":[0.9897947,0.00006821194,0.0081605,0.00002818816,0.000007440213,0.00002466711,0.00003764788,0.00001719172,0.001861437],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.002403083,"threshold_uncertainty_score":0.008039117,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2804528140","doi":"10.1016/j.ast.2018.05.029","title":"Aerodynamic model-based robust adaptive control for close formation flight","year":2018,"lang":"en","type":"article","venue":"Aerospace Science and Technology","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":40,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"University of Toronto","funders":"Natural Sciences and Engineering Research Council of Canada; China Scholarship Council","keywords":"Aerodynamics; Robustness (evolution); Control theory (sociology); Computer science; Robust control; Micro air vehicle; Control engineering; Engineering; Control system; Control (management); Aerospace engineering; Artificial intelligence","authors":[{"name":"Qingrui Zhang","is_ca":true},{"name":"Hugh H. T. Liu","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.005576281568531494,"gpt":0.199029541071316,"spread":0.1934532595027846,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003903578,0.000671384,0.0009350441,0.0003292861,0.0003625389,0.0006440547,0.000730368,0.0006895876,0.001683521],"category_scores_gemma":[0.001116285,0.0003621867,0.0004721887,0.0002390633,0.0005087449,0.000549265,0.001103846,0.0008481369,0.0002832731],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.000348277,"about_ca_system_score_gemma":0.0004581024,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.007120518,"about_ca_topic_score_gemma":0.004430676,"domain_scores_codex":[0.9997732,0.00005419129,0.00000980698,0.00005121841,0.00007847053,0.00003321191],"domain_scores_gemma":[0.9997097,0.0001093117,0.00006080807,0.00002362772,0.00008180951,0.00001486111],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.00006458723,0.00003052843,0.0001460159,0.00004538696,0.00002943654,0.00003139986,0.00003645258,0.9726784,0.00309888,0.002623467,0.0005686287,0.02064689],"study_design_scores_gemma":[0.000005301367,0.00002926148,0.00006730137,0.000001391295,0.000002692912,0.000004298745,0.000002001487,0.9991326,0.0001597246,0.0004727624,0.000120526,0.00000217091],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"methods","genre_scores_codex":[0.03633057,0.0003701315,0.9583563,0.0001815538,0.0001553761,0.00002865288,0.00003595875,0.0004584623,0.004082866],"genre_scores_gemma":[0.9830459,0.0001275533,0.0139275,0.00006105226,0.00005404089,0.00006913266,0.00005830099,0.00003483935,0.002621609],"genre_candidate":"methods","genre_consensus":"methods","teacher_disagreement_score":0.007120518,"threshold_uncertainty_score":0.01415813,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2011993410","doi":"10.1016/j.ast.2014.04.004","title":"Low-thrust trajectory design with constrained particle swarm optimization","year":2014,"lang":"en","type":"article","venue":"Aerospace Science and Technology","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":39,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"York University","funders":"","keywords":"Particle swarm optimization; Thrust; Trajectory; Trajectory optimization; Multi-swarm optimization; Particle (ecology); Control theory (sociology); Aerospace engineering; Mathematical optimization; Computer science; Physics; Engineering; Mathematics; Geology; Artificial intelligence","authors":[{"name":"Jinjun Shan","is_ca":true},{"name":"Yuan Ren","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.003271104028031969,"gpt":0.1684758946865334,"spread":0.1652047906585014,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007004968,0.0011215,0.0009957929,0.0007797345,0.000502324,0.0009019,0.000849465,0.001418691,0.002620071],"category_scores_gemma":[0.002535697,0.0007320739,0.0005242359,0.0006178778,0.0007016406,0.001010212,0.001224658,0.0009633243,0.000525968],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.000521745,"about_ca_system_score_gemma":0.001292579,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.003916338,"about_ca_topic_score_gemma":0.002481645,"domain_scores_codex":[0.9997277,0.00008573978,0.00001337865,0.00004391907,0.00009716322,0.00003223338],"domain_scores_gemma":[0.9993134,0.0003670958,0.00009821872,0.00003903641,0.0001350343,0.00004721002],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.00006514665,0.00002355934,0.0001730577,0.00005379355,0.0000187928,0.00003207152,0.00003308421,0.9805925,0.00109724,0.004071905,0.0004409563,0.01339784],"study_design_scores_gemma":[0.00000823305,0.00002314625,0.00002687212,0.000002908049,0.000001826419,0.000002913923,0.000003127859,0.9987339,0.0001575926,0.0008955811,0.0001422828,0.000001652054],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.009113093,0.0001168742,0.9879594,0.0001119846,0.0000365091,0.00004817781,0.00002638054,0.000137113,0.002450512],"genre_scores_gemma":[0.694818,0.0002733043,0.2976729,0.0001241927,0.00006637393,0.0005163707,0.0002140786,0.0001509104,0.006163832],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.003916338,"threshold_uncertainty_score":0.008764982,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2141674198","doi":"10.1007/s10569-007-9102-9","title":"Seven-body central configurations: a family of central configurations in the spatial seven-body problem","year":2007,"lang":"en","type":"article","venue":"Celestial Mechanics and Dynamical Astronomy","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":38,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Wilfrid Laurier University","funders":"","keywords":"Concentric; Simplex; Newtonian fluid; Celestial mechanics","authors":[],"retraction":null,"screen_n_in":null,"score":{"opus":0.004352839425113587,"gpt":0.1941981626705457,"spread":0.1898453232454321,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.001114363,0.0009558662,0.001422476,0.001534335,0.002113661,0.002576554,0.001600114,0.002328324,0.007131287],"category_scores_gemma":[0.003713369,0.0005400821,0.0009251499,0.001108043,0.00351311,0.002803118,0.003095737,0.002620546,0.0009523587],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0006585025,"about_ca_system_score_gemma":0.00116115,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.0008095299,"about_ca_topic_score_gemma":0.0007665487,"domain_scores_codex":[0.9995406,0.0001671822,0.00001318743,0.00007236659,0.0001157729,0.00009081272],"domain_scores_gemma":[0.9986797,0.0004032428,0.0001533264,0.0001422726,0.0002501037,0.0003713026],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"theoretical_or_conceptual","study_design_scores_codex":[0.0001306298,0.00004520977,0.0007145991,0.00007529564,0.0000274868,0.0003422434,0.0001547714,0.03183992,0.001075229,0.9465597,0.005838822,0.01319603],"study_design_scores_gemma":[0.00005591273,0.0000426586,0.0003226128,0.00004185945,0.000009074229,0.0002977831,0.0001801525,0.1361631,0.0003710749,0.8594804,0.003006812,0.00002868044],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":"theoretical_or_conceptual","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.3546273,0.002174775,0.5570151,0.003679359,0.0005706418,0.0001464044,0.000443673,0.0005536833,0.08078921],"genre_scores_gemma":[0.9304729,0.0009367337,0.05358566,0.0005984958,0.0003032309,0.0001766318,0.0006452946,0.0002697647,0.0130113],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.007131287,"threshold_uncertainty_score":0.02385652,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2112178366","doi":"10.1080/00207179.2011.582157","title":"Cooperative actuator fault accommodation in formation flight of unmanned vehicles using relative measurements","year":2011,"lang":"en","type":"article","venue":"International Journal of Control","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":37,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"Concordia University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Supervisor; Actuator; Fault (geology); Control theory (sociology); Controller (irrigation); Accommodation; Hierarchy; Control engineering; Fault tolerance; Engineering; Control (management); Computer science; Reliability engineering; Artificial intelligence","authors":[{"name":"S. Mohsen Azizi","is_ca":true},{"name":"K. Khorasani","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.03260077640033182,"gpt":0.2495083919345672,"spread":0.2169076155342353,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006148788,0.0005149289,0.0004935316,0.0002416746,0.0003729341,0.0004883868,0.0008946898,0.0005335291,0.00032695],"category_scores_gemma":[0.001938117,0.0002511983,0.0003260302,0.0002302572,0.0006988318,0.000803115,0.0008252839,0.0005651863,0.00007967833],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0004544627,"about_ca_system_score_gemma":0.0005794267,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.004467553,"about_ca_topic_score_gemma":0.003587684,"domain_scores_codex":[0.9994336,0.0001496229,0.00001983308,0.0001507398,0.0001751711,0.00007106922],"domain_scores_gemma":[0.9992899,0.0002243856,0.0002365552,0.00009933066,0.0001135461,0.00003632265],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.0001934362,0.00006372822,0.002078567,0.0001152101,0.00004579599,0.0002428275,0.0004441135,0.8989805,0.02857361,0.008417543,0.0002341596,0.06061053],"study_design_scores_gemma":[0.000009557359,0.0001694183,0.00065219,0.000004055074,0.000008795262,0.00003163781,0.00004439661,0.9938345,0.003422657,0.001504337,0.0003103235,0.000008106594],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.09332456,0.0001991437,0.9052451,0.00006439701,0.00001841282,0.00002364997,0.000007606482,0.0001887511,0.0009284837],"genre_scores_gemma":[0.9829009,0.00004049195,0.01659143,0.00001155799,0.000008587901,0.00001401207,0.000007945525,0.000004958696,0.0004202303],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.004467553,"threshold_uncertainty_score":0.008883059,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2005815933","doi":"10.2514/1.20126","title":"Improvement to the Analytical Predictor-Corrector Guidance Algorithm Applied to Mars Aerocapture","year":2006,"lang":"en","type":"article","venue":"Journal of Guidance Control and Dynamics","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":37,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Algorithm; Atmospheric entry; Circular orbit; Orbital maneuver; Mars Exploration Program; Orbit (dynamics); Reduction (mathematics); Aerospace engineering; Predictor–corrector method; Elliptic orbit; Computer science; Physics; Control theory (sociology); Spacecraft; Mathematics; Engineering; Geometry; Classical mechanics","authors":[{"name":"Jean‐François Hamel","is_ca":true},{"name":"Jean de Lafontaine","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.001791282179320886,"gpt":0.1775430282177747,"spread":0.1757517460384538,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004090446,0.0006193925,0.0004090002,0.0004242223,0.0004594618,0.0006170948,0.0008370859,0.0006357969,0.003791486],"category_scores_gemma":[0.001983237,0.0001655512,0.0002685594,0.0004021607,0.0003605507,0.0003704523,0.0005385836,0.0008345629,0.0008294252],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0005052039,"about_ca_system_score_gemma":0.001871819,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.01454636,"about_ca_topic_score_gemma":0.007553301,"domain_scores_codex":[0.9997652,0.00003513269,0.00001257248,0.00003696221,0.0001153665,0.00003485118],"domain_scores_gemma":[0.9996096,0.00009566599,0.0000300466,0.00003886825,0.0002072089,0.00001860763],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.0001239092,0.00006315362,0.001353294,0.00008210668,0.0000203261,0.0001242602,0.0001026995,0.632701,0.007083019,0.01367641,0.003018676,0.3416512],"study_design_scores_gemma":[0.000006727168,0.00002357584,0.00007958638,0.000004510712,0.00000187828,0.00002199926,0.000004553379,0.9969908,0.00111245,0.0004739015,0.001277544,0.000002388025],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"methods","genre_scores_codex":[0.01560145,0.0002155338,0.9765646,0.0002246281,0.0001146131,0.00005978985,0.00003469011,0.001291768,0.005892844],"genre_scores_gemma":[0.5245679,0.000410231,0.4652233,0.0001331912,0.00009758751,0.0001413377,0.0001504063,0.000117985,0.009158005],"genre_candidate":"methods","genre_consensus":"methods","teacher_disagreement_score":0.01454636,"threshold_uncertainty_score":0.02892339,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W1928296088","doi":"10.1007/s10569-012-9434-y","title":"Boundary-value problem formulations for computing invariant manifolds and connecting orbits in the circular restricted three body problem","year":2012,"lang":"en","type":"article","venue":"Celestial Mechanics and Dynamical Astronomy","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":37,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"Concordia University; McGill University","funders":"Natural Sciences and Engineering Research Council of Canada; Fonds Québécois de la Recherche sur la Nature et les Technologies","keywords":"Homoclinic orbit; Heteroclinic orbit; Halo orbit; Heteroclinic cycle; Invariant (physics); Periodic orbits; Continuation; Orbit (dynamics); Lyapunov function; Fixed point","authors":[],"retraction":null,"screen_n_in":null,"score":{"opus":0.007703325401235662,"gpt":0.2054666783213994,"spread":0.1977633529201638,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.001340218,0.0007595443,0.001145219,0.001230164,0.001021042,0.001828776,0.001836115,0.002366617,0.005477929],"category_scores_gemma":[0.006884488,0.0006280297,0.0008865218,0.0006573729,0.001913309,0.002924117,0.002640026,0.002317747,0.0006607591],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0008096147,"about_ca_system_score_gemma":0.0009875599,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.003098259,"about_ca_topic_score_gemma":0.00301966,"domain_scores_codex":[0.9996967,0.0001197503,0.00001631981,0.00005604795,0.0000802096,0.0000309641],"domain_scores_gemma":[0.9983698,0.001101354,0.0001021956,0.00008326056,0.0002095833,0.0001338376],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"theoretical_or_conceptual","study_design_scores_codex":[0.0001314065,0.00009330343,0.0006839045,0.0001239923,0.00002552056,0.00009900011,0.0002347736,0.7445932,0.001846676,0.2182499,0.001937339,0.03198091],"study_design_scores_gemma":[0.000009315143,0.00001201365,0.00003578192,0.0000101209,0.000002317551,0.000006318908,0.00002468106,0.9548328,0.0002280759,0.04449297,0.0003408002,0.000004949902],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":null,"genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.02122291,0.0001147977,0.9751548,0.0002255878,0.0000327144,0.00003903984,0.00005767129,0.0001312078,0.003021214],"genre_scores_gemma":[0.4354165,0.0002018209,0.5582721,0.0001312991,0.00008226009,0.0002838586,0.000475053,0.0004636559,0.004673492],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.005477929,"threshold_uncertainty_score":0.01832551,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2139528613","doi":"10.1007/s10569-009-9219-0","title":"Central configurations of the five-body problem with equal masses","year":2009,"lang":"en","type":"article","venue":"Celestial Mechanics and Dynamical Astronomy","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":37,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Wilfrid Laurier University","funders":"","keywords":"Homotopy; Exact solutions in general relativity; n-body problem; Homotopy lifting property; Three-body problem","authors":[],"retraction":null,"screen_n_in":null,"score":{"opus":0.002275152269308595,"gpt":0.1627184287166644,"spread":0.1604432764473558,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.001111422,0.0007949179,0.001162057,0.001248333,0.001463348,0.00313424,0.001645195,0.002439834,0.01277722],"category_scores_gemma":[0.003530526,0.0006465791,0.0006756113,0.000681858,0.003548081,0.002608029,0.003814204,0.002135459,0.000901223],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.001036099,"about_ca_system_score_gemma":0.001098657,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.001838207,"about_ca_topic_score_gemma":0.0017964,"domain_scores_codex":[0.9996427,0.0001676556,0.00001224976,0.00005099484,0.00006514495,0.00006116662],"domain_scores_gemma":[0.9989465,0.0003824371,0.0001606526,0.00005613968,0.0001369028,0.0003173358],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"theoretical_or_conceptual","study_design_scores_codex":[0.0004167604,0.00008484453,0.0005552253,0.00008060352,0.00003690017,0.0003396365,0.0001426387,0.0954235,0.0007575125,0.8949285,0.002442315,0.004791534],"study_design_scores_gemma":[0.0002832891,0.00008032375,0.0004984318,0.00005143049,0.00001740956,0.0001449957,0.0003102192,0.2483934,0.0003879318,0.748091,0.001700016,0.00004153655],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":"theoretical_or_conceptual","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.5946602,0.001279417,0.2786233,0.005738274,0.0006759173,0.000149887,0.0006442025,0.0002464674,0.1179824],"genre_scores_gemma":[0.9566296,0.0002699246,0.02633244,0.0002746241,0.0001843364,0.0001337509,0.0003517594,0.0001153572,0.01570813],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.01277722,"threshold_uncertainty_score":0.04274404,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2346174159","doi":"10.1016/j.asr.2016.04.022","title":"State dependent model predictive control for orbital rendezvous using pulse-width pulse-frequency modulated thrusters","year":2016,"lang":"en","type":"article","venue":"Advances in Space Research","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":35,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"University of New Brunswick; University of Toronto; York University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Control theory (sociology); Model predictive control; Optimal control; Sequential quadratic programming; Trajectory; Pulse-width modulation; Pulse (music); Trajectory optimization; Spacecraft; Orbit (dynamics); Computer science; Physics; Quadratic programming; Mathematics; Optics; Voltage; Control (management); Mathematical optimization; Engineering; Aerospace engineering; Detector","authors":[{"name":"Peng Li","is_ca":true},{"name":"Zheng Zhu","is_ca":true},{"name":"S. A. Meguid","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.02173177700804565,"gpt":0.3140503776622215,"spread":0.2923186006541759,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002061821,0.0004458372,0.0004557134,0.0001525542,0.0004201286,0.0005881394,0.0005349664,0.0004064805,0.001040816],"category_scores_gemma":[0.0005335453,0.0002444399,0.0002641253,0.0002077791,0.0003638704,0.000369257,0.0004384458,0.0006080655,0.0001450681],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0003280278,"about_ca_system_score_gemma":0.0004264332,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.006177531,"about_ca_topic_score_gemma":0.005637601,"domain_scores_codex":[0.9999114,0.00001827017,0.000004278603,0.00001843855,0.00003368098,0.00001388212],"domain_scores_gemma":[0.9998491,0.00006511665,0.00002681905,0.0000117393,0.00004134734,0.000005824194],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.0001531069,0.00004419722,0.0003342746,0.00007338587,0.0000408688,0.00007355361,0.00007940649,0.9483128,0.01202118,0.00374016,0.0006579029,0.0344692],"study_design_scores_gemma":[0.000005773513,0.00002642796,0.0000815392,0.000001880833,0.0000039223,0.00000317501,0.00000302965,0.998668,0.0007813149,0.0002815157,0.0001413315,0.000002160713],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"methods","genre_scores_codex":[0.208941,0.0007221328,0.7789758,0.0004159796,0.0002449442,0.00004966367,0.00006785041,0.0004637933,0.01011873],"genre_scores_gemma":[0.9928115,0.00009745402,0.005294446,0.00001830959,0.00001295572,0.00002312673,0.00001866501,0.000007147389,0.001716461],"genre_candidate":"methods","genre_consensus":"methods","teacher_disagreement_score":0.006177531,"threshold_uncertainty_score":0.01228315,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W1973148663","doi":"10.1088/0951-7715/22/12/006","title":"Numerical continuation of families of homoclinic connections of periodic orbits in the RTBP","year":2009,"lang":"en","type":"article","venue":"Nonlinearity","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":34,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Homoclinic orbit; Mathematics; Continuation; Numerical continuation; Manifold (fluid mechanics); Stable manifold; Nonlinear system; Computation; Mathematical analysis; Section (typography); Periodic point; Homoclinic bifurcation; Planar; Equilibrium point; Numerical analysis; Bifurcation; Differential equation","authors":[{"name":"Esther Barrabés","is_ca":false},{"name":"Josep–Maria Mondelo","is_ca":true},{"name":"Mercè Ollé","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.008412961014896563,"gpt":0.2409163205771742,"spread":0.2325033595622777,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006763522,0.0002820502,0.0003461912,0.000655069,0.0004727134,0.0005159185,0.0004657522,0.0006309021,0.001739244],"category_scores_gemma":[0.0024902,0.0002371572,0.0002976413,0.000314686,0.000767311,0.0003858656,0.0005963456,0.0005133587,0.0001925882],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0005148032,"about_ca_system_score_gemma":0.0005233088,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.002221877,"about_ca_topic_score_gemma":0.001627296,"domain_scores_codex":[0.9999113,0.00003427793,0.000003917835,0.00001012056,0.00002746239,0.00001293396],"domain_scores_gemma":[0.999402,0.0003015809,0.00009248043,0.00006734328,0.00008506212,0.00005153402],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.00009505433,0.00004235274,0.002100476,0.00005671522,0.00001591499,0.0001522362,0.0002414152,0.9620097,0.00374721,0.01973452,0.0001844074,0.01162002],"study_design_scores_gemma":[0.000007766681,0.00001542822,0.0001721542,0.000006188632,0.000001552223,0.00001360831,0.00003028329,0.9971862,0.0005018273,0.00188182,0.0001792588,0.000003815834],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.7988247,0.0001184663,0.191242,0.000123154,0.00003346328,0.00007873961,0.00009405275,0.0003761475,0.00910924],"genre_scores_gemma":[0.9347378,0.00005937016,0.06356925,0.00001514386,0.000006109169,0.00009448779,0.00005820947,0.00005916787,0.001400473],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.002221877,"threshold_uncertainty_score":0.005818307,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2075088810","doi":"10.1016/j.actaastro.2006.07.009","title":"Stability of equilibrium points in the restricted full three-body problem","year":2006,"lang":"en","type":"article","venue":"Acta Astronautica","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":34,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":false,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"","funders":"Jet Propulsion Laboratory; Fonds Québécois de la Recherche sur la Nature et les Technologies; Natural Sciences and Engineering Research Council of Canada; California Institute of Technology","keywords":"Ellipsoid; Gravitational field; Stability (learning theory); Equilateral triangle; Orbit (dynamics); Classical mechanics; Mathematics; Physics; Equilibrium point; Mathematical analysis; Range (aeronautics); Mass distribution; Three-body problem; Geometry; Materials science; Differential equation","authors":[{"name":"Julie Bellerose","is_ca":false},{"name":"Daniel J. Scheeres","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.005796439376802387,"gpt":0.190767099725871,"spread":0.1849706603490686,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006465021,0.0005013783,0.0008973689,0.0009874635,0.0007134753,0.001405493,0.0009498816,0.0009839536,0.002615588],"category_scores_gemma":[0.003410278,0.0003755687,0.0005407193,0.000447081,0.001843171,0.001219239,0.002482477,0.00101914,0.0004159012],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0004425409,"about_ca_system_score_gemma":0.0005118823,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.002789048,"about_ca_topic_score_gemma":0.001292193,"domain_scores_codex":[0.999793,0.00008466063,0.000007272055,0.00003122547,0.0000449872,0.0000389393],"domain_scores_gemma":[0.999288,0.0004065332,0.00009347471,0.0000460288,0.00009319664,0.00007282395],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"theoretical_or_conceptual","study_design_scores_codex":[0.0006027736,0.0001040089,0.00232128,0.0001736283,0.0001307761,0.0005001579,0.0005149413,0.7325597,0.007097084,0.2347745,0.001848289,0.01937288],"study_design_scores_gemma":[0.0000519139,0.00005441947,0.0007430906,0.00002104018,0.00001074571,0.00005252675,0.0001437995,0.8630624,0.0007381546,0.1345354,0.0005704226,0.00001609929],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":null,"genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.7312263,0.0004359178,0.2437277,0.0009624353,0.00004901408,0.00007675355,0.0002597354,0.0001601363,0.02310201],"genre_scores_gemma":[0.9852039,0.0001759435,0.01052947,0.00005151256,0.00002895872,0.00008362057,0.0001654604,0.00005020323,0.003710902],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.002789048,"threshold_uncertainty_score":0.008750081,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2888079633","doi":"10.2514/1.a34117","title":"GPS Relative Navigation for the CanX-4 and CanX-5 Formation-Flying Nanosatellites","year":2018,"lang":"en","type":"article","venue":"Journal of Spacecraft and Rockets","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":33,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"University of Toronto; University of Calgary","funders":"Natural Sciences and Engineering Research Council of Canada; Canadian Space Agency; Zonta International Foundation; Engineers Canada; Alberta Innovates; Alberta Innovates - Technology Futures; Ontario Centres of Excellence","keywords":"Spacecraft; Global Positioning System; Orbit determination; Aerospace engineering; Orbit (dynamics); Computer science; Differential GPS; Geodesy; Differential (mechanical device); Aerospace; Range (aeronautics); Remote sensing; Engineering; Geology; Telecommunications","authors":[{"name":"Erin Kahr","is_ca":true},{"name":"Niels Roth","is_ca":true},{"name":"Oliver Montenbruck","is_ca":false},{"name":"Ben Risi","is_ca":true},{"name":"Robert Zee","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.006955105655757138,"gpt":0.2135149340685764,"spread":0.2065598284128193,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005257304,0.0002303617,0.0002087031,0.0003886774,0.0003768588,0.0004726178,0.0003581189,0.0002000255,0.001239077],"category_scores_gemma":[0.0007925505,0.000125499,0.000142704,0.0004359976,0.0002498621,0.0002697174,0.0003869187,0.0003487722,0.0002878815],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0007591173,"about_ca_system_score_gemma":0.0008088537,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.01393381,"about_ca_topic_score_gemma":0.0248107,"domain_scores_codex":[0.9997138,0.0000580835,0.000006528103,0.00004197597,0.0001537794,0.00002581952],"domain_scores_gemma":[0.9998485,0.00002766071,0.00001541501,0.00002291977,0.0000672017,0.00001827449],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","study_design_scores_codex":[0.002167445,0.0001837759,0.03000274,0.000418338,0.0001770947,0.0002441245,0.001563966,0.3866441,0.1372921,0.02159542,0.00701429,0.4126967],"study_design_scores_gemma":[0.0002632155,0.001862738,0.04723439,0.00008658355,0.0001095942,0.0002647128,0.0005789142,0.7982265,0.09944417,0.003301999,0.04852961,0.00009754458],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.7954615,0.0007993531,0.1689911,0.0003448168,0.0001025713,0.0001156509,0.0007750636,0.001876333,0.0315335],"genre_scores_gemma":[0.9394251,0.0001406329,0.05404487,0.00002842658,0.00001012254,0.00003823558,0.001028207,0.0001126129,0.005171706],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.01393381,"threshold_uncertainty_score":0.02770543,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2768701690","doi":"10.1016/j.actaastro.2017.10.027","title":"Onboard guidance system design for reusable launch vehicles in the terminal area energy management phase","year":2017,"lang":"en","type":"article","venue":"Acta Astronautica","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":32,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"Concordia University","funders":"Natural Sciences and Engineering Research Council of Canada; National Natural Science Foundation of China","keywords":"Terminal (telecommunication); Phase (matter); Systems engineering; Launch vehicle; Engineering; Aeronautics; Aerospace engineering; Automotive engineering; Telecommunications; Physics","authors":[{"name":"Lingxia Mu","is_ca":true},{"name":"Xiang Yu","is_ca":true},{"name":"Youmin Zhang","is_ca":true},{"name":"Ping Li","is_ca":false},{"name":"Xinmin Wang","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.01656874066241052,"gpt":0.2427459757004044,"spread":0.2261772350379939,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002670031,0.0006105923,0.0003517904,0.0003938505,0.000636983,0.001018768,0.0006270957,0.0007641846,0.005506696],"category_scores_gemma":[0.0004662984,0.0002273061,0.00027396,0.0001986695,0.0002260025,0.0004475882,0.0005406428,0.0004212254,0.0008595761],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0005520081,"about_ca_system_score_gemma":0.001586473,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.008093366,"about_ca_topic_score_gemma":0.009208025,"domain_scores_codex":[0.9997485,0.00004640039,0.000008312232,0.00003933885,0.00009940383,0.00005795609],"domain_scores_gemma":[0.9997768,0.00003168869,0.00002979163,0.00002040197,0.0001228721,0.00001846619],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.0005792813,0.0001962168,0.00232594,0.000439101,0.00009104292,0.0003523671,0.0005677317,0.6058397,0.1576298,0.01114383,0.003787727,0.2170473],"study_design_scores_gemma":[0.0001006518,0.001065264,0.002078298,0.00003984038,0.00006905932,0.000120253,0.0002346212,0.950424,0.03149793,0.001540942,0.01280678,0.0000225172],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"methods","genre_scores_codex":[0.1689337,0.0002975198,0.795373,0.0002946197,0.0001451019,0.0003121173,0.0001506433,0.001129244,0.03336402],"genre_scores_gemma":[0.9428056,0.0001518482,0.04622411,0.00006457764,0.00002861393,0.0001562342,0.0001646992,0.00009918639,0.01030516],"genre_candidate":"methods","genre_consensus":"methods","teacher_disagreement_score":0.008093366,"threshold_uncertainty_score":0.01842171,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W1523389231","doi":"10.2514/1.g000903","title":"Reliability-Based Soft Landing Trajectory Optimization near Asteroid with Uncertain Gravitational Field","year":2015,"lang":"en","type":"article","venue":"Journal of Guidance Control and Dynamics","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":31,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"York University","funders":"","keywords":"Trajectory optimization; Trajectory; Optimal control; Control theory (sociology); Gravitational field; Optimization problem; Reliability (semiconductor); Boundary value problem; Computer science; Mathematical optimization; Mathematics; Physics; Mathematical analysis; Control (management); Classical mechanics","authors":[{"name":"Yuan Ren","is_ca":true},{"name":"Jinjun Shan","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.00541745003008289,"gpt":0.2018130149907021,"spread":0.1963955649606192,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000593161,0.0008224992,0.0007723505,0.0004718099,0.0003976664,0.0005355518,0.0005082827,0.0005147885,0.0009056039],"category_scores_gemma":[0.001089153,0.0004626741,0.0005594981,0.0002760094,0.0005212995,0.0005839947,0.0006616495,0.000623845,0.0001354345],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0006629374,"about_ca_system_score_gemma":0.001006372,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.007479275,"about_ca_topic_score_gemma":0.002800673,"domain_scores_codex":[0.9997807,0.00005743195,0.000009242574,0.0000472653,0.00006726011,0.00003804337],"domain_scores_gemma":[0.9995463,0.000212804,0.00009325079,0.00002784176,0.00008960933,0.00003012348],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.00001829716,0.000004122136,0.0001852944,0.00001701873,0.00000716448,0.00002634698,0.00002228119,0.9920547,0.000922129,0.001662599,0.00008232095,0.004997754],"study_design_scores_gemma":[0.000002455804,0.00001180803,0.00005163018,0.000001458823,0.000001793306,0.000003457358,0.000004244446,0.9990951,0.0001631881,0.0005986062,0.00006471369,0.000001696734],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.04685246,0.000181286,0.9504793,0.0001079312,0.00001624971,0.00001891298,0.00002059105,0.0001217325,0.002201461],"genre_scores_gemma":[0.9495269,0.0001527109,0.04824396,0.00002202821,0.00001309386,0.00006520123,0.00005841379,0.0000469325,0.001870696],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.007479275,"threshold_uncertainty_score":0.01487148,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2084009366","doi":"10.1016/j.actaastro.2014.10.008","title":"Robust stationkeeping and reconfiguration of underactuated spacecraft formations","year":2014,"lang":"en","type":"article","venue":"Acta Astronautica","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":31,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"Toronto Metropolitan University","funders":"Natural Sciences and Engineering Research Council of Canada; Canada Research Chairs","keywords":"Control theory (sociology); Underactuation; Control reconfiguration; Nonlinear system; Robustness (evolution); Spacecraft; Thrust; Computer science; Backstepping; Control engineering; Engineering; Control (management); Physics; Adaptive control; Aerospace engineering","authors":[{"name":"Godard","is_ca":true},{"name":"Krishna Dev Kumar","is_ca":true},{"name":"An‐Min Zou","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.00800823340531275,"gpt":0.1788140520621096,"spread":0.1708058186567969,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003158862,0.000455746,0.000714126,0.000358994,0.0004121949,0.0009674025,0.0005163259,0.0002487269,0.0007922258],"category_scores_gemma":[0.00148146,0.0002744042,0.0003234334,0.0002962818,0.0007965508,0.000468703,0.0009138049,0.0004559946,0.0001475001],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0002603447,"about_ca_system_score_gemma":0.0004750105,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.00220908,"about_ca_topic_score_gemma":0.00176059,"domain_scores_codex":[0.9997317,0.00006655495,0.00001490934,0.00007910835,0.00005837642,0.00004934039],"domain_scores_gemma":[0.9994801,0.0001323969,0.0001702798,0.000119625,0.00006098812,0.00003666292],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.0002676476,0.0000274109,0.0007723293,0.00005288848,0.00005454612,0.0001678612,0.0001875927,0.9251713,0.01558803,0.01745317,0.0004694109,0.03978794],"study_design_scores_gemma":[0.00002414199,0.0001783015,0.001012406,0.000005372349,0.00001619834,0.0000631314,0.00004478138,0.9829689,0.003888761,0.01093735,0.0008481736,0.00001252045],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.4502024,0.0004073334,0.5417578,0.000142462,0.0001081837,0.00003095696,0.00009273266,0.0004708015,0.006787324],"genre_scores_gemma":[0.9909489,0.00006990143,0.00787092,0.000008331086,0.00001638677,0.00001142427,0.00003417801,0.00001954225,0.001020539],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.00220908,"threshold_uncertainty_score":0.004392445,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W3187771405","doi":"10.1016/j.ast.2021.106971","title":"Distributed optimal control allocation for 6-dof spacecraft with redundant thrusters","year":2021,"lang":"en","type":"article","venue":"Aerospace Science and Technology","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":28,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"Toronto Metropolitan University","funders":"Natural Sciences and Engineering Research Council of Canada; Canada Research Chairs","keywords":"Thrust; Spacecraft; Control theory (sociology); Optimal control; Norm (philosophy); Computer science; Scheme (mathematics); Optimal allocation; Mathematical optimization; Distributed computing; Topology (electrical circuits); Engineering; Control (management); Mathematics; Aerospace engineering","authors":[{"name":"Xiaoyu Lang","is_ca":true},{"name":"Anton de Ruiter","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.002556779781313152,"gpt":0.1860814045493775,"spread":0.1835246247680644,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004328497,0.0006064189,0.000713894,0.0002971746,0.0002910078,0.0004694253,0.000596863,0.0004538848,0.002057353],"category_scores_gemma":[0.0009480565,0.0002713465,0.0002964889,0.0002700826,0.0004369617,0.0004914691,0.0007950569,0.0003468877,0.00022829],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0003235778,"about_ca_system_score_gemma":0.0003816436,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.001864067,"about_ca_topic_score_gemma":0.001544763,"domain_scores_codex":[0.9997985,0.00005879294,0.0000104517,0.00003571676,0.00004554801,0.00005101884],"domain_scores_gemma":[0.9997203,0.000106715,0.00005458172,0.00003152167,0.00005957954,0.00002730644],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.0002315481,0.00003648906,0.0001619072,0.00003982659,0.00002195387,0.00004182127,0.00003728063,0.9721178,0.004013866,0.003574935,0.0003235094,0.01939907],"study_design_scores_gemma":[0.00001962041,0.00006206259,0.0001124177,0.000001940154,0.000003538836,0.00000625541,0.000008051302,0.9974774,0.0004390939,0.001698761,0.0001679588,0.000002943964],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.1718549,0.0002847397,0.8208158,0.000181204,0.00009104666,0.00004183458,0.00005297305,0.0001679072,0.006509626],"genre_scores_gemma":[0.9769601,0.00007094153,0.02028155,0.00002405772,0.00003189536,0.00004250304,0.00002767805,0.00001542041,0.002545873],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.002057353,"threshold_uncertainty_score":0.006882489,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W3118933506","doi":"10.1007/s11071-020-06067-7","title":"Stability and control of radial deployment of electric solar wind sail","year":2021,"lang":"en","type":"article","venue":"Nonlinear Dynamics","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":28,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"York University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Solar sail; Software deployment; Aerospace engineering; Stability (learning theory); Control theory (sociology); Aeronautics; Physics; Environmental science; Engineering; Computer science; Control (management); Propulsion","authors":[{"name":"Gangqiang Li","is_ca":true},{"name":"Zheng Zhu","is_ca":true},{"name":"Chonggang Du","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.004018698531111885,"gpt":0.1845209168867157,"spread":0.1805022183556038,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003263885,0.0005112786,0.0003259211,0.0002601197,0.0003552338,0.0006482077,0.0002870743,0.0002909029,0.001269569],"category_scores_gemma":[0.0007715116,0.0001786421,0.0001929337,0.0001319725,0.0005168794,0.0002422388,0.0005501429,0.0003114838,0.0001545743],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0003596514,"about_ca_system_score_gemma":0.0002945064,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.005701813,"about_ca_topic_score_gemma":0.003218243,"domain_scores_codex":[0.9999173,0.00003103956,0.000002598492,0.00001651262,0.00001600372,0.00001661655],"domain_scores_gemma":[0.999782,0.00006693257,0.00004615114,0.000009019738,0.00007400958,0.00002191476],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.0005854108,0.00005240162,0.001340442,0.00008556341,0.00004164813,0.0001445231,0.0001585588,0.9482233,0.01888849,0.01186988,0.001062101,0.01754765],"study_design_scores_gemma":[0.000007252647,0.00006537892,0.0003477586,0.000002898165,0.000003277387,0.000005577852,0.00002547413,0.9982464,0.000530837,0.000612072,0.000149972,0.000003011242],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.7292745,0.0004374932,0.2422595,0.0004209059,0.0001631836,0.00005160196,0.00008131222,0.0002039336,0.02710761],"genre_scores_gemma":[0.9979552,0.00003695886,0.0006234977,0.000007118149,0.000006428738,0.000006755976,0.000008422634,0.000005955968,0.001349678],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.005701813,"threshold_uncertainty_score":0.01133722,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2990107848","doi":"10.2514/1.g004608","title":"Flight Dynamics and Control Strategy of Electric Solar Wind Sails","year":2019,"lang":"en","type":"article","venue":"Journal of Guidance Control and Dynamics","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":28,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"York University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Solar sail; Aerospace engineering; Physics; Attitude control; Dynamics (music); Electric field; Control theory (sociology); Computer science; Engineering; Propulsion; Control (management); Acoustics","authors":[{"name":"Gangqiang Li","is_ca":true},{"name":"Zheng Zhu","is_ca":true},{"name":"Chonggang Du","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.001860661539241704,"gpt":0.1749048745213933,"spread":0.1730442129821516,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001309937,0.0003227068,0.0002345147,0.0001432988,0.0002978426,0.0003325054,0.0003474563,0.0003084536,0.001019624],"category_scores_gemma":[0.0002076428,0.0001129274,0.0002117125,0.00006515218,0.0002933633,0.0002436184,0.0003001487,0.0002544716,0.0001201269],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0001571691,"about_ca_system_score_gemma":0.0002310154,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.00277329,"about_ca_topic_score_gemma":0.001727557,"domain_scores_codex":[0.9999545,0.00001086828,0.000002061114,0.000009283158,0.0000157519,0.00000756579],"domain_scores_gemma":[0.9999472,0.00001217233,0.00001202914,0.000003559616,0.0000174964,0.000007476808],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.0001549951,0.00003589776,0.001596266,0.00008816277,0.00002748458,0.0002371397,0.0001828227,0.9180515,0.03644977,0.00854338,0.0004744339,0.03415811],"study_design_scores_gemma":[0.0000105282,0.00007803241,0.0003032078,0.000005582996,0.00000579759,0.00002810906,0.00003312069,0.9971632,0.001316668,0.0004693,0.0005815488,0.000004894629],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.3313352,0.0004310358,0.6494404,0.0002450055,0.00008856223,0.00005694227,0.00003309663,0.0001840554,0.01818574],"genre_scores_gemma":[0.9892805,0.0001123229,0.007912182,0.00002164131,0.000008163306,0.00002841898,0.00001342854,0.00000580796,0.002617585],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.00277329,"threshold_uncertainty_score":0.005514264,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W1974126309","doi":"10.2514/1.28844","title":"Attitude Dynamics of Rigid Bodies in the Vicinity of the Lagrangian Points","year":2008,"lang":"en","type":"article","venue":"Journal of Guidance Control and Dynamics","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":27,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"McGill University","funders":"","keywords":"Lagrangian point; Spacecraft; Libration (molecule); Satellite; Physics; Orbit (dynamics); Rigid body dynamics; Circular orbit; Rigid body; Orbital mechanics; Orbital plane; Dynamics (music); Lyapunov function; Classical mechanics; Three-body problem; Equilibrium point; Point (geometry); Mathematics; Geometry; Aerospace engineering; Astronomy","authors":[{"name":"Brian Wong","is_ca":true},{"name":"Rakesh Patil","is_ca":true},{"name":"Arun K. Misra","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.004922758357298495,"gpt":0.1950360302859722,"spread":0.1901132719286737,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000144317,0.0002041488,0.000332204,0.0003834265,0.0005408185,0.0005435346,0.0004725899,0.0004603474,0.002043578],"category_scores_gemma":[0.0005278033,0.0001923982,0.0003251955,0.0002520375,0.001198049,0.0006366012,0.0008407832,0.0005115201,0.0003845783],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0004563405,"about_ca_system_score_gemma":0.0002918775,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.004416346,"about_ca_topic_score_gemma":0.001781125,"domain_scores_codex":[0.9999111,0.00001276312,0.000002370732,0.00002275598,0.000032105,0.00001894986],"domain_scores_gemma":[0.9998411,0.00003168288,0.00005465973,0.00001399367,0.00002976441,0.00002875425],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.0004319167,0.0001982567,0.0264566,0.0001336178,0.000105353,0.001726359,0.002303166,0.7104109,0.08178172,0.1389111,0.002406806,0.0351342],"study_design_scores_gemma":[0.00003242241,0.0002177245,0.007514345,0.00002183601,0.00001665646,0.0001869648,0.00049167,0.9680663,0.003920393,0.01764001,0.001858156,0.0000335695],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.9160846,0.0003074612,0.06640702,0.0001832539,0.00003573827,0.00002545,0.00005667219,0.0000763002,0.01682364],"genre_scores_gemma":[0.9943331,0.0001715192,0.002325035,0.0000291494,0.00001424222,0.000012135,0.00005245626,0.00001134136,0.003050905],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.004416346,"threshold_uncertainty_score":0.008781254,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W4200346827","doi":"10.1016/j.ast.2021.107285","title":"Multi-impulse smooth trajectory design for long-range rendezvous with an orbiting target using multi-objective non-dominated sorting genetic algorithm","year":2021,"lang":"en","type":"article","venue":"Aerospace Science and Technology","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":26,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"Carleton University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Rendezvous; Trajectory optimization; Control theory (sociology); Trajectory; Orbital maneuver; Impulse (physics); Mathematical optimization; Multi-objective optimization; Pareto principle; Orbit (dynamics); Computer science; Genetic algorithm; Sorting; Range (aeronautics); Mathematics; Algorithm; Optimal control; Engineering; Spacecraft; Physics; Aerospace engineering","authors":[{"name":"Sanaz Samsam","is_ca":true},{"name":"Robin Chhabra","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.01170868923922416,"gpt":0.2382939282950942,"spread":0.22658523905587,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005706325,0.0009775599,0.0009105848,0.0008533302,0.0007106927,0.0007719775,0.0008371514,0.001140831,0.00210809],"category_scores_gemma":[0.001071212,0.000575013,0.0007357982,0.0006511705,0.000575504,0.0004079618,0.0007649343,0.0006796997,0.0002825934],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0008265344,"about_ca_system_score_gemma":0.001877379,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.01431213,"about_ca_topic_score_gemma":0.008093948,"domain_scores_codex":[0.999785,0.00004350327,0.000008981979,0.00003818981,0.00007648893,0.0000478197],"domain_scores_gemma":[0.9996154,0.0001709459,0.00005921739,0.00001642434,0.0001047769,0.00003321399],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.00003430918,0.00001729925,0.0001964832,0.0000310529,0.0000182693,0.00003977533,0.00003757723,0.9860802,0.001451867,0.001220204,0.0002173293,0.01065568],"study_design_scores_gemma":[0.000006740211,0.00002977604,0.00005362489,0.000002411405,0.000003328929,0.000005907489,0.000007916108,0.9993287,0.0001912154,0.0002488186,0.0001192594,0.000002341964],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.04327019,0.000207809,0.9510381,0.0001231714,0.00003990774,0.00007560111,0.00003678612,0.0003337437,0.00487469],"genre_scores_gemma":[0.8545389,0.0001816553,0.1392335,0.0000688439,0.0000201706,0.0003077228,0.0001410789,0.00009118422,0.00541696],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.01431213,"threshold_uncertainty_score":0.0284577,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2092867415","doi":"10.2514/1.54599","title":"Attitude Dynamics and Control of Satellites With Fluid Ring Actuators","year":2012,"lang":"en","type":"article","venue":"Journal of Guidance Control and Dynamics","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":26,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"McGill University","funders":"","keywords":"Actuator; Attitude control; Control theory (sociology); Ring (chemistry); Dynamics (music); Aerospace engineering; Orbital mechanics; Control (management); Computer science; Satellite; Control engineering; Physics; Engineering; Artificial intelligence; Acoustics","authors":[{"name":"Nona Abolfathi Nobari","is_ca":true},{"name":"Arun K. Misra","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.002725814728871983,"gpt":0.1841321516437547,"spread":0.1814063369148828,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001236102,0.0001946332,0.0002410737,0.0001091975,0.0002228201,0.0003818004,0.0002682398,0.0002384994,0.0006479698],"category_scores_gemma":[0.0002280931,0.0001138246,0.0002439145,0.00008671983,0.0003084792,0.000203035,0.0003340648,0.0002106899,0.0001053162],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0001929061,"about_ca_system_score_gemma":0.000275129,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.001872741,"about_ca_topic_score_gemma":0.001160847,"domain_scores_codex":[0.999946,0.00001031075,0.000003587003,0.00001348946,0.00001778098,0.000008824932],"domain_scores_gemma":[0.9999242,0.00001855465,0.0000289465,0.000007099301,0.00001638487,0.00000487866],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.0001912169,0.0000386869,0.00199942,0.000247109,0.00005177176,0.0003045058,0.0003642649,0.7866446,0.1608811,0.01937984,0.0005078154,0.02938953],"study_design_scores_gemma":[0.000009930583,0.000166679,0.0008265265,0.000007441807,0.00001235511,0.00004387555,0.00004653748,0.9905205,0.006208546,0.001044073,0.001106395,0.000007142745],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.6597491,0.0006470851,0.3289759,0.0001666376,0.00006025879,0.00004153935,0.00008010111,0.0002812327,0.009998132],"genre_scores_gemma":[0.9922932,0.0002068099,0.005609579,0.000007293062,0.00000783036,0.00002115817,0.00002080128,0.000004747225,0.001828524],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.001872741,"threshold_uncertainty_score":0.003723621,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2144943890","doi":"10.1109/robot.2002.1014252","title":"First experiment in sun-synchronous exploration","year":2003,"lang":"en","type":"article","venue":"","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":26,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":false,"ca_fund":false,"ca_venue":false,"about_ca":true},"ca_institutions":"","funders":"","keywords":"Terrain; Mars Exploration Program; Sky; Sunlight; Computer science; Meteorology; Solar System; Plan (archaeology); Solar power; Exploration of Mars; Power consumption; Remote sensing; Environmental science; Aerospace engineering; Power (physics); Astrobiology; Geology; Geography; Astronomy; Engineering; Physics","authors":[{"name":"David Wettergreen","is_ca":false},{"name":"Bernardine Dias","is_ca":false},{"name":"Ben Shamah","is_ca":false},{"name":"J. Teza","is_ca":false},{"name":"P. Tompkins","is_ca":false},{"name":"C. Urmson","is_ca":false},{"name":"Michael Wagner","is_ca":false},{"name":"William Whittaker","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.007445368164320524,"gpt":0.1934715793606903,"spread":0.1860262111963698,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007058646,0.0003686713,0.000605578,0.0002562032,0.0007481217,0.0004490041,0.0007863524,0.0006911008,0.00437898],"category_scores_gemma":[0.002526467,0.0002033157,0.0003334237,0.0003158675,0.0007098553,0.001118064,0.001122596,0.0007390488,0.0006588349],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0003802195,"about_ca_system_score_gemma":0.0004595998,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.001638426,"about_ca_topic_score_gemma":0.002375809,"domain_scores_codex":[0.9992259,0.0001813247,0.0000273845,0.0002308949,0.0002037281,0.000130847],"domain_scores_gemma":[0.997891,0.0007425181,0.000115161,0.0004368154,0.0004279938,0.0003865636],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","study_design_scores_codex":[0.009752337,0.005292811,0.0436232,0.0008431586,0.0004084552,0.001596199,0.00783127,0.03341522,0.5891237,0.01380861,0.01405055,0.2802545],"study_design_scores_gemma":[0.002000527,0.04413031,0.08528377,0.0001083368,0.000299186,0.001162343,0.004188087,0.2190471,0.5318307,0.01319057,0.0984714,0.000287701],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.9366266,0.0001268365,0.04792146,0.0002266875,0.0000668119,0.0002607615,0.0004322013,0.002258025,0.01208067],"genre_scores_gemma":[0.9609942,0.00008589193,0.03390106,0.0001092606,0.00001859876,0.0002541704,0.0006357841,0.0001618797,0.003839265],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.00437898,"threshold_uncertainty_score":0.01464915,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W3030101670","doi":"10.2514/1.g004701","title":"Optimal Planar Powered Descent with Independent Thrust and Torque","year":2020,"lang":"en","type":"article","venue":"Journal of Guidance Control and Dynamics","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":26,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":false,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"","funders":"Natural Sciences and Engineering Research Council of Canada; Johnson Space Center","keywords":"Thrust; Descent (aeronautics); Control theory (sociology); Torque; Gradient descent; Generalization; Boundary (topology); Mathematics; Plane (geometry); Computer science; Physics; Mathematical analysis; Aerospace engineering; Geometry; Engineering; Artificial intelligence; Control (management)","authors":[{"name":"Taylor P. Reynolds","is_ca":false},{"name":"Mehran Mesbahi","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.003414521093192666,"gpt":0.1685532184464229,"spread":0.1651386973532302,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003509924,0.0008125419,0.0009272489,0.0003960835,0.0003431204,0.0008945854,0.0004134192,0.001083189,0.001490775],"category_scores_gemma":[0.001442154,0.0003909761,0.0005282022,0.0004159041,0.0006612996,0.0005359795,0.0008254836,0.000535442,0.0002681462],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0005111778,"about_ca_system_score_gemma":0.0006242016,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.002713091,"about_ca_topic_score_gemma":0.001625173,"domain_scores_codex":[0.9998183,0.00005598809,0.000005984389,0.00002930271,0.00004197279,0.00004851922],"domain_scores_gemma":[0.9995403,0.0002573104,0.00006735537,0.00002165187,0.00006578887,0.00004764973],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.00008268179,0.00002179708,0.0003013118,0.00005270718,0.00001688655,0.000167498,0.00003813825,0.9799858,0.002360896,0.007378973,0.0005391945,0.009054078],"study_design_scores_gemma":[0.0000228237,0.00008351072,0.0002162757,0.000008372807,0.000006589357,0.00003350609,0.00003170641,0.9932716,0.0005405411,0.005314379,0.0004628613,0.000007905902],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"methods","genre_scores_codex":[0.2121494,0.0004819867,0.7624364,0.0004867791,0.00006400628,0.00007423889,0.0001720285,0.0002438556,0.02389132],"genre_scores_gemma":[0.9658491,0.0002236019,0.02844959,0.0000620365,0.00002766069,0.00006104886,0.0001495532,0.00005513937,0.005122252],"genre_candidate":"methods","genre_consensus":"methods","teacher_disagreement_score":0.002713091,"threshold_uncertainty_score":0.005394578,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2289501510","doi":"10.1109/tcst.2015.2461593","title":"Lorentz-Augmented Spacecraft Formation Reconfiguration","year":2015,"lang":"en","type":"article","venue":"IEEE Transactions on Control Systems Technology","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":25,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"University of Toronto","funders":"","keywords":"Control reconfiguration; Control theory (sociology); Spacecraft; Linear-quadratic regulator; Thrust; Lorentz force; Lorentz transformation; Aerospace engineering; Computer science; Optimal control; Engineering; Control engineering; Physics; Control (management); Mathematics; Classical mechanics; Magnetic field; Mathematical optimization","authors":[{"name":"Ludwik A. Sobiesiak","is_ca":true},{"name":"Christopher J. Damaren","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.009873918020990148,"gpt":0.1963401603373228,"spread":0.1864662423163327,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001626595,0.0003363175,0.0002887072,0.0001434585,0.0001749325,0.0003590795,0.000285464,0.0002804034,0.001030347],"category_scores_gemma":[0.0003221465,0.0001065483,0.0002909315,0.0001410234,0.0003027586,0.0002579931,0.0005523665,0.0003057608,0.0001833194],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0001814563,"about_ca_system_score_gemma":0.0002920826,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.0008886555,"about_ca_topic_score_gemma":0.0007628967,"domain_scores_codex":[0.9998556,0.00003511453,0.000006902135,0.0000303875,0.00004440937,0.00002748963],"domain_scores_gemma":[0.9998895,0.00002282142,0.00003554786,0.00002045301,0.00001939635,0.00001228956],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"not_applicable","study_design_scores_codex":[0.0002621917,0.00003974143,0.0005033487,0.00008704881,0.00003114445,0.0003893265,0.0001450604,0.8338895,0.05297766,0.01684128,0.0009273756,0.09390644],"study_design_scores_gemma":[0.00003333455,0.0002050357,0.0004586626,0.000003344092,0.00001044815,0.0001042741,0.00002098882,0.9864514,0.006408519,0.003464969,0.002825125,0.0000139258],"study_design_candidate":"not_applicable","study_design_consensus":null,"genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.1368807,0.0003956758,0.8436984,0.0001892547,0.0001428709,0.00004150474,0.00005771052,0.001575953,0.01701789],"genre_scores_gemma":[0.9818131,0.00006612105,0.0154681,0.00003849075,0.00002440772,0.00002282297,0.00003153831,0.0000214285,0.002513954],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.001030347,"threshold_uncertainty_score":0.003446877,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W1776510966","doi":"10.1111/j.1365-2966.2011.19707.x","title":"Aligned major axes in a planetary system without tidal evolution: the 61 Virginis example","year":2011,"lang":"en","type":"article","venue":"Monthly Notices of the Royal Astronomical Society","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":25,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":false,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"","funders":"Natural Sciences and Engineering Research Council of Canada; National Aeronautics and Space Administration","keywords":"Amplitude; Planetary system; Tidal acceleration; Celestial mechanics; Orbital elements; Tidal Waves","authors":[],"retraction":null,"screen_n_in":null,"score":{"opus":0.006586282116182385,"gpt":0.1585831339449581,"spread":0.1519968518287757,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001048606,0.0002148355,0.0002596509,0.0002221771,0.0007405793,0.000530326,0.0002225797,0.0004758849,0.005770097],"category_scores_gemma":[0.0003896834,0.00009408397,0.0002841159,0.0003300328,0.000556228,0.0003381124,0.0006105365,0.0004090269,0.0004806419],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0002500539,"about_ca_system_score_gemma":0.0002412178,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.007293554,"about_ca_topic_score_gemma":0.008994456,"domain_scores_codex":[0.9999125,0.00001476331,0.000004243061,0.000009879948,0.00003610194,0.00002242752],"domain_scores_gemma":[0.9999219,0.00002296513,0.00001138992,0.000009992129,0.00001675893,0.00001684859],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.0005115056,0.0001481863,0.01355602,0.0002885797,0.00007346999,0.005340862,0.001419815,0.174994,0.01079715,0.6836764,0.02411098,0.085083],"study_design_scores_gemma":[0.0004308463,0.0005140999,0.01911013,0.00006728651,0.00005759537,0.002451742,0.001731291,0.5572071,0.003953613,0.2861573,0.1282461,0.00007287281],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.7110888,0.0005980573,0.03733316,0.001821013,0.0002070769,0.00004602461,0.0004756262,0.000242509,0.2481878],"genre_scores_gemma":[0.9730775,0.0002554657,0.00838308,0.00004798613,0.00004019437,0.0000163469,0.000234753,0.0000254328,0.0179192],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.007293554,"threshold_uncertainty_score":0.01930285,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2619351775","doi":"10.1007/s12555-016-0239-8","title":"Almost global finite-time stabilization of spacecraft formation flying with decentralized collision avoidance","year":2017,"lang":"en","type":"article","venue":"International Journal of Control Automation and Systems","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":23,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"York University","funders":"","keywords":"Collision avoidance; Spacecraft; Collision; Control theory (sociology); Scheme (mathematics); Computer science; Lyapunov function; Control (management); Aerospace engineering; Engineering; Physics; Mathematics; Nonlinear system; Mathematical analysis","authors":[{"name":"Daero Lee","is_ca":true},{"name":"George Vukovich","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.00510907167862858,"gpt":0.2256371196377875,"spread":0.2205280479591589,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003104628,0.0003669621,0.0004781013,0.0002081326,0.0003785609,0.0003979617,0.0004253985,0.0003381275,0.000885022],"category_scores_gemma":[0.0009763248,0.0001733128,0.0002847557,0.0001706748,0.0007634382,0.0004027255,0.00117075,0.0004139598,0.00006527345],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0003021804,"about_ca_system_score_gemma":0.0004239455,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.002185141,"about_ca_topic_score_gemma":0.001704134,"domain_scores_codex":[0.9998562,0.00004393758,0.000004495138,0.00002933424,0.00004393859,0.000021967],"domain_scores_gemma":[0.9996865,0.000135096,0.00006827222,0.00003352911,0.00005007159,0.00002655732],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.0001667675,0.00002357762,0.0004072017,0.00004968601,0.00003953242,0.00006310904,0.0001046251,0.9568914,0.007589866,0.0179778,0.0004069125,0.01627949],"study_design_scores_gemma":[0.00001225488,0.00004948307,0.000151566,0.000001908957,0.000003884328,0.000008051477,0.00001018235,0.9951684,0.0003845419,0.004109887,0.00009710497,0.000002675585],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.2324374,0.0001764084,0.7617558,0.0001891707,0.00005779567,0.00002012731,0.00003048925,0.0001373085,0.005195473],"genre_scores_gemma":[0.9946708,0.00002562858,0.004728986,0.00001242812,0.000006939798,0.00001150387,0.00001134422,0.000006099706,0.0005262178],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.002185141,"threshold_uncertainty_score":0.004344881,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2327243740","doi":"10.2514/6.2014-0412","title":"Adjoint-Based Aerodynamic Optimization Framework","year":2014,"lang":"en","type":"article","venue":"52nd Aerospace Sciences Meeting","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":22,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"McGill University","funders":"","keywords":"Aerodynamics; Computer science; Aerospace engineering; Mathematical optimization; Engineering; Mathematics","authors":[{"name":"Francois Bisson","is_ca":true},{"name":"Sivakumaran Nadarajah","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.004581414351579695,"gpt":0.197313672948116,"spread":0.1927322585965363,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008376769,0.0007802909,0.0009756269,0.0006236171,0.0003990291,0.001247437,0.001541899,0.001338769,0.007030226],"category_scores_gemma":[0.001099629,0.0004392578,0.0007296476,0.000433698,0.0006488396,0.0009242288,0.002095193,0.00168377,0.001698498],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0003152117,"about_ca_system_score_gemma":0.001274185,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.001988607,"about_ca_topic_score_gemma":0.002253576,"domain_scores_codex":[0.9995777,0.0001178089,0.00001385337,0.00006070902,0.0001869848,0.00004294138],"domain_scores_gemma":[0.9996688,0.00009338387,0.00002637185,0.00004856437,0.0001261448,0.00003667523],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.0000611467,0.00009307128,0.0002583601,0.0001104235,0.00004500985,0.00009216891,0.00003375576,0.7964258,0.004952583,0.1479776,0.004430023,0.04552007],"study_design_scores_gemma":[0.000005690773,0.00001663011,0.00002551242,0.000003740602,0.000003177558,0.00001260151,0.000003084704,0.9851967,0.0003114515,0.01287392,0.001543517,0.00000402083],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"methods","genre_scores_codex":[0.001576677,0.00009284091,0.9925919,0.00009990686,0.00006007892,0.00001782136,0.00008388629,0.0002749131,0.005201969],"genre_scores_gemma":[0.3992075,0.0004198238,0.5750362,0.0003743689,0.000352679,0.000282296,0.00105457,0.0005253935,0.02274727],"genre_candidate":"methods","genre_consensus":"methods","teacher_disagreement_score":0.007030226,"threshold_uncertainty_score":0.02351844,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W1978279563","doi":"10.1007/s10569-014-9560-9","title":"A novel algorithm for generating libration point orbits about the collinear points","year":2014,"lang":"en","type":"article","venue":"Celestial Mechanics and Dynamical Astronomy","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":21,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"York University","funders":"","keywords":"Libration (molecule); Lagrangian point; Orbit (dynamics); Algorithm; Bisection method; Elliptic orbit; Numerical continuation; Point (geometry); Manifold (fluid mechanics); Computer science; Mathematics; Physics; Geometry; Classical mechanics; Bifurcation; Aerospace engineering","authors":[{"name":"Yuan Ren","is_ca":true},{"name":"Jinjun Shan","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.004900496359055252,"gpt":0.1837326075622271,"spread":0.1788321112031718,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004027794,0.0009130947,0.0007659836,0.0009774365,0.0008261813,0.001105882,0.001517589,0.001152465,0.00704439],"category_scores_gemma":[0.001427983,0.0004638386,0.0005487896,0.001105663,0.0004375108,0.0009008358,0.001444556,0.000979598,0.002095853],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0004831176,"about_ca_system_score_gemma":0.001121228,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.002815618,"about_ca_topic_score_gemma":0.004635083,"domain_scores_codex":[0.9996169,0.00003959808,0.00002461286,0.0001136184,0.000171594,0.00003362344],"domain_scores_gemma":[0.9995672,0.0001207995,0.00003248082,0.00008753753,0.0001611499,0.00003078635],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.00029911,0.0001322091,0.0008567296,0.00016191,0.00007821846,0.0001909234,0.0001341245,0.1304633,0.02290587,0.02684791,0.007124939,0.8108048],"study_design_scores_gemma":[0.0001222215,0.00008102792,0.0002667402,0.00001641933,0.00002341274,0.0001987873,0.00002896486,0.9686793,0.008920692,0.01298459,0.008653782,0.00002394281],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"genre_codex":"methods","genre_gemma":"methods","genre_scores_codex":[0.003023552,0.00003878258,0.9948959,0.00003538203,0.00003983974,0.00004968521,0.00004973646,0.0008178885,0.001049325],"genre_scores_gemma":[0.04528582,0.0000602381,0.9514748,0.00004635383,0.00002888217,0.0001262744,0.0003271342,0.0001569279,0.00249354],"genre_candidate":"methods","genre_consensus":"methods","teacher_disagreement_score":0.00704439,"threshold_uncertainty_score":0.02356589,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2921430369","doi":"10.2514/1.g003528","title":"Experimental Validation of Pseudospectral-Based Optimal Trajectory Planning for Free-Floating Robots","year":2019,"lang":"en","type":"article","venue":"Journal of Guidance Control and Dynamics","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":20,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Carleton University","funders":"","keywords":"Trajectory; Pseudospectral optimal control; Pseudo-spectral method; Computer science; Trajectory optimization; Robot; Control theory (sociology); Gauss pseudospectral method; Simulation; Mathematics; Artificial intelligence; Physics; Control (management); Mathematical analysis","authors":[{"name":"Alexander Crain","is_ca":true},{"name":"Steve Ulrich","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.005037526142161237,"gpt":0.2195165895327492,"spread":0.2144790633905879,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004268059,0.0004049276,0.0001892334,0.0002724887,0.0003221873,0.0002399089,0.000516196,0.0004741828,0.001468102],"category_scores_gemma":[0.001467535,0.0001683875,0.0001523089,0.0001708767,0.0005638362,0.0004885116,0.0004637566,0.0003835058,0.0002378175],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0002589426,"about_ca_system_score_gemma":0.0004986696,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.001095285,"about_ca_topic_score_gemma":0.001334919,"domain_scores_codex":[0.9997749,0.00003873829,0.000009403122,0.00002239521,0.0001299726,0.0000245276],"domain_scores_gemma":[0.9993097,0.0002963218,0.00008110239,0.0001304009,0.0001406344,0.00004175546],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.0006311726,0.0004660471,0.001381109,0.0003655266,0.0000334479,0.0003600792,0.0005092078,0.7386272,0.1884712,0.01152308,0.000955535,0.05667635],"study_design_scores_gemma":[0.00008579942,0.001573558,0.001335111,0.00003158769,0.000008967582,0.00008921405,0.0001526318,0.8819496,0.1096621,0.00256108,0.00252151,0.0000289157],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.7866967,0.0001697153,0.2017362,0.0001781055,0.00007381286,0.000116923,0.0001343815,0.0007953867,0.01009874],"genre_scores_gemma":[0.9727438,0.00004516798,0.02605452,0.00001410424,0.000002466143,0.00005856425,0.00005860185,0.00002882662,0.0009938624],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.001468102,"threshold_uncertainty_score":0.004911244,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W1665030202","doi":"10.1177/0954410015586843","title":"Linearized J2 and atmospheric drag model for satellite relative motion with small eccentricity","year":2015,"lang":"en","type":"article","venue":"Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":20,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"McGill University","funders":"","keywords":"Eccentricity (behavior); Nonlinear system; Drag; Motion (physics); Satellite; Equations of motion; Orbit (dynamics); Physics; Mathematical analysis; Mathematics; Classical mechanics; Mechanics; Aerospace engineering; Engineering; Law","authors":[{"name":"Lu Cao","is_ca":true},{"name":"Arun K. Misra","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.01353594397311979,"gpt":0.1840213842489856,"spread":0.1704854402758658,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001386406,0.000709619,0.0006153376,0.000397955,0.0004035887,0.0006821133,0.0008736865,0.0007751568,0.002489805],"category_scores_gemma":[0.0002915465,0.0002810441,0.0005385369,0.0004521981,0.0004556763,0.000759427,0.0006666004,0.000640324,0.0004975204],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0005379333,"about_ca_system_score_gemma":0.0006895462,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.01343054,"about_ca_topic_score_gemma":0.008244839,"domain_scores_codex":[0.9998993,0.00001506122,0.000003906297,0.00002132669,0.00004250986,0.00001789838],"domain_scores_gemma":[0.9999106,0.0000173826,0.00002635593,0.000006907341,0.00003005183,0.000008758526],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.00003159443,0.00001792593,0.0006222039,0.00007950675,0.00002237481,0.0002167023,0.0001107814,0.9641684,0.006579055,0.02042295,0.001977417,0.005751152],"study_design_scores_gemma":[0.000003775628,0.00001062101,0.0001668559,0.000002152103,0.0000047809,0.00002637801,0.000009169707,0.9977238,0.0002398112,0.001002398,0.0008030019,0.000007239806],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"methods","genre_scores_codex":[0.08739629,0.001310104,0.8597425,0.0006831261,0.000258225,0.00008095169,0.0006615808,0.000808127,0.04905915],"genre_scores_gemma":[0.9406951,0.0009604426,0.01760736,0.0001642829,0.0001100239,0.0001573812,0.0004914259,0.0001215612,0.03969246],"genre_candidate":"methods","genre_consensus":"methods","teacher_disagreement_score":0.01343054,"threshold_uncertainty_score":0.02670473,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W1976633314","doi":"10.1243/09544100jaero405","title":"Satellite formation flying using variable structure model reference adaptive control","year":2009,"lang":"en","type":"article","venue":"Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":20,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Control theory (sociology); Control reconfiguration; Lyapunov function; Adaptive control; Robustness (evolution); Computer science; Variable structure control; State variable; Sliding mode control; Nonlinear system; Control (management); Physics","authors":[{"name":"K. Shahid","is_ca":true},{"name":"Krishna Dev Kumar","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.01055244855555107,"gpt":0.1907868509052983,"spread":0.1802344023497472,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001711607,0.0002272712,0.0002191654,0.0001254157,0.0001891501,0.0003058463,0.0003970059,0.0002845928,0.0007627789],"category_scores_gemma":[0.0003557692,0.00008536563,0.000214804,0.0001360664,0.0002301145,0.0002283862,0.0002391671,0.0003019785,0.000140985],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0001566075,"about_ca_system_score_gemma":0.0002451361,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.002733464,"about_ca_topic_score_gemma":0.002094019,"domain_scores_codex":[0.9999092,0.00001822352,0.000003066621,0.00002050286,0.00003985481,0.000009143077],"domain_scores_gemma":[0.9999162,0.00002262216,0.00002025201,0.00001253852,0.00002397392,0.00000443084],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.00009032509,0.00004822891,0.0006913723,0.0001451066,0.00005566021,0.0001561101,0.0001856326,0.7446725,0.05250522,0.01617523,0.001726675,0.1835479],"study_design_scores_gemma":[0.00001937161,0.0001359164,0.0003060783,0.000007129265,0.00001004476,0.00005126682,0.00001206755,0.9921808,0.003473426,0.00120057,0.002596039,0.00000734629],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.04356783,0.0005772294,0.9499161,0.0001165923,0.00008609646,0.00002653345,0.00001639261,0.0006564547,0.005036879],"genre_scores_gemma":[0.9332533,0.0003224629,0.06348042,0.0000526201,0.00003662962,0.000043777,0.00004406013,0.00001995354,0.002746848],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.002733464,"threshold_uncertainty_score":0.005435109,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null}]}