{"meta":{"page":1,"per_page":50,"max_per_page":100,"total":147,"total_is_capped":false,"direct_labels_cover":0,"predictions_cover":147,"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":"047b61fae346","filters":{"topic":"Aerospace Engineering and Control Systems"}},"results":[{"id":"W3003124108","doi":"10.1155/2020/9689604","title":"Multirotor Sizing Methodology with Flight Time Estimation","year":2020,"lang":"en","type":"article","venue":"Journal of Advanced Transportation","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":61,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":false,"ca_fund":false,"ca_venue":true,"about_ca":false},"ca_institutions":"","funders":"Cranfield University","keywords":"Multirotor; Sizing; Drone; USable; Computer science; Propeller; Software; Process (computing); Set (abstract data type); Simulation; Engineering; Marine engineering","authors":[{"name":"Marcin Biczyski","is_ca":false},{"name":"Rabia Sehab","is_ca":false},{"name":"James F. Whidborne","is_ca":false},{"name":"Guillaume Krebs","is_ca":false},{"name":"P.C.K. Luk","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.01118577428790698,"gpt":0.2164111452757285,"spread":0.2052253709878215,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003977165,0.0007684767,0.0004859461,0.001063133,0.0002583946,0.0006586227,0.0005535429,0.0003248726,0.005121046],"category_scores_gemma":[0.0007527031,0.0003386802,0.0004682335,0.0007245105,0.0002086617,0.0005911283,0.0004243596,0.0004138004,0.001227229],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0003221873,"about_ca_system_score_gemma":0.0006320002,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.001632225,"about_ca_topic_score_gemma":0.001990298,"domain_scores_codex":[0.9995895,0.00005408232,0.00002203055,0.00009437621,0.0002094249,0.00003052284],"domain_scores_gemma":[0.9997009,0.00008190129,0.00006318487,0.00003918739,0.0001063663,0.000008406141],"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":[0.00009092764,0.00005279222,0.0007097147,0.0003736134,0.00004273377,0.0000739393,0.0001224697,0.2214585,0.06974901,0.009392196,0.001714334,0.6962197],"study_design_scores_gemma":[0.00002674357,0.0002572178,0.001198533,0.00003634848,0.0000249182,0.0002392899,0.0000489125,0.9239184,0.04954807,0.003661182,0.02100112,0.0000393383],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"genre_codex":"methods","genre_gemma":"methods","genre_scores_codex":[0.004948216,0.0001307311,0.9922372,0.00001222883,0.00001923334,0.0000463406,0.00003376631,0.0004853377,0.002087002],"genre_scores_gemma":[0.1460813,0.000213551,0.8489281,0.00003168185,0.00002640235,0.0001117279,0.0002194417,0.0003522321,0.00403566],"genre_candidate":"methods","genre_consensus":"methods","teacher_disagreement_score":0.005121046,"threshold_uncertainty_score":0.01713163,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2044593289","doi":"10.2514/1.17311","title":"Elastodynamic Analysis of Aerial Refueling Hose Using Curved Beam Element","year":2006,"lang":"en","type":"article","venue":"AIAA Journal","topic":"Aerospace Engineering and Control Systems","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":"University of Toronto","funders":"","keywords":"Beam (structure); Finite element method; Structural engineering; Mechanics; Physics; Engineering","authors":[{"name":"Zheng Zhu","is_ca":true},{"name":"S. A. Meguid","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.004766953355663021,"gpt":0.1955484426872451,"spread":0.1907814893315821,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002064512,0.0002911302,0.0002490263,0.0002646546,0.0001614274,0.0003439334,0.0004372181,0.0007029524,0.001228248],"category_scores_gemma":[0.0003540488,0.000201927,0.0002901077,0.0001936832,0.0004426052,0.0004058395,0.0003883031,0.0002403716,0.0002601827],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0002607385,"about_ca_system_score_gemma":0.0003644485,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.002545514,"about_ca_topic_score_gemma":0.001722106,"domain_scores_codex":[0.9999102,0.00001962012,0.000003986095,0.00001446262,0.00003961596,0.00001220861],"domain_scores_gemma":[0.9998624,0.00005085083,0.00002347533,0.00001831264,0.00003391093,0.00001091862],"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":[0.00003793151,0.00001904884,0.001369863,0.00002081484,0.0000111119,0.0001322134,0.00008812681,0.9538028,0.03363983,0.003403035,0.0001318249,0.007343334],"study_design_scores_gemma":[0.00000249707,0.00001728987,0.0002583326,0.000001438269,0.000001151508,0.000009661872,0.00001211325,0.9979519,0.001291125,0.0001684692,0.0002824884,0.000003451084],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.3607702,0.0001016472,0.6322091,0.0001357793,0.0000189304,0.00004456952,0.0001036765,0.0002892088,0.006326885],"genre_scores_gemma":[0.9611632,0.00008998611,0.03471994,0.00001723239,0.000004523696,0.00004486492,0.00007313941,0.00003413218,0.003852955],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.002545514,"threshold_uncertainty_score":0.005061448,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2734747191","doi":"10.2514/1.c034271","title":"Aerodynamics Modeling and Analysis of Close Formation Flight","year":2017,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":52,"is_retracted":false,"has_abstract":true,"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","keywords":"Wingspan; Aerodynamics; Vortex; Aerospace engineering; Lift (data mining); Angle of attack; Lift-to-drag ratio; Lift-induced drag; Drag; Mechanics; Computer science; Physics; Control theory (sociology); Engineering","authors":[{"name":"Qingrui Zhang","is_ca":true},{"name":"Hugh H. T. Liu","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.006730311846025809,"gpt":0.2090112796189674,"spread":0.2022809677729416,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001665271,0.0003704405,0.0004240515,0.000287435,0.0004534346,0.0006250589,0.0005985843,0.0005869961,0.001475426],"category_scores_gemma":[0.0003613724,0.0001605771,0.0004982295,0.0001476294,0.0003679892,0.0005746065,0.0006714992,0.0004898959,0.0003577431],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0002739431,"about_ca_system_score_gemma":0.0004245176,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.003106932,"about_ca_topic_score_gemma":0.001106589,"domain_scores_codex":[0.9998699,0.00002103113,0.000003968059,0.0000180504,0.00006940342,0.00001763975],"domain_scores_gemma":[0.9999059,0.00002374069,0.00002003629,0.00001471276,0.00002493077,0.00001069255],"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":[0.00001538387,0.00002504801,0.000651823,0.00002170128,0.000007511915,0.0001241032,0.00005270728,0.9762937,0.005855665,0.007924164,0.000253608,0.008774571],"study_design_scores_gemma":[0.000001930995,0.00001609788,0.0002129303,0.000001403733,0.000001044594,0.00002917149,0.000006751742,0.9983518,0.0002604657,0.0007138093,0.0004020906,0.000002505926],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.114586,0.0003639961,0.8656343,0.0001287791,0.00007143038,0.00007252121,0.0001231406,0.0003610665,0.01865884],"genre_scores_gemma":[0.968731,0.0003139044,0.02331235,0.00004128063,0.00003943179,0.0000795708,0.0001238664,0.00004807682,0.00731061],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.003106932,"threshold_uncertainty_score":0.006177664,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2102270523","doi":"10.1016/j.ijsolstr.2007.05.026","title":"Modeling and simulation of aerial refueling by finite element method","year":2007,"lang":"en","type":"article","venue":"International Journal of Solids and Structures","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":47,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"University of Toronto; York University","funders":"","keywords":"Finite element method; Vortex; Airflow; Wake; Engineering; Tension (geology); Vibration; Instability; Structural engineering; Modal analysis; Flow (mathematics); Point (geometry); Marine engineering; Mechanics; Physics; Acoustics; Aerospace engineering; Mechanical engineering; Classical mechanics","authors":[{"name":"Zheng Zhu","is_ca":true},{"name":"S. A. Meguid","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.007710551281709528,"gpt":0.2706377611994655,"spread":0.262927209917756,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001970824,0.0005294681,0.0008821178,0.00055598,0.0005871117,0.0007462107,0.001304703,0.001656749,0.004590594],"category_scores_gemma":[0.0006458683,0.000537882,0.0005985521,0.00056765,0.0005522391,0.0005534039,0.0004856502,0.0005871377,0.0005472711],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0005333424,"about_ca_system_score_gemma":0.0009112456,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.0221497,"about_ca_topic_score_gemma":0.009179865,"domain_scores_codex":[0.9998555,0.00003021717,0.000008042661,0.00002200464,0.00005469556,0.00002949341],"domain_scores_gemma":[0.999733,0.0001205192,0.00003700024,0.00002676652,0.00005881679,0.00002383222],"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":[0.00001243202,0.00001333299,0.0001889875,0.00001181728,0.000004902579,0.00003240285,0.00001499202,0.996932,0.000806737,0.0005851118,0.0000733164,0.001324033],"study_design_scores_gemma":[0.00000395054,0.000005846315,0.00006143072,0.0000015337,0.000001713998,0.000004986275,0.000006983356,0.9993268,0.0002805657,0.00009869449,0.0002053626,0.000002142583],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.4300617,0.0005636491,0.5138174,0.0004413332,0.0001933994,0.000217287,0.0009817595,0.002059112,0.05166434],"genre_scores_gemma":[0.9598941,0.0002287291,0.03191023,0.00004901041,0.00001165656,0.0001218915,0.0003111982,0.000101147,0.007371989],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.0221497,"threshold_uncertainty_score":0.04404157,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W4398250458","doi":"10.1109/tie.2024.3393153","title":"Finite-Time Control Design for a Coaxial Tilt-Rotor UAV","year":2024,"lang":"en","type":"article","venue":"IEEE Transactions on Industrial Electronics","topic":"Aerospace Engineering and Control Systems","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":"University of Alberta","funders":"National Natural Science Foundation of China","keywords":"Coaxial; Tilt (camera); Rotor (electric); Control theory (sociology); Computer science; Control (management); Engineering; Physics; Automotive engineering; Electrical engineering; Mechanical engineering","authors":[{"name":"Zongyang Lv","is_ca":false},{"name":"Qing Zhao","is_ca":true},{"name":"Xi‐Ming Sun","is_ca":false},{"name":"Yuhu Wu","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.0196884912054535,"gpt":0.2127892002855037,"spread":0.1931007090800502,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004622602,0.0005551825,0.0003865296,0.0002114458,0.000408582,0.0007711719,0.0008392389,0.0007267063,0.001541075],"category_scores_gemma":[0.000791899,0.0002152977,0.0003392512,0.0001497547,0.0005205701,0.0002674193,0.0004561126,0.0006414164,0.0001837984],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0005001337,"about_ca_system_score_gemma":0.000708011,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.005623486,"about_ca_topic_score_gemma":0.003604754,"domain_scores_codex":[0.9997007,0.00004000215,0.00001881517,0.00008741273,0.0001226743,0.00003054968],"domain_scores_gemma":[0.9997117,0.00007649426,0.0000694358,0.00001660754,0.0001092582,0.00001639444],"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":[0.000275724,0.00008751963,0.0006671983,0.0003163622,0.00005864828,0.0003357531,0.000226545,0.8580346,0.07665851,0.007042675,0.0008695418,0.05542696],"study_design_scores_gemma":[0.00001690165,0.0002046173,0.0002007349,0.000007004639,0.0000113265,0.00002085503,0.000009848231,0.9959215,0.002896179,0.0001708672,0.0005344575,0.000005676772],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.04974411,0.0003888851,0.9434764,0.0001898795,0.0001846958,0.00007552079,0.00002617896,0.0002710783,0.00564315],"genre_scores_gemma":[0.9749688,0.0001705571,0.02289974,0.00005272246,0.00003154664,0.0001053017,0.00002844239,0.000009455646,0.001733525],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.005623486,"threshold_uncertainty_score":0.01118153,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W1973397253","doi":"10.2514/1.j052268","title":"Approach to Aerodynamic Design Through Numerical Optimization","year":2013,"lang":"en","type":"article","venue":"AIAA Journal","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":38,"is_retracted":false,"has_abstract":true,"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; Canada Research Chairs","keywords":"Aerodynamics; Airfoil; Transonic; Range (aeronautics); Mathematical optimization; Computer science; Pareto principle; Quadrature (astronomy); Function (biology); Weighting; Engineering; Aerospace engineering; Mathematics","authors":[{"name":"Howard Buckley","is_ca":true},{"name":"David W. Zingg","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.008671107173831748,"gpt":0.1767963969376283,"spread":0.1681252897637966,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.002023414,0.001121593,0.001028587,0.001344068,0.00079061,0.002053361,0.001583714,0.001425105,0.006782488],"category_scores_gemma":[0.002979695,0.0005494564,0.001046475,0.0009027257,0.001705986,0.001266896,0.002092017,0.002184539,0.001696397],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.001095144,"about_ca_system_score_gemma":0.002067981,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.001720062,"about_ca_topic_score_gemma":0.001501658,"domain_scores_codex":[0.9989285,0.0003916423,0.00004104163,0.0000925572,0.0005003886,0.00004585345],"domain_scores_gemma":[0.9991468,0.0004280968,0.00005774758,0.0001149208,0.0002255074,0.0000268718],"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":[0.00001557112,0.0000317395,0.0002006976,0.000218083,0.00003482012,0.00004562627,0.00008760474,0.6464266,0.001802788,0.305411,0.001961841,0.04376368],"study_design_scores_gemma":[0.00002057472,0.00003163486,0.00006355404,0.00006695759,0.000009719624,0.0000363571,0.0000246365,0.8510404,0.0005770769,0.1253446,0.02277136,0.00001308627],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.0005998076,0.0003134106,0.98862,0.0001867171,0.00004078866,0.00004721457,0.00002642727,0.0001017767,0.01006384],"genre_scores_gemma":[0.0773158,0.001701271,0.909846,0.000233409,0.0001556305,0.0008301699,0.0001136388,0.0002119118,0.009592124],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.006782488,"threshold_uncertainty_score":0.0226897,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2319088646","doi":"10.2514/6.2014-0908","title":"High-fidelity Aerodynamic Shape Optimization of Unconventional Aircraft through Axial Deformation","year":2014,"lang":"en","type":"article","venue":"52nd Aerospace Sciences Meeting","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":25,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"University of Toronto","funders":"","keywords":"Aerodynamics; Deformation (meteorology); Aerospace engineering; Computer science; High fidelity; Fidelity; Structural engineering; Geology; Engineering; Acoustics; Physics; Meteorology; Telecommunications","authors":[{"name":"Hugo Gagnon","is_ca":true},{"name":"David W. Zingg","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.007238438151435379,"gpt":0.2043545209908328,"spread":0.1971160828393974,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003477973,0.0005502942,0.0005980828,0.0003029887,0.0003569436,0.0006992202,0.0005940308,0.0009261775,0.001984855],"category_scores_gemma":[0.001146334,0.0003917644,0.0003522099,0.0002581408,0.0005146529,0.0004979828,0.000755483,0.0005923624,0.000270596],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0003913335,"about_ca_system_score_gemma":0.0007144885,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.004643723,"about_ca_topic_score_gemma":0.006308258,"domain_scores_codex":[0.9998554,0.00003475514,0.000006099667,0.0000153826,0.00006364564,0.00002473758],"domain_scores_gemma":[0.9996025,0.0001935312,0.00003972853,0.00005799849,0.00007633885,0.00002998993],"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":[0.00005628833,0.00002972011,0.0005456955,0.00001920854,0.00001044176,0.00005156552,0.00003190169,0.9882314,0.002782421,0.001041692,0.0003061872,0.006893494],"study_design_scores_gemma":[0.000005049184,0.00001189204,0.0001070782,0.000001460138,9.481221e-7,0.000006031032,0.000006439284,0.9992274,0.0003250301,0.0001766922,0.0001301175,0.000001891695],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.6293451,0.0003200411,0.3417064,0.0005042196,0.0001536216,0.00007748579,0.000261789,0.000901351,0.02672993],"genre_scores_gemma":[0.9642354,0.00004510866,0.03340659,0.00004592918,0.00001891825,0.00002922891,0.00010876,0.000124152,0.001985946],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.004643723,"threshold_uncertainty_score":0.009233415,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2171616619","doi":"10.1109/acc.2007.4283054","title":"Control of Large Angle Attitude Maneuvers for Rigid Bodies Using Sum of Squares","year":2007,"lang":"en","type":"article","venue":"Proceedings of the ... American Control Conference/Proceedings of the American Control Conference","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":22,"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":"Quaternion; Rigid body; Rigid body dynamics; Control theory (sociology); Explained sum of squares; Attitude control; Regular polygon; Least-squares function approximation; Representation (politics); Controller (irrigation); Mathematics; Convex optimization; Rotation (mathematics); Computer science; Control (management); Control engineering; Geometry; Engineering; Physics; Artificial intelligence; Classical mechanics","authors":[{"name":"Narendra Gollu","is_ca":true},{"name":"Luís Rodrigues","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.01086407840116157,"gpt":0.2346144416730066,"spread":0.223750363271845,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004715428,0.0009504601,0.0008473006,0.0002416695,0.000296969,0.0006185754,0.0005594362,0.0003942438,0.001166391],"category_scores_gemma":[0.0009329328,0.0003752203,0.0005363603,0.0003157023,0.0007544905,0.0005232582,0.0007899774,0.0007905177,0.0003453987],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0003397313,"about_ca_system_score_gemma":0.0005255886,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.002908235,"about_ca_topic_score_gemma":0.002377283,"domain_scores_codex":[0.9996594,0.000100926,0.00001842586,0.00007899648,0.0001089979,0.00003310931],"domain_scores_gemma":[0.9995716,0.0002055667,0.00009857097,0.00003805635,0.00006821401,0.00001802926],"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":[0.00006474529,0.00002163011,0.0001368715,0.00006369491,0.0000371919,0.00003802062,0.0000692004,0.9528959,0.009709073,0.007106788,0.000384679,0.02947214],"study_design_scores_gemma":[0.000006818138,0.00005423732,0.00005655695,0.000002851489,0.000003747879,0.000008984583,0.000006651811,0.9965522,0.001059503,0.00174824,0.0004959566,0.000004266002],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.009272217,0.00006722743,0.9889309,0.00004414108,0.00001413446,0.00001773065,0.00001085541,0.0001828819,0.001459973],"genre_scores_gemma":[0.8739868,0.0002568873,0.1215045,0.00006925107,0.00004223511,0.0001503284,0.00008186045,0.000108179,0.003799962],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.002908235,"threshold_uncertainty_score":0.005782604,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W4206912236","doi":"10.23952/jnva.6.2022.1.06","title":"Accelerated inertial subgradient extragradient algorithms with non-monotonic step sizes for equilibrium problems and fixed point problems","year":2022,"lang":"en","type":"article","venue":"Journal of Nonlinear and Variational Analysis","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":18,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":false,"ca_fund":false,"ca_venue":true,"about_ca":false},"ca_institutions":"","funders":"","keywords":"Subgradient method; Monotonic function; Inertial frame of reference; Fixed point; Point (geometry); Mathematics; Mathematical optimization; Algorithm; Applied mathematics; Computer science; Mathematical analysis; Physics; Geometry","authors":[{"name":"Bing Tan","is_ca":false},{"name":"Sun Young Cho","is_ca":false},{"name":"Jen‐Chih Yao","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.01012600292941987,"gpt":0.2024008983545651,"spread":0.1922748954251453,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.001517615,0.001547967,0.001315026,0.0008278219,0.0004163186,0.0006410033,0.001511504,0.001019711,0.001686972],"category_scores_gemma":[0.002932915,0.0005571789,0.0009148629,0.0005470057,0.0007544456,0.001367967,0.00108769,0.001782761,0.0004940103],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0006111783,"about_ca_system_score_gemma":0.0009853556,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.002441958,"about_ca_topic_score_gemma":0.002548733,"domain_scores_codex":[0.9994888,0.0002330863,0.00003432343,0.00005018785,0.000154604,0.00003891068],"domain_scores_gemma":[0.9994296,0.0002605387,0.00007482126,0.00005473957,0.0001318902,0.0000483169],"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":[0.0001837665,0.0001232007,0.0006227214,0.0003492924,0.00009359408,0.0002050152,0.0002498054,0.6925644,0.008945199,0.1309483,0.002550794,0.1631639],"study_design_scores_gemma":[0.00001685805,0.00005503237,0.00007145024,0.00001007265,0.000005101157,0.00002169196,0.000006344401,0.9930772,0.0007621719,0.004423633,0.001542942,0.000007521627],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"methods","genre_scores_codex":[0.003894839,0.0002489101,0.9947668,0.00005470953,0.00004139443,0.00003106971,0.000007584284,0.00009398557,0.0008606664],"genre_scores_gemma":[0.2132961,0.0007411574,0.7807878,0.0001255753,0.0001295037,0.0003513672,0.0001058771,0.0001620898,0.004300515],"genre_candidate":"methods","genre_consensus":"methods","teacher_disagreement_score":0.002441958,"threshold_uncertainty_score":0.008026004,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2315634073","doi":"10.2514/6.2016-1788","title":"Design Optimization of Small Rotors in Quad-Rotor Configuration","year":2016,"lang":"en","type":"article","venue":"54th AIAA Aerospace Sciences Meeting","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":13,"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":"Rotor (electric); Computer science; Automotive engineering; Mechanical engineering; Engineering","authors":[{"name":"Tim Carroll","is_ca":true},{"name":"Issi-Rae E. George","is_ca":true},{"name":"Goetz Bramesfeld","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.01699347802154062,"gpt":0.2063176874645376,"spread":0.189324209442997,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004051176,0.0007060173,0.0009220967,0.0004687736,0.0003248357,0.0006595963,0.0004364658,0.000764154,0.003824665],"category_scores_gemma":[0.000941882,0.0005164795,0.0004445783,0.0002830342,0.0003914012,0.000392293,0.0005098165,0.0003031445,0.00048081],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0003538831,"about_ca_system_score_gemma":0.0004355996,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.0009903578,"about_ca_topic_score_gemma":0.001318837,"domain_scores_codex":[0.9998814,0.00004542971,0.000004359482,0.0000199435,0.00003035034,0.0000184258],"domain_scores_gemma":[0.9997014,0.0001616048,0.00004405858,0.00001489504,0.00004766032,0.0000302568],"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":[0.0001364319,0.00004130618,0.0004341392,0.0001147769,0.00002306704,0.00009074487,0.00003437108,0.9736332,0.009150393,0.003424193,0.0006881069,0.01222918],"study_design_scores_gemma":[0.00002474752,0.0001507643,0.0002474805,0.000006640915,0.000008112979,0.00001691082,0.00002374215,0.9973176,0.0006830689,0.0009026598,0.000613619,0.000004635902],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.2325463,0.0008675091,0.7395273,0.0005043957,0.0001516885,0.0001553424,0.0001767114,0.0003596015,0.02571119],"genre_scores_gemma":[0.9420802,0.0002248774,0.05319538,0.0000654143,0.00003103639,0.0001509396,0.0000823864,0.0001116391,0.00405816],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.003824665,"threshold_uncertainty_score":0.01279473,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2513758990","doi":"10.1017/s0263574716000564","title":"Design, analysis and modelling of a hybrid controller for serial robotic manipulators","year":2016,"lang":"en","type":"article","venue":"Robotica","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":13,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"Ontario Tech University; York University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"PID controller; Control theory (sociology); Payload (computing); Convergence (economics); Controller (irrigation); Computer science; Control engineering; Adaptive control; Robotic arm; Engineering; Control (management); Artificial intelligence; Temperature control","authors":[{"name":"Dan Zhang","is_ca":true},{"name":"Bin Wei","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.01955320148407462,"gpt":0.1906958114339816,"spread":0.171142609949907,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004027353,0.0004178406,0.0003838946,0.0003547398,0.000309371,0.0005676903,0.0006564035,0.0005290451,0.002134022],"category_scores_gemma":[0.0004378997,0.0002589794,0.0004638435,0.0001605115,0.0003157351,0.000328946,0.0003327727,0.0003925354,0.0004049084],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0003476259,"about_ca_system_score_gemma":0.0004967014,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.003980638,"about_ca_topic_score_gemma":0.002359823,"domain_scores_codex":[0.9997759,0.00002565757,0.00001263456,0.00004722732,0.0001210003,0.00001757033],"domain_scores_gemma":[0.9997643,0.00005817541,0.00004516882,0.00002529806,0.00009944797,0.000007684689],"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":[0.00009681107,0.0000430518,0.0006399238,0.0001891559,0.00006338238,0.0002324289,0.0001361052,0.875307,0.05786541,0.007403134,0.0007669313,0.05725669],"study_design_scores_gemma":[0.00001258559,0.00008243378,0.0002604045,0.000006677859,0.00001043268,0.00005201389,0.000007194594,0.9931719,0.004168688,0.0005702677,0.001649859,0.000007561062],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.02518191,0.0002292021,0.9682566,0.0000501868,0.00003587715,0.00007109417,0.00003098194,0.0005795051,0.005564759],"genre_scores_gemma":[0.9000713,0.0002049098,0.09162872,0.00003296623,0.00002247683,0.0002368002,0.00007142796,0.00004207254,0.007689288],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.003980638,"threshold_uncertainty_score":0.00791496,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2328727338","doi":"10.2514/6.2016-1385","title":"Autonomous Position Control Analysis of Quadrotor Flight in Urban Wind Gust Conditions","year":2016,"lang":"en","type":"article","venue":"AIAA Guidance, Navigation, and Control Conference","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":12,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Carleton University","funders":"","keywords":"Aeronautics; Aerospace engineering; Position (finance); Aerodynamics; Wind power; Control (management); Computer science; Control theory (sociology); Marine engineering; Engineering; Artificial intelligence; Electrical engineering; Economics","authors":[{"name":"Syed Ali Raza","is_ca":true},{"name":"Jason Etele","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.004189927986307442,"gpt":0.1975653993862881,"spread":0.1933754713999807,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002008321,0.000296397,0.0002728543,0.0002203031,0.0002678978,0.0005114877,0.0002483309,0.0002990077,0.001397761],"category_scores_gemma":[0.0004243469,0.0001587358,0.0002306259,0.0001358517,0.0003666502,0.000240453,0.0002722068,0.0002477194,0.0001065667],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0004044986,"about_ca_system_score_gemma":0.0003541918,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.01536826,"about_ca_topic_score_gemma":0.008513247,"domain_scores_codex":[0.9999357,0.00001231361,0.000001997746,0.0000118657,0.00002059176,0.00001736349],"domain_scores_gemma":[0.9998472,0.00006054404,0.00002982458,0.000009212054,0.00004362946,0.000009616778],"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":[0.0001874642,0.00003304552,0.001632478,0.00004557956,0.00002546848,0.0001968739,0.00007786482,0.9758078,0.009223716,0.004408283,0.0003636672,0.007997784],"study_design_scores_gemma":[0.000002610435,0.00002229567,0.0006505891,6.519089e-7,0.000001650027,0.000006332009,0.000009994603,0.9988901,0.0002213735,0.0001592909,0.00003373777,0.000001322716],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.8369081,0.0004380073,0.1491071,0.0002046345,0.0000527638,0.0000385261,0.00008907292,0.0001106483,0.01305102],"genre_scores_gemma":[0.9986981,0.00002939498,0.0005498271,0.00000557671,0.000003487224,0.000003292023,0.00001235906,0.000005489209,0.0006924174],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.01536826,"threshold_uncertainty_score":0.03055757,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W4252434439","doi":"10.1023/a:1009874504407","title":"The Dynamics of the Swashplate Mechanism of a VTOL Unmanned Aerial Vehicle","year":2001,"lang":"en","type":"article","venue":"Multibody System Dynamics","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":11,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"Bombardier (Canada); McGill University","funders":"McGill University","keywords":"Mechanism (biology); Kinematics; Control theory (sociology); Computer science; Aerospace engineering; Engineering; Control (management); Physics; Classical mechanics","authors":[{"name":"Christian Lange","is_ca":false},{"name":"Jorge Angeles","is_ca":true},{"name":"F. Ranjbaran","is_ca":true},{"name":"G. Goritschnig","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.003168721119888947,"gpt":0.1719290354290318,"spread":0.1687603143091429,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001184715,0.0002445101,0.0002588738,0.0004464058,0.0003627114,0.0005538706,0.0004817429,0.0007782755,0.004628323],"category_scores_gemma":[0.0003568679,0.0002092615,0.0002980363,0.0001525085,0.0006541125,0.0006184935,0.0008042986,0.000326121,0.0004330922],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0001939957,"about_ca_system_score_gemma":0.0002965777,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.002709393,"about_ca_topic_score_gemma":0.00145131,"domain_scores_codex":[0.9999529,0.000007318577,0.000002223143,0.000009377444,0.00001797401,0.00001018396],"domain_scores_gemma":[0.9999084,0.00001407715,0.00003286704,0.000008929073,0.00001368418,0.00002196915],"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":[0.0009316934,0.000170702,0.01309414,0.0002558099,0.0001728529,0.004602561,0.0009048429,0.6501451,0.1500614,0.1249972,0.00241124,0.0522524],"study_design_scores_gemma":[0.00007652029,0.0005142483,0.01091333,0.0000311309,0.00002077047,0.0005268442,0.0003347328,0.9706256,0.003447943,0.0106291,0.00283864,0.00004111667],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.9543437,0.0002459809,0.02829827,0.0002426311,0.0000756087,0.00004048413,0.0001254473,0.0001169778,0.01651083],"genre_scores_gemma":[0.9955907,0.00008104977,0.001007025,0.000009994752,0.000006063303,0.00000605381,0.00002731956,0.000006675309,0.003265274],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.004628323,"threshold_uncertainty_score":0.01548332,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W4404697657","doi":"10.23952/jnva.5.2021.5.12","title":"An inertial algorithm with a self-adaptive step size for a split equilibrium problem and a fixed point problem of an infinite family of strict pseudo-contractions","year":2021,"lang":"en","type":"article","venue":"Journal of Nonlinear and Variational Analysis","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":11,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":false,"ca_fund":false,"ca_venue":true,"about_ca":false},"ca_institutions":"","funders":"National Research Foundation","keywords":"Fixed point; Inertial frame of reference; Mathematics; Algorithm; Mathematical optimization; Point (geometry); Applied mathematics; Computer science; Mathematical analysis; Physics; Geometry; Classical mechanics","authors":[],"retraction":null,"screen_n_in":null,"score":{"opus":0.005351864562655264,"gpt":0.209326395611638,"spread":0.2039745310489827,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.001072375,0.0005662509,0.0007073477,0.0004158603,0.0004955851,0.0005235751,0.001175157,0.001314797,0.001802023],"category_scores_gemma":[0.001978291,0.0002898741,0.0005429762,0.000217154,0.001036233,0.001178812,0.001475165,0.001074563,0.0002440154],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0003332289,"about_ca_system_score_gemma":0.0009144006,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.001038587,"about_ca_topic_score_gemma":0.001050829,"domain_scores_codex":[0.9997202,0.00007855952,0.00002260297,0.00005412303,0.00009787123,0.00002668172],"domain_scores_gemma":[0.9994372,0.0002680937,0.00008048397,0.00005323838,0.0001004572,0.00006055039],"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":[0.0001736913,0.0001659609,0.001651799,0.000270891,0.00006337964,0.0003484379,0.0004297677,0.6765841,0.02369994,0.1792995,0.001202915,0.1161096],"study_design_scores_gemma":[0.00001121444,0.00006597173,0.00005628742,0.000007304002,0.000003518067,0.00003066323,0.00001235294,0.9940102,0.0009660893,0.004340784,0.0004885364,0.000007107552],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":null,"genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.01338863,0.0000576401,0.9855312,0.00006453878,0.0000200059,0.00003281598,0.000003503697,0.0000359565,0.0008657794],"genre_scores_gemma":[0.4317143,0.0001814113,0.5640059,0.00009349213,0.00004687845,0.0003843639,0.00004335697,0.00005788959,0.003472397],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.001802023,"threshold_uncertainty_score":0.006028354,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W4293061206","doi":"10.26467/2079-0619-2022-25-3-51-60","title":"Development of the technical solution to prevent a single-rotor helicopter from entering uncontrolled rotation","year":2022,"lang":"en","type":"article","venue":"Civil Aviation High TECHNOLOGIES","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":10,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Bell Helicopter Textron (Canada)","funders":"","keywords":"Rotor (electric); Pitot tube; Aerospace engineering; Aerodynamics; Rotation (mathematics); Aeronautics; Engineering; Flow (mathematics); Computer science; Physics; Mechanical engineering; Mechanics","authors":[{"name":"Валерий Андреевич Ивчин","is_ca":true},{"name":"K. Y. Samsonov","is_ca":true},{"name":"А. М. Касимов","is_ca":false},{"name":"A. I. Popov","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.007410471862234131,"gpt":0.1787876660305793,"spread":0.1713771941683452,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004795703,0.000851437,0.0005879853,0.001209707,0.0008450272,0.00100894,0.001291557,0.001459096,0.003658621],"category_scores_gemma":[0.0006858099,0.0004245613,0.0005561837,0.0004216924,0.0005170506,0.001548252,0.001000334,0.001153755,0.002767485],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0003364498,"about_ca_system_score_gemma":0.001491438,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.0009466467,"about_ca_topic_score_gemma":0.000761488,"domain_scores_codex":[0.9992853,0.00006034842,0.00004814435,0.0001408964,0.0003760644,0.00008935222],"domain_scores_gemma":[0.9994329,0.0000371258,0.00007854338,0.00006930345,0.0003270863,0.0000551626],"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":[0.0002105396,0.0003241426,0.003768066,0.001491835,0.00007243546,0.001376161,0.0006005762,0.007688431,0.3865123,0.02370411,0.01539079,0.5588606],"study_design_scores_gemma":[0.0001598799,0.003281482,0.01035966,0.0007287147,0.000332711,0.006762924,0.001779604,0.1746991,0.3473238,0.01285825,0.4413765,0.0003374368],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.03535652,0.002921504,0.9313129,0.001730128,0.0009180951,0.0005473725,0.0001008591,0.002332245,0.02478049],"genre_scores_gemma":[0.3637254,0.004786628,0.6000818,0.0009600566,0.0005439098,0.0006340608,0.0004141922,0.0001467017,0.02870729],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.003658621,"threshold_uncertainty_score":0.01223934,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2145685177","doi":"10.2514/6.2010-7927","title":"Investigating Nonlinear Control Architecture Options for Aerial Refueling","year":2010,"lang":"en","type":"article","venue":"AIAA Atmospheric Flight Mechanics Conference","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":10,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Architecture; Computer science; Nonlinear system; Control (management); Artificial intelligence; Physics; Geography; Archaeology","authors":[{"name":"Christopher M. Elliott","is_ca":true},{"name":"Atilla Dogan","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.007067249848769476,"gpt":0.1952424593512914,"spread":0.188175209502522,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004892931,0.0004793669,0.0002391664,0.0001883372,0.0002373153,0.0008034782,0.0005567218,0.0005029186,0.003735567],"category_scores_gemma":[0.0009066258,0.0001635211,0.0002353426,0.0001157609,0.0004890115,0.0008180248,0.0005230139,0.0005130667,0.0003328209],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0004287588,"about_ca_system_score_gemma":0.0004368043,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.003580316,"about_ca_topic_score_gemma":0.005049801,"domain_scores_codex":[0.9998571,0.00003471525,0.000006246096,0.00003169607,0.0000397936,0.00003054782],"domain_scores_gemma":[0.9997541,0.0001002397,0.00004742239,0.00002111184,0.0000663363,0.00001071282],"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":[0.000331175,0.0001815541,0.002540938,0.0006296657,0.00005892496,0.0003994638,0.0003563683,0.8035806,0.04493659,0.03367398,0.0007561275,0.1125547],"study_design_scores_gemma":[0.00004520605,0.0004776478,0.000743953,0.00002688342,0.00002763918,0.00004050722,0.0001935886,0.982265,0.008059008,0.005464661,0.002642058,0.00001380478],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.3825454,0.001944907,0.5635874,0.0007826844,0.0001007309,0.0003133772,0.0001143472,0.0004414593,0.05016959],"genre_scores_gemma":[0.9785196,0.0004893845,0.01463808,0.00005546469,0.0000188287,0.00005414834,0.00003782125,0.00001140194,0.006175295],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.003735567,"threshold_uncertainty_score":0.01249671,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W4404697916","doi":"10.23952/jnva.5.2021.5.10","title":"A simple strong convergent method for solving split common fixed point problems","year":2021,"lang":"en","type":"article","venue":"Journal of Nonlinear and Variational Analysis","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":false,"ca_fund":false,"ca_venue":true,"about_ca":false},"ca_institutions":"","funders":"International Mathematical Union; National Research Foundation","keywords":"Simple (philosophy); Mathematics; Applied mathematics; Point (geometry); Calculus (dental); Mathematical analysis; Computer science; Geometry; Medicine; Philosophy","authors":[],"retraction":null,"screen_n_in":null,"score":{"opus":0.01108033354931072,"gpt":0.2521547480341665,"spread":0.2410744144848558,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.001583767,0.0007825397,0.0009288874,0.0008015815,0.0004310251,0.0005145432,0.00155566,0.001487463,0.002344762],"category_scores_gemma":[0.002233579,0.0003638854,0.0008372954,0.0004803931,0.001198776,0.001133986,0.001790403,0.001551249,0.000532073],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0003751388,"about_ca_system_score_gemma":0.0008591581,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.000788071,"about_ca_topic_score_gemma":0.0008864994,"domain_scores_codex":[0.9995425,0.000149529,0.00002272812,0.00006515619,0.0001931643,0.00002690845],"domain_scores_gemma":[0.9993693,0.0002869753,0.00004996667,0.00006853219,0.0001692979,0.00005603697],"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":[0.000206504,0.000155515,0.0008635856,0.0005388957,0.0001608413,0.0002965968,0.0002652493,0.5978054,0.04640416,0.1884547,0.002713051,0.1621356],"study_design_scores_gemma":[0.00001423621,0.00004956954,0.00003956112,0.000008181334,0.000005615784,0.00003652405,0.000007826999,0.9909038,0.001390279,0.006329916,0.001206796,0.000007747743],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":null,"genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.004355145,0.0001123396,0.9944947,0.00006117502,0.00003625662,0.00003237926,0.000006081957,0.00004227597,0.0008596465],"genre_scores_gemma":[0.1999343,0.0003054352,0.7932885,0.0001562874,0.00008291831,0.0003266115,0.00006719317,0.0000899048,0.005748828],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.002344762,"threshold_uncertainty_score":0.008375883,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W4241864462","doi":"10.23952/jano.3.2021.1.13","title":"Convergence of relaxed inertial methods for equilibrium problems","year":2021,"lang":"en","type":"article","venue":"Journal of Applied and Numerical Optimization","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":false,"ca_fund":false,"ca_venue":true,"about_ca":false},"ca_institutions":"","funders":"National Foundation for Science and Technology Development","keywords":"Convergence (economics); Inertial frame of reference; Applied mathematics; Mathematical economics; Mathematics; Computer science; Economics; Physics; Classical mechanics; Macroeconomics","authors":[{"name":"Ngoc T. Hoang","is_ca":false},{"name":"B. Nguyen Thai","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.007613119653564279,"gpt":0.2363308686665417,"spread":0.2287177490129774,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.002905195,0.001391036,0.001061517,0.001106542,0.0005808386,0.0009791711,0.001566533,0.001288685,0.003653099],"category_scores_gemma":[0.006247946,0.0005379351,0.001058946,0.0004255196,0.001676135,0.001950451,0.003050904,0.001877559,0.0008147967],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.000568781,"about_ca_system_score_gemma":0.001061575,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.001580228,"about_ca_topic_score_gemma":0.0009984329,"domain_scores_codex":[0.9988897,0.0004616251,0.00006533376,0.0001404236,0.000349327,0.00009342668],"domain_scores_gemma":[0.9987028,0.0006888203,0.0001506507,0.0001105261,0.0002474414,0.00009984054],"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":[0.0002433217,0.0001072047,0.0006807424,0.0003796513,0.00008145031,0.0001262553,0.0003227172,0.4969395,0.007289221,0.415322,0.00218469,0.07632325],"study_design_scores_gemma":[0.00002698302,0.0001375858,0.0001187764,0.00002409501,0.000007209097,0.00003139158,0.0000222633,0.9738429,0.001202245,0.02194186,0.002627679,0.00001698733],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":null,"genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.004517928,0.0001505511,0.9930121,0.00007226645,0.0000381922,0.0000374562,0.00001234368,0.00006178777,0.002097322],"genre_scores_gemma":[0.2810183,0.0009579281,0.7053869,0.0002701336,0.0002821337,0.0007714924,0.0002781973,0.0003061423,0.0107288],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.003653099,"threshold_uncertainty_score":0.01536429,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2091931249","doi":"10.1007/s004660050496","title":"Beam analogy for optimal control of linear dynamic systems","year":2000,"lang":"en","type":"article","venue":"Computational Mechanics","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"University of Saskatchewan","funders":"","keywords":"Finite element method; Beam (structure); Mathematics; Analogy; Optimal control; Domain (mathematical analysis); Time domain; Quadratic equation; Differential equation; Partial differential equation; Modal analysis; Mathematical analysis; Applied mathematics; Control theory (sociology); Computer science; Mathematical optimization; Engineering; Control (management); Geometry; Structural engineering","authors":[{"name":"W. Szyszkowski","is_ca":true},{"name":"Inderjit Singh Grewal","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.004532103719470541,"gpt":0.1977459473844904,"spread":0.1932138436650199,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005129253,0.0004330299,0.000893859,0.0004755171,0.0005036506,0.0009507889,0.000761217,0.001336355,0.008340021],"category_scores_gemma":[0.001557116,0.0002960773,0.0005095429,0.0005803502,0.0008288587,0.001602484,0.00118163,0.00163394,0.00104408],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0004203073,"about_ca_system_score_gemma":0.0004108995,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.001363809,"about_ca_topic_score_gemma":0.001048174,"domain_scores_codex":[0.9996924,0.0001320486,0.00001266303,0.00004555543,0.00009311813,0.00002421746],"domain_scores_gemma":[0.9996965,0.0001732162,0.00002533405,0.0000330293,0.00005253064,0.00001932087],"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":[0.00004846188,0.00002754589,0.0000806237,0.00008173348,0.00002016762,0.00004119848,0.00007555183,0.06011873,0.003347744,0.909042,0.003389169,0.02372718],"study_design_scores_gemma":[0.00002869543,0.00005045686,0.00016472,0.00002209917,0.00001371517,0.0000309769,0.00001896048,0.4623698,0.0006040774,0.5245214,0.0121591,0.00001606907],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.007632741,0.001921533,0.962262,0.0009719122,0.0004575868,0.00001990512,0.00004385635,0.000150103,0.0265403],"genre_scores_gemma":[0.7279808,0.004040422,0.2079074,0.001906473,0.001232993,0.0003769742,0.0001662764,0.0003350915,0.05605362],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.008340021,"threshold_uncertainty_score":0.02790016,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2119609257","doi":"10.2514/2.3140","title":"Theoretical Solutions for Finite-Span Wings of Arbitrary Shapes Using Velocity Singularities","year":2003,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":8,"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":"Span (engineering); Gravitational singularity; Finite element method; Angle of attack; Swept wing; Physics; Mechanics; Aerospace engineering; Geometry; Mathematics; Classical mechanics; Aerodynamics; Structural engineering; Mathematical analysis; Engineering","authors":[{"name":"Dan Mateescu","is_ca":true},{"name":"Jean Francois Seytre","is_ca":true},{"name":"A. M. Berhe","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.01500723685481205,"gpt":0.214952600519448,"spread":0.1999453636646359,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005126465,0.0008963614,0.0004380777,0.000619724,0.0005114273,0.0007030034,0.001124095,0.001318729,0.003391899],"category_scores_gemma":[0.001683603,0.0003959621,0.0008846429,0.0002694961,0.001062517,0.001414701,0.0009037081,0.001232365,0.0009376433],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0004511508,"about_ca_system_score_gemma":0.00048755,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.0007279012,"about_ca_topic_score_gemma":0.0007807688,"domain_scores_codex":[0.999833,0.00003749945,0.000006995628,0.00001520868,0.00009093064,0.00001635457],"domain_scores_gemma":[0.9997213,0.0001239916,0.00003382437,0.00003973932,0.00006727241,0.00001382084],"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":[0.00003025592,0.00003638172,0.0004124043,0.0002019562,0.00001641197,0.0002304459,0.0003113867,0.5728275,0.01169536,0.3788484,0.001824543,0.03356494],"study_design_scores_gemma":[0.00001051823,0.00001357322,0.00006124473,0.00002162301,0.000003663239,0.00007248874,0.00003939697,0.9566207,0.001779195,0.03819047,0.003178177,0.000008967778],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":null,"genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.01140462,0.0002523152,0.9803028,0.0001114246,0.00004845376,0.00002484505,0.00002522033,0.0000796106,0.007750732],"genre_scores_gemma":[0.4055812,0.002333453,0.5631043,0.0002039407,0.0002155264,0.0003288259,0.0002563957,0.0003526941,0.02762363],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.003391899,"threshold_uncertainty_score":0.011347,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2586877469","doi":"10.2316/journal.206.2017.1.206-4661","title":"POSITION AND ORIENTATION MEASUREMENT FOR AUTONOMOUS AERIAL REFUELING BASED ON MONOCULAR VISION","year":2017,"lang":"en","type":"article","venue":"International Journal of Robotics and Automation","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":false,"ca_fund":false,"ca_venue":true,"about_ca":false},"ca_institutions":"","funders":"","keywords":"Orientation (vector space); Computer vision; Monocular; Artificial intelligence; Monocular vision; Position (finance); Computer science; Mathematics; Business; Geometry","authors":[{"name":"Wenqi Wu","is_ca":false},{"name":"Xingang Wang","is_ca":false},{"name":"De Xu","is_ca":false},{"name":"Yingjie Yin","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.01097667295266191,"gpt":0.2485451933305891,"spread":0.2375685203779272,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002521531,0.00072487,0.0006439148,0.001237096,0.0003705996,0.0004966316,0.0006452805,0.0005137449,0.000765102],"category_scores_gemma":[0.0007823876,0.0004029624,0.00028627,0.0008987036,0.0003086119,0.001047285,0.000920311,0.0004476153,0.0004528989],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0003813864,"about_ca_system_score_gemma":0.0006587916,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.003173705,"about_ca_topic_score_gemma":0.003725066,"domain_scores_codex":[0.9993989,0.00007528807,0.00001971991,0.0001326397,0.000313808,0.00005956101],"domain_scores_gemma":[0.9996418,0.00003646019,0.00007888616,0.00006398237,0.0001522316,0.00002670855],"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":[0.0003528568,0.00009969123,0.008311122,0.0003529063,0.00008307879,0.0004213448,0.0004673684,0.03836132,0.3578604,0.003466636,0.002516554,0.5877068],"study_design_scores_gemma":[0.00007597772,0.0004791529,0.02843454,0.0000650296,0.00008768901,0.001417998,0.0003524956,0.7899456,0.1667116,0.002873864,0.009367138,0.0001889448],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.1120607,0.0008701294,0.8814428,0.000091799,0.00009814896,0.00005600242,0.000149528,0.001257469,0.003973471],"genre_scores_gemma":[0.8171381,0.0004851738,0.1808136,0.00008926737,0.00003673195,0.00007305453,0.0001943928,0.00004782738,0.001121814],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.003173705,"threshold_uncertainty_score":0.006310463,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W4404312924","doi":"10.4050/jahs.70.012008","title":"Progress in Rotorcraft Design: 1974–2024","year":2024,"lang":"en","type":"article","venue":"Journal of the American Helicopter Society","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Aeronautics; Engineering","authors":[{"name":"Mark W. Scott","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.007261223147982259,"gpt":0.223409904492618,"spread":0.2161486813446357,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.001880582,0.0007376813,0.0001909987,0.001633793,0.0005119191,0.001649866,0.0006837662,0.0008568615,0.01414164],"category_scores_gemma":[0.00176813,0.0003684339,0.0003551627,0.001179481,0.0009282907,0.001150765,0.0009662059,0.0007368003,0.007270789],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.004087328,"about_ca_system_score_gemma":0.002473186,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.004732787,"about_ca_topic_score_gemma":0.005252141,"domain_scores_codex":[0.9985626,0.0002195483,0.0000905074,0.0001459231,0.0008804046,0.000101011],"domain_scores_gemma":[0.9991038,0.0001266475,0.00004485225,0.00009413239,0.0005660956,0.00006440383],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"design_other","study_design_gemma":"not_applicable","study_design_scores_codex":[0.0001242616,0.00004997349,0.001401851,0.0004793254,0.00001854403,0.0001513039,0.0002853951,0.009078847,0.007792308,0.0901656,0.03652829,0.8539243],"study_design_scores_gemma":[0.000009259172,0.0001118875,0.001057971,0.0002146423,0.000005450016,0.0001282384,0.00004975743,0.001998572,0.003594165,0.004285197,0.9885366,0.000008294194],"study_design_candidate":"not_applicable","study_design_consensus":null,"genre_codex":"other","genre_gemma":"review","genre_scores_codex":[0.05325439,0.1356899,0.142783,0.01393832,0.006684987,0.0003229379,0.0008721648,0.0009066067,0.6455477],"genre_scores_gemma":[0.257554,0.1224432,0.157596,0.003273827,0.00208128,0.0002813062,0.002117758,0.0006832191,0.4539695],"genre_candidate":"review","genre_consensus":null,"teacher_disagreement_score":0.01414164,"threshold_uncertainty_score":0.0473085,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W4232971337","doi":"10.13111/2066-8201.2013.5.3.9","title":"Algorithm for the aircraft trajectories considering No Fly Zones for a Flight Management System","year":2013,"lang":"en","type":"article","venue":"INCAS BULLETIN","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"École de Technologie Supérieure","funders":"","keywords":"Computer science; Aerospace engineering; Flight management system; Aeronautics; Fly-by-wire; Real-time computing; Environmental science; Systems engineering; Flight simulator; Simulation; Engineering","authors":[{"name":"Julien Fays","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.005191702439958739,"gpt":0.1740943257986997,"spread":0.168902623358741,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000608427,0.000854962,0.0005956326,0.0005684632,0.0006659454,0.0009225321,0.0007471268,0.0009979655,0.00550721],"category_scores_gemma":[0.00154588,0.0003158416,0.0004882067,0.0003633475,0.0004914601,0.0007347213,0.0008764276,0.001016517,0.0007786019],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.001050441,"about_ca_system_score_gemma":0.002054441,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.006102413,"about_ca_topic_score_gemma":0.005674095,"domain_scores_codex":[0.9997446,0.00006149246,0.0000143304,0.00005978463,0.00007054348,0.00004920865],"domain_scores_gemma":[0.999598,0.0001935575,0.00003924554,0.00002344013,0.0001244831,0.00002127528],"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":[0.0001160708,0.00003790766,0.0006431075,0.00008486004,0.00002712279,0.00006675997,0.000100012,0.9114702,0.001721916,0.01760097,0.00133251,0.06679862],"study_design_scores_gemma":[0.00002899125,0.00003507443,0.00007003859,0.000007633024,0.00000692957,0.00001509882,0.00001759621,0.9954541,0.0003559877,0.003359048,0.0006452794,0.000004201438],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"methods","genre_scores_codex":[0.007793006,0.00007548663,0.9895789,0.00009292579,0.00002708127,0.00006833098,0.00003470486,0.0002063106,0.002123283],"genre_scores_gemma":[0.3908422,0.0001744604,0.6024662,0.0001188401,0.00004790131,0.0005828319,0.0002858195,0.0001198913,0.005361966],"genre_candidate":"methods","genre_consensus":"methods","teacher_disagreement_score":0.006102413,"threshold_uncertainty_score":0.01842344,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2116882460","doi":"10.1109/naecon.2000.894996","title":"Design of a reconfigurable automated landing system for VTOL unmanned air vehicles","year":2002,"lang":"en","type":"article","venue":"","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"Concordia University","funders":"Canadian Aeronautics and Space Institute; Concordia University; Bombardier","keywords":"Controller (irrigation); Computer science; Generator (circuit theory); Global Positioning System; Trajectory; Simulation; Engineering; Telecommunications","authors":[{"name":"Michael Bole","is_ca":true},{"name":"Jiří Svoboda","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.01622794635489284,"gpt":0.1855996858935189,"spread":0.1693717395386261,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001803331,0.0003997857,0.0003221154,0.0003451364,0.000373299,0.0007175746,0.001081041,0.0003782751,0.002831657],"category_scores_gemma":[0.0001959092,0.0002360595,0.0002652806,0.0001234798,0.000197448,0.0002472444,0.0003494816,0.0002984307,0.001226846],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0004255518,"about_ca_system_score_gemma":0.0006391156,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.003086868,"about_ca_topic_score_gemma":0.002253615,"domain_scores_codex":[0.9997944,0.00002190776,0.00001085245,0.00005943129,0.00007383067,0.00003968973],"domain_scores_gemma":[0.9998647,0.00001457582,0.00002366902,0.00001745716,0.00005779497,0.00002170549],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.00082261,0.0002897583,0.006998723,0.0004777567,0.000165786,0.001600193,0.0008125605,0.300714,0.4068123,0.00959173,0.006683137,0.2650315],"study_design_scores_gemma":[0.0001965676,0.001343236,0.005679252,0.0000499153,0.00009363735,0.0005720835,0.000195996,0.8960079,0.06833787,0.001016254,0.0264397,0.0000675325],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.2121408,0.0002149975,0.7573671,0.0002573833,0.0001666229,0.0006145872,0.0001652509,0.008211844,0.02086149],"genre_scores_gemma":[0.8982375,0.00006754545,0.09320837,0.00009155412,0.00002347034,0.0002296424,0.0001166067,0.000101542,0.007923838],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.003086868,"threshold_uncertainty_score":0.009472847,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2569930162","doi":"10.2514/6.2017-1255","title":"Integrator-Augmented Robust Adaptive Control Design for Close Formation Flight","year":2017,"lang":"en","type":"article","venue":"AIAA Guidance, Navigation, and Control Conference","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"University of Toronto","funders":"","keywords":"Integrator; Computer science; Adaptive control; Robust control; Control theory (sociology); Control (management); Control engineering; Control system; Engineering; Artificial intelligence; Telecommunications; Electrical engineering; Bandwidth (computing)","authors":[{"name":"Qingrui Zhang","is_ca":true},{"name":"Hugh H. Liu","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.02058477869521637,"gpt":0.218580434414789,"spread":0.1979956557195726,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007741422,0.000813653,0.0009136935,0.0003147553,0.0004717103,0.001052496,0.0008120261,0.0009956269,0.002298008],"category_scores_gemma":[0.001418785,0.0004897792,0.0004564671,0.0002125478,0.0005456286,0.0006521359,0.001167062,0.0008000009,0.0003753635],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0003969835,"about_ca_system_score_gemma":0.0006866395,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.00465625,"about_ca_topic_score_gemma":0.004513564,"domain_scores_codex":[0.9996985,0.0000748813,0.00001665398,0.00006420857,0.0001081011,0.00003763735],"domain_scores_gemma":[0.9996064,0.0001159449,0.00006547468,0.00002883146,0.0001649061,0.00001848592],"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":[0.0001698215,0.00006273518,0.000434414,0.0001353082,0.00006788254,0.0001346299,0.0002001559,0.9388801,0.007751727,0.01159864,0.0008558698,0.03970865],"study_design_scores_gemma":[0.00001047989,0.00008088213,0.00007544402,0.000003940104,0.000007551769,0.000009784381,0.000006565559,0.9983507,0.0004386018,0.0006570091,0.0003549654,0.000004086738],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.02062682,0.0002203348,0.9749257,0.00008141008,0.00009994739,0.00002749505,0.00001880425,0.000170737,0.003828756],"genre_scores_gemma":[0.9535104,0.0001674943,0.04124358,0.00007173912,0.00004335417,0.0001067881,0.00006628523,0.00003043315,0.004759946],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.00465625,"threshold_uncertainty_score":0.00925833,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2570204968","doi":"10.2514/6.2017-1241","title":"Vertical and Horizontal Flight Reference Trajectory Optimization for a Commercial Aircraft","year":2017,"lang":"en","type":"article","venue":"AIAA Guidance, Navigation, and Control Conference","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Université du Québec","funders":"Oklahoma Agricultural Experiment Station","keywords":"Trajectory; Aerospace engineering; Trajectory optimization; Computer science; Aeronautics; Automotive engineering; Engineering; Physics","authors":[{"name":"Alejandro Murrieta Mendoza","is_ca":true},{"name":"Paul Mugnier","is_ca":true},{"name":"Ruxandra Mihaela Botez","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.01214802760848662,"gpt":0.2247659308979501,"spread":0.2126179032894635,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003383752,0.0004771731,0.0003652909,0.0003233095,0.000353415,0.0004629024,0.0003099648,0.0008911174,0.00204697],"category_scores_gemma":[0.0006639551,0.0002848847,0.000341324,0.000356388,0.0002797559,0.0002762825,0.0003638566,0.0003370997,0.0001825402],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0006835427,"about_ca_system_score_gemma":0.001090281,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.04073384,"about_ca_topic_score_gemma":0.02561791,"domain_scores_codex":[0.9999267,0.00002138514,0.00000272661,0.00001218342,0.0000208386,0.00001609897],"domain_scores_gemma":[0.9998653,0.00005822558,0.00001276519,0.00000746555,0.00004550481,0.00001074205],"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":[0.00007422406,0.00002210571,0.0003367853,0.00002579197,0.00001502624,0.00003924436,0.00002035928,0.987025,0.001215798,0.002163709,0.0005281549,0.008533731],"study_design_scores_gemma":[0.000006552937,0.00002174013,0.0001882976,0.000001452355,0.000002587288,0.000003401201,0.000009278901,0.9992195,0.0001745326,0.0002576933,0.0001133034,0.000001661106],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.5624074,0.0008102995,0.4085866,0.0009360213,0.0000967654,0.0001104376,0.0004963093,0.000390092,0.02616605],"genre_scores_gemma":[0.9573202,0.00009665293,0.03655118,0.00004171629,0.00001670859,0.00004173742,0.0002064141,0.00005345858,0.005671906],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.04073384,"threshold_uncertainty_score":0.08099347,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2810811804","doi":"10.2514/6.2018-3637","title":"A Parametric Study of Multimodality in Aerodynamic Shape Optimization of Wings","year":2018,"lang":"en","type":"article","venue":"","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"University of Toronto","funders":"","keywords":"Aerodynamics; Multimodality; Parametric statistics; Computer science; Aerospace engineering; Engineering; Mathematics","authors":[{"name":"Gregg M. Streuber","is_ca":true},{"name":"David W. Zingg","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.006927930934241019,"gpt":0.2084598730473119,"spread":0.2015319421130709,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006524707,0.000434229,0.0004423171,0.0004078633,0.0003297259,0.0007066143,0.0004336046,0.0007800548,0.001672178],"category_scores_gemma":[0.003337373,0.0003204192,0.0004886411,0.0003058043,0.0008514411,0.0006858769,0.000843698,0.0005678101,0.00009637645],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0002835412,"about_ca_system_score_gemma":0.0002104522,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.0008449398,"about_ca_topic_score_gemma":0.0008048348,"domain_scores_codex":[0.9998488,0.00006764212,0.000003574515,0.00001886795,0.00003055485,0.00003052689],"domain_scores_gemma":[0.9990677,0.0006864959,0.00008693172,0.00004875878,0.00006355482,0.00004646078],"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":[0.000154374,0.00008334919,0.001370208,0.00005935608,0.0000349261,0.000323553,0.0002417458,0.9220585,0.02236121,0.03922135,0.0003229014,0.0137685],"study_design_scores_gemma":[0.000005056459,0.00004863799,0.0004741861,0.000005026702,0.000005009865,0.0000587813,0.00004281527,0.9939778,0.0007706603,0.004383855,0.0002208494,0.000007321806],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.7541304,0.0006700191,0.2241096,0.0005245126,0.00002893799,0.00003872638,0.00003894727,0.00006243987,0.02039632],"genre_scores_gemma":[0.9934422,0.00008219312,0.005156552,0.00002109614,0.00001102653,0.000009395065,0.000007211639,0.00001999124,0.001250394],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.001672178,"threshold_uncertainty_score":0.005594015,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2976956143","doi":"10.18280/mmep.060320","title":"Spherical Storage Tank Development Through Mathematical Modeling of Constituent Sections","year":2019,"lang":"en","type":"article","venue":"Mathematical Modelling and Engineering Problems","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":false,"ca_fund":false,"ca_venue":true,"about_ca":false},"ca_institutions":"","funders":"","keywords":"Development (topology); Petroleum engineering; Computer science; Process engineering; Engineering; Mathematics; Mathematical analysis","authors":[{"name":"Adekunle Taofeek Oyelami","is_ca":false},{"name":"S.O.O. Olusunle","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.0158513572711241,"gpt":0.1824305605311507,"spread":0.1665792032600266,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004046336,0.0005224404,0.0004593484,0.000410572,0.0003885064,0.0008332268,0.001114124,0.0007999555,0.002899928],"category_scores_gemma":[0.0005588974,0.0003561964,0.0009619563,0.0002442728,0.0006492442,0.0006950285,0.0006372061,0.0005925747,0.00071629],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.000829236,"about_ca_system_score_gemma":0.001224618,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.006045816,"about_ca_topic_score_gemma":0.004390598,"domain_scores_codex":[0.9998362,0.0000387236,0.000009056559,0.0000272571,0.00007005255,0.00001865188],"domain_scores_gemma":[0.9997562,0.0000837077,0.00004683903,0.00002292443,0.00007729015,0.0000130251],"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":[0.00001311706,0.000009454009,0.0001491059,0.00003077396,0.000003725523,0.00004335481,0.00004600633,0.9822899,0.003979841,0.01088975,0.0001268452,0.002418126],"study_design_scores_gemma":[0.000003495148,0.00002224277,0.00006694377,0.000004957611,0.000004208308,0.00001826943,0.0000125207,0.9958627,0.001395936,0.00112057,0.001483909,0.000004216797],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.06625625,0.0002156427,0.9052006,0.0001380022,0.00003412444,0.0001188244,0.0002308999,0.0004077364,0.02739794],"genre_scores_gemma":[0.8494459,0.0006339909,0.1265932,0.00004518171,0.0000204446,0.0003688568,0.0002753171,0.0001801796,0.02243689],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.006045816,"threshold_uncertainty_score":0.01202124,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W4402124582","doi":"10.1109/tiv.2024.3453208","title":"Coaxial Tilt-Rotor UAV: Fixed-Time Control, Mixer, and Flight Test","year":2024,"lang":"en","type":"article","venue":"IEEE Transactions on Intelligent Vehicles","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"University of Alberta","funders":"National Natural Science Foundation of China","keywords":"Rotor (electric); Coaxial; Tilt (camera); Flight test; Control theory (sociology); Fixed wing; Aerospace engineering; Computer science; Control (management); Engineering; Electrical engineering; Mechanical engineering; Artificial intelligence","authors":[{"name":"Zongyang Lv","is_ca":true},{"name":"Shengming Li","is_ca":false},{"name":"Yuhu Wu","is_ca":false},{"name":"Xi‐Ming Sun","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.005065517978872086,"gpt":0.1885706563692885,"spread":0.1835051383904164,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000282259,0.0004758271,0.0002431012,0.0002875817,0.000275854,0.000271625,0.0004365818,0.0005579391,0.0008299118],"category_scores_gemma":[0.0003331529,0.00008792841,0.0001729748,0.0001334231,0.0002628746,0.0002424672,0.0002847299,0.0003075765,0.0001460124],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0002027481,"about_ca_system_score_gemma":0.000215723,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.001852149,"about_ca_topic_score_gemma":0.001384457,"domain_scores_codex":[0.9998326,0.00002371712,0.000008906311,0.000025497,0.00007391718,0.00003533897],"domain_scores_gemma":[0.9997851,0.00003871055,0.0000425179,0.00003533157,0.00006294089,0.00003538309],"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":[0.002183128,0.001503782,0.009185927,0.001105056,0.0001205676,0.001281806,0.0006540493,0.2012011,0.6993853,0.005091446,0.00281344,0.07547452],"study_design_scores_gemma":[0.0004019491,0.0127732,0.0176003,0.00006164971,0.00006824118,0.0003739554,0.0003440684,0.6029557,0.3597183,0.0005880736,0.005021061,0.00009351841],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.9555199,0.0003338566,0.03801588,0.000119446,0.0001160272,0.0002302595,0.0001767521,0.0003586271,0.005129253],"genre_scores_gemma":[0.9955696,0.00004877386,0.003466092,0.00001355912,0.000004710024,0.00005083998,0.00005335988,0.000005792202,0.000787165],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.001852149,"threshold_uncertainty_score":0.003682733,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W4391450589","doi":"10.1016/j.cja.2024.01.028","title":"Aerial refueling scheduling of multi-receiver and multi-tanker under spatial-temporal constraints for forest firefighting","year":2024,"lang":"en","type":"article","venue":"Chinese Journal of Aeronautics","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Concordia University","funders":"Key Research and Development Program of Jiangxi Province; National Natural Science Foundation of China","keywords":"Firefighting; Rendezvous; Scheduling (production processes); Fuel efficiency; Computer science; Engineering; Aerospace engineering; Operations management","authors":[{"name":"Jing Huang","is_ca":false},{"name":"Jiaqi XING","is_ca":false},{"name":"Jinrui Ren","is_ca":false},{"name":"Quan Quan","is_ca":false},{"name":"Youmin Zhang","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.01504047619884703,"gpt":0.2528614304404456,"spread":0.2378209542415985,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003833422,0.000739313,0.0007460528,0.0002751726,0.0004012643,0.0006968364,0.0006267635,0.0004944147,0.002235077],"category_scores_gemma":[0.0006003673,0.000275712,0.000624445,0.0003504449,0.0003000339,0.0005213008,0.0006488987,0.000552132,0.0001924512],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0006390181,"about_ca_system_score_gemma":0.001483841,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.01673182,"about_ca_topic_score_gemma":0.01345927,"domain_scores_codex":[0.9997969,0.0000396728,0.00000716352,0.00004628923,0.00004667515,0.00006330197],"domain_scores_gemma":[0.9997953,0.00007823644,0.0000377474,0.00001394554,0.00003977968,0.00003499898],"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":[0.00003725143,0.00001791811,0.0003454943,0.00004993814,0.000009614969,0.00006183438,0.00003161843,0.9870164,0.002406943,0.002130691,0.0004174026,0.007474971],"study_design_scores_gemma":[0.000004490921,0.00001429605,0.00008111378,0.000002233623,0.000003955777,0.000005667704,0.00001296073,0.9990288,0.0002614804,0.0003761803,0.0002066889,0.000002214762],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.1237873,0.0007753667,0.8639978,0.0002470372,0.00008171525,0.00007552879,0.0001335729,0.0002973936,0.01060429],"genre_scores_gemma":[0.9080115,0.0004253144,0.08741296,0.00006391144,0.00002688349,0.00009627019,0.0001486133,0.00006572994,0.003748946],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.01673182,"threshold_uncertainty_score":0.03326887,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W180077639","doi":"10.1007/978-1-4757-3333-4_5","title":"Evaluation of Penalty Functions for Optimal Control","year":2001,"lang":"en","type":"book-chapter","venue":"Applied optimization","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":5,"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; Mashhad University of Medical Sciences","keywords":"Penalty method; Optimal control; Quadratic equation; Function (biology); Mathematical optimization; Mathematics; Bellman equation; State (computer science); Series (stratigraphy); Value (mathematics); Control theory (sociology); Control (management); Computer science; Algorithm; Statistics","authors":[{"name":"Rein Luus","is_ca":true},{"name":"Wichaya Mekarapiruk","is_ca":true},{"name":"C. Storey","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.0137973281288541,"gpt":0.1993677330224825,"spread":0.1855704048936284,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.001035019,0.001342292,0.001334217,0.00076895,0.0003175224,0.001574138,0.001258949,0.0008909696,0.006301452],"category_scores_gemma":[0.002792756,0.0005122488,0.0005213902,0.001014121,0.0009724114,0.001575654,0.001037758,0.001823989,0.00170328],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0007882569,"about_ca_system_score_gemma":0.0006028064,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.0009571339,"about_ca_topic_score_gemma":0.001379497,"domain_scores_codex":[0.9992581,0.0002147824,0.00002492295,0.00006073512,0.0004032951,0.00003811621],"domain_scores_gemma":[0.9993386,0.0003355759,0.00003009562,0.00007100807,0.0001965845,0.00002817054],"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":[0.00007662422,0.00007312014,0.0001448394,0.0004321641,0.00003789959,0.00005449568,0.00007328798,0.2368634,0.004786535,0.4186147,0.02800785,0.3108351],"study_design_scores_gemma":[0.00001038297,0.00003003715,0.0001615038,0.0000806788,0.00001079993,0.00005345848,0.00001403259,0.7925134,0.002979649,0.1756238,0.02850262,0.00001972751],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.002072952,0.003427911,0.9642816,0.0002311078,0.000284003,0.00002020793,0.00005292359,0.0002202432,0.02940906],"genre_scores_gemma":[0.1400822,0.007590178,0.7377907,0.0002097537,0.000554627,0.0002133602,0.0005009801,0.001484407,0.1115738],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.006301452,"threshold_uncertainty_score":0.02108049,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W4285737283","doi":"10.15407/itm2022.02.039","title":"Gas flow in a truncated Laval nozzle with a bell-shaped tip","year":2022,"lang":"en","type":"article","venue":"Technical mechanics","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":false,"ca_fund":false,"ca_venue":false,"about_ca":true},"ca_institutions":"","funders":"","keywords":"Nozzle; Mechanics; Flow (mathematics); Mach number; Discharge coefficient; Rocket engine nozzle; Streamlines, streaklines, and pathlines; Mechanical engineering; Physics; Engineering","authors":[{"name":"O.D. Ihnatiev","is_ca":false},{"name":"N.S. Pryadko","is_ca":false},{"name":"G.O. Strelnikov","is_ca":false},{"name":"K.V. Ternova","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.004847209419835015,"gpt":0.1702826664072432,"spread":0.1654354569874082,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002352448,0.000251348,0.0003732245,0.0002277326,0.0003200108,0.0006026944,0.0004320479,0.0006413394,0.0004147073],"category_scores_gemma":[0.000503708,0.0001350942,0.0003474455,0.0001820009,0.0005505491,0.0004758622,0.0003295241,0.0002484702,0.00008442091],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0005131527,"about_ca_system_score_gemma":0.0005239797,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.001872907,"about_ca_topic_score_gemma":0.0007041331,"domain_scores_codex":[0.9998574,0.00001884663,0.00000732848,0.00003951622,0.00005046024,0.00002648118],"domain_scores_gemma":[0.9998155,0.00007534416,0.00003590726,0.00001468994,0.00004257656,0.00001608172],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.0004081766,0.0001189316,0.00800922,0.0002358932,0.00002250998,0.001407119,0.000331205,0.1535917,0.8115214,0.008936547,0.0002958132,0.01512147],"study_design_scores_gemma":[0.00007407334,0.0009930636,0.005233863,0.00003073294,0.00002071881,0.0006120097,0.000182962,0.7845913,0.2051049,0.001163241,0.001934056,0.00005915912],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.9673468,0.0004325804,0.02942152,0.00006608228,0.00002325514,0.00003105173,0.00007032678,0.0000975901,0.002510761],"genre_scores_gemma":[0.9897434,0.0001686483,0.009186284,0.00001247532,0.000004994821,0.000009231551,0.00007219747,0.000007654888,0.0007950911],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.001872907,"threshold_uncertainty_score":0.003723979,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2314262400","doi":"10.2514/6.2004-4815","title":"Flight Manoeuvre and Spin Characteristics of the Harvard 4: Application to Human Factors Flight Research","year":2004,"lang":"en","type":"article","venue":"AIAA Atmospheric Flight Mechanics Conference and Exhibit","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"National Research Council Canada","funders":"Crohn's and Colitis Foundation of Canada","keywords":"Aileron; Cockpit; Vestibular system; Aeronautics; Wing; Stall (fluid mechanics); Aerospace engineering; Engineering; Physics","authors":[{"name":"Anthony Brown","is_ca":true},{"name":"Jeremy Dillon","is_ca":true},{"name":"Greg Craig","is_ca":true},{"name":"R. Erdos","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.01409716754415507,"gpt":0.2319508158889031,"spread":0.217853648344748,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.001285271,0.0003238271,0.0003544364,0.001499222,0.0005614504,0.0007988171,0.0003768633,0.0005582016,0.00735972],"category_scores_gemma":[0.008321034,0.0001809228,0.0002513138,0.001130829,0.0002550125,0.0006090024,0.0004013253,0.0001976586,0.0008037876],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0003797828,"about_ca_system_score_gemma":0.0004048072,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.009053485,"about_ca_topic_score_gemma":0.01372431,"domain_scores_codex":[0.9997504,0.00008429209,0.00001389917,0.00003675232,0.00009193063,0.00002273321],"domain_scores_gemma":[0.996124,0.002031518,0.0003189615,0.0002029675,0.00101837,0.0003042069],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"observational","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.003423472,0.0004643446,0.5781225,0.0002341407,0.0001063829,0.0005821898,0.001362746,0.02565838,0.04815004,0.002997747,0.006314969,0.3325831],"study_design_scores_gemma":[0.0001245258,0.002144136,0.8815327,0.00003407106,0.00009659403,0.0004166033,0.0008239229,0.09994512,0.01043953,0.001473903,0.002871412,0.00009749992],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.9761646,0.0002283092,0.01337213,0.0001857866,0.00004491167,0.0001165558,0.0007298236,0.000283451,0.008874455],"genre_scores_gemma":[0.9901405,0.00008360948,0.006306882,0.00001769527,0.00002124091,0.00004477616,0.0003677635,0.0000508721,0.002966565],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.009053485,"threshold_uncertainty_score":0.02462071,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W4391531743","doi":"10.28924/2291-8639-22-2024-25","title":"Optimal Quadrature Formula of Hermite Type in the Space of Differentiable Functions","year":2024,"lang":"en","type":"article","venue":"International Journal of Analysis and Applications","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":false,"ca_fund":false,"ca_venue":true,"about_ca":false},"ca_institutions":"","funders":"","keywords":"Mathematics; Quadrature (astronomy); Hermite polynomials; Differentiable function; Type (biology); Space (punctuation); Applied mathematics; Pure mathematics; Mathematical analysis; Calculus (dental); Computer science; Medicine","authors":[{"name":"F.A. Nuraliev","is_ca":false},{"name":"Shaxobiddin Kuziev","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.003167473406211826,"gpt":0.2176435956179057,"spread":0.2144761222116939,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.002523491,0.0004090167,0.0008193811,0.0007862868,0.0003186797,0.001085972,0.0008601299,0.0009505914,0.001174046],"category_scores_gemma":[0.003199795,0.0002710639,0.0005293379,0.0007697491,0.0008581042,0.001728585,0.0006893326,0.001061714,0.000230187],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0007360164,"about_ca_system_score_gemma":0.0008596657,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.0009176295,"about_ca_topic_score_gemma":0.0008589223,"domain_scores_codex":[0.9993431,0.0002042507,0.00003423298,0.00006192446,0.0002986522,0.00005782264],"domain_scores_gemma":[0.9993821,0.0002426494,0.00005211356,0.00004584659,0.0002510738,0.00002620524],"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":[0.00008292583,0.00005388866,0.0008793543,0.0001530421,0.00003109084,0.00009076266,0.0001656842,0.1836438,0.01281321,0.7432248,0.001032051,0.05782944],"study_design_scores_gemma":[0.00001049143,0.00002548756,0.0001152506,0.00001125657,0.000006528933,0.0000410555,0.00001383032,0.9524639,0.001433088,0.04493663,0.0009308979,0.00001153692],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":"theoretical_or_conceptual","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.009979588,0.0002147637,0.9883699,0.00007782612,0.00003648799,0.00001033339,0.00001248082,0.00002174484,0.001276751],"genre_scores_gemma":[0.4352788,0.0008505743,0.5580308,0.0001642125,0.0001403277,0.0001209867,0.0001245479,0.00009028771,0.005199521],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.002523491,"threshold_uncertainty_score":0.01334566,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2910367618","doi":"10.2514/6.2019-0583","title":"Wake Modelling with Embedded Lateral and Directional Stability Sensitivity Analysis for Aerial Refuelling or Formation Flight","year":2019,"lang":"en","type":"article","venue":"AIAA Scitech 2019 Forum","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Royal Military College of Canada","funders":"","keywords":"Wake; Sensitivity (control systems); Aerospace engineering; Stability (learning theory); Computer science; Engineering; Electronic engineering","authors":[{"name":"Luke H. Peristy","is_ca":true},{"name":"Ruben E. Perez","is_ca":true},{"name":"Peter Jansen","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.008000437714739284,"gpt":0.1846302173669959,"spread":0.1766297796522567,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002439887,0.0006739785,0.0004327098,0.0003544233,0.0002289404,0.0005829853,0.0004550434,0.0006240809,0.001683343],"category_scores_gemma":[0.0007084271,0.0004023887,0.000683823,0.0001379576,0.0003314612,0.000614783,0.0007781324,0.000650178,0.0002733117],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0002592025,"about_ca_system_score_gemma":0.0003765043,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.005989331,"about_ca_topic_score_gemma":0.003829974,"domain_scores_codex":[0.9999055,0.00002718456,0.000004682166,0.00001529981,0.00003035906,0.00001695329],"domain_scores_gemma":[0.9997965,0.0001055051,0.00002808648,0.00001797497,0.00004387287,0.000008135742],"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":[0.00001660758,0.00001486087,0.0001264281,0.00001404177,0.00000913122,0.00002286938,0.00001029469,0.9938754,0.002114862,0.001175691,0.00007451225,0.002545244],"study_design_scores_gemma":[7.968014e-7,0.000003883061,0.00003635422,7.9624e-7,9.365086e-7,0.000001231157,0.000001167047,0.9995017,0.0001564897,0.0002562641,0.00003916068,0.000001135604],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.1318079,0.0003156333,0.8569375,0.0001601153,0.00008363299,0.00006264568,0.0001612302,0.0005650729,0.009906209],"genre_scores_gemma":[0.9820733,0.00009962294,0.01398044,0.00002882016,0.00001579187,0.00004269376,0.00009703475,0.00006455793,0.003597729],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.005989331,"threshold_uncertainty_score":0.01190895,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2970037498","doi":"10.2316/j.2019.206-0330","title":"ANALYSIS OF POWER SOURCE OF MULTIROTOR UAVs","year":2019,"lang":"en","type":"article","venue":"International Journal of Robotics and Automation","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":false,"ca_fund":false,"ca_venue":true,"about_ca":false},"ca_institutions":"","funders":"","keywords":"Multirotor; Power (physics); Computer science; Aerospace engineering; Physics; Engineering","authors":[{"name":"Yuehao Yan","is_ca":false},{"name":"Zhiying Lv","is_ca":false},{"name":"Jinbiao Yuan","is_ca":false},{"name":"Jigui Chai","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.002839169172305432,"gpt":0.1971068201416626,"spread":0.1942676509693572,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001226996,0.0005008713,0.0004919706,0.0007709372,0.0004321192,0.0008395503,0.0006676599,0.0007492343,0.008708856],"category_scores_gemma":[0.0004009729,0.0001959523,0.0005395948,0.0005004725,0.0002838401,0.0006842577,0.0003523451,0.0003575515,0.001012196],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0006099813,"about_ca_system_score_gemma":0.0002679466,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.002865173,"about_ca_topic_score_gemma":0.001797378,"domain_scores_codex":[0.999856,0.00001495795,0.000004336821,0.00002758336,0.00007541336,0.00002168992],"domain_scores_gemma":[0.9998823,0.00002775884,0.00001753256,0.000007277701,0.0000572245,0.000007911826],"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":[0.0003020632,0.0001103266,0.004878059,0.0007193768,0.0001341796,0.00191081,0.0002695779,0.7416029,0.06710671,0.07811282,0.007820741,0.09703242],"study_design_scores_gemma":[0.00001220061,0.00008477394,0.001680047,0.00002729415,0.00001980251,0.0002375985,0.00009131968,0.9830595,0.003469519,0.006022084,0.00528389,0.0000119204],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.2091691,0.005215171,0.583334,0.001054043,0.0003250678,0.0002585951,0.0007842915,0.0009888341,0.1988709],"genre_scores_gemma":[0.9761993,0.0008344591,0.005733751,0.00005489628,0.00004281108,0.00005493157,0.0001986683,0.00007864901,0.0168026],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.008708856,"threshold_uncertainty_score":0.02913404,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W1518800580","doi":"10.1109/cdc.2003.1272637","title":"Viability, the solution set, and fixed point approximation of hybrid systems","year":2004,"lang":"en","type":"article","venue":"","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Queen's University","funders":"","keywords":"Kernel (algebra); Computer science; Constraint (computer-aided design); Algorithm; Mathematical optimization; Set (abstract data type); Sampling (signal processing); Hybrid algorithm (constraint satisfaction); Mathematics; Artificial intelligence; Constraint satisfaction; Discrete mathematics; Local consistency; Telecommunications","authors":[{"name":"G. Labinaz","is_ca":true},{"name":"Martin Guay","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.006207430773789745,"gpt":0.1736948027493661,"spread":0.1674873719755764,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00144441,0.0006370471,0.0006670604,0.0007046998,0.0006241109,0.001263256,0.000847825,0.0009495332,0.001270811],"category_scores_gemma":[0.006170995,0.0003171158,0.0006137921,0.0004164338,0.002014935,0.001553217,0.001480147,0.001629946,0.0002037108],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0009707763,"about_ca_system_score_gemma":0.0007989141,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.001957376,"about_ca_topic_score_gemma":0.0007588157,"domain_scores_codex":[0.9993198,0.0002845933,0.00002531741,0.00008522392,0.0002230544,0.00006198316],"domain_scores_gemma":[0.9977871,0.001608762,0.0001289374,0.0001240293,0.0002845181,0.0000665711],"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":[0.0000950962,0.00003129985,0.0006950301,0.00009067093,0.00003260485,0.0001260952,0.0003080343,0.4148498,0.005678159,0.5234486,0.0005658558,0.05407877],"study_design_scores_gemma":[0.00001193916,0.0000639948,0.0001065427,0.00001677784,0.000006598929,0.00004209885,0.00004091849,0.8739967,0.002437378,0.1217431,0.001521198,0.00001275905],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":"theoretical_or_conceptual","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.01362914,0.0001886998,0.9843672,0.000114917,0.00001515287,0.00001775954,0.000008540456,0.00004100381,0.001617543],"genre_scores_gemma":[0.7254016,0.0007041217,0.2692933,0.00007178247,0.00005314135,0.0001864639,0.00007309877,0.00006944296,0.004146948],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.001957376,"threshold_uncertainty_score":0.007638872,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2801427796","doi":"10.1139/tcsme-2016-0075","title":"THE DEVELOPMENT OF TILT-ROTOR UNMANNED AERIAL VEHICLE","year":2016,"lang":"en","type":"article","venue":"Transactions of the Canadian Society for Mechanical Engineering","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":false,"ca_fund":false,"ca_venue":true,"about_ca":false},"ca_institutions":"","funders":"","keywords":"Tilt (camera); Rotor (electric); Aerospace engineering; Automotive engineering; Computer science; Aeronautics; Environmental science; Engineering; Mechanical engineering","authors":[{"name":"Jie-Tong Zou","is_ca":false},{"name":"Pan Zheng-Yan","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.007010622956417679,"gpt":0.1749804432053382,"spread":0.1679698202489205,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001235534,0.0002153203,0.0001471182,0.0002099581,0.0001528485,0.0002133002,0.0002863243,0.0002340167,0.0007482311],"category_scores_gemma":[0.0001680897,0.00009236475,0.000183639,0.0001540499,0.0001591916,0.0004841409,0.0003846907,0.0002574688,0.0002783352],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0001660667,"about_ca_system_score_gemma":0.0003698889,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.001671972,"about_ca_topic_score_gemma":0.0009360228,"domain_scores_codex":[0.999895,0.0000108035,0.00000517817,0.0000230818,0.00005374751,0.00001225968],"domain_scores_gemma":[0.9999245,0.000004264612,0.000007708521,0.000007220171,0.00004657132,0.000009665196],"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":[0.00008861017,0.00005388664,0.00837538,0.000652484,0.00004393877,0.000511952,0.0003412334,0.06693225,0.1828216,0.06549076,0.006582497,0.6681055],"study_design_scores_gemma":[0.00007755747,0.001757728,0.01677071,0.000183937,0.00008755043,0.001814244,0.0004711353,0.6267507,0.08181525,0.01471092,0.2554436,0.0001168256],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.1717979,0.01099767,0.7763638,0.0007891332,0.0007408796,0.0002211321,0.0001626752,0.0007833858,0.03814343],"genre_scores_gemma":[0.7996106,0.007993436,0.1751642,0.0002179569,0.0001163176,0.000101752,0.0003610782,0.00003108884,0.01640371],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.001671972,"threshold_uncertainty_score":0.003324449,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2122534094","doi":"10.5194/isprsarchives-xxxix-b1-453-2012","title":"COMPARISON AND ANALYSIS OF NONLINEAR LEAST SQUARES METHODS FOR VISION BASED NAVIGATION (VBN) ALGORITHMS","year":2012,"lang":"en","type":"article","venue":"˜The œinternational archives of the photogrammetry, remote sensing and spatial information sciences/International archives of the photogrammetry, remote sensing and spatial information sciences","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"University of Calgary","funders":"Natural Sciences and Engineering Research Council of Canada; Canada Research Chairs","keywords":"Algorithm; Levenberg–Marquardt algorithm; Collinearity; Least-squares function approximation; Rotation (mathematics); Computer science; Non-linear least squares; Linear least squares; Transformation (genetics); Convergence (economics); Conjugate gradient method; Computer vision; Mathematics; Artificial intelligence; Estimation theory; Singular value decomposition; Geometry","authors":[{"name":"Bassem Sheta","is_ca":true},{"name":"Mohamed Elhabiby","is_ca":true},{"name":"N. Sheimy","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.01887748219527969,"gpt":0.3057569392994908,"spread":0.2868794571042111,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00295116,0.0007972942,0.0007333241,0.0008914474,0.0004420065,0.0008600148,0.0008531461,0.0007226194,0.002274269],"category_scores_gemma":[0.01053194,0.0003115174,0.0006325669,0.0008906943,0.0004961778,0.001132592,0.0009509709,0.0007771564,0.0006818599],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0007881769,"about_ca_system_score_gemma":0.00116851,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.007103003,"about_ca_topic_score_gemma":0.004961621,"domain_scores_codex":[0.9985606,0.0006107551,0.00006802269,0.0001618247,0.0005445565,0.00005420015],"domain_scores_gemma":[0.9950176,0.003062002,0.000252971,0.000201162,0.001417352,0.00004896346],"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":[0.0002692306,0.0000890068,0.001905975,0.0003729863,0.000121514,0.00004958228,0.0001482296,0.5858346,0.005126958,0.009885311,0.001440762,0.3947559],"study_design_scores_gemma":[0.000006345394,0.0000355293,0.00034597,0.00001021858,0.000007924054,0.0000193489,0.00001676433,0.9968575,0.0009176428,0.001135158,0.0006410748,0.000006509606],"study_design_candidate":"not_applicable","study_design_consensus":null,"genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.008260996,0.000573026,0.9897176,0.00007886517,0.00004053005,0.00003247844,0.00001806112,0.0002287013,0.001049786],"genre_scores_gemma":[0.2691357,0.0009673811,0.7250569,0.00009929546,0.00006874336,0.0001883003,0.0002046152,0.0002747784,0.004004186],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.007103003,"threshold_uncertainty_score":0.01560742,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2314359732","doi":"10.2514/6.2009-3961","title":"Static and Dynamic Pitch Stability of Outboard-Horizontal-Stabilizer Aircraft","year":2009,"lang":"en","type":"article","venue":"","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"University of Calgary","funders":"","keywords":"Stabilizer (aeronautics); Control theory (sociology); Longitudinal static stability; Stability (learning theory); Pitch control; Computer science; Aerodynamics; Aerospace engineering; Engineering; Control (management)","authors":[{"name":"J. A. C. KentŽfield","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.003900176688229259,"gpt":0.1855117978396438,"spread":0.1816116211514145,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000172216,0.0003255485,0.000270491,0.0004674568,0.0004100097,0.0005620267,0.0001800222,0.0002033919,0.002188057],"category_scores_gemma":[0.0005770515,0.0001301827,0.0001428298,0.00013138,0.0003877285,0.000294657,0.0003857542,0.0001755019,0.0002091653],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.000221379,"about_ca_system_score_gemma":0.0002078427,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.003117525,"about_ca_topic_score_gemma":0.002249175,"domain_scores_codex":[0.9999388,0.00001112181,0.000003044768,0.00001123414,0.00001701848,0.00001867596],"domain_scores_gemma":[0.9997744,0.00007292863,0.00004000804,0.00001582238,0.00007102372,0.00002579502],"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":[0.003297505,0.0002298025,0.03196363,0.0001690165,0.0001921899,0.001559709,0.0006666663,0.6981719,0.1725689,0.03583289,0.002302679,0.05304519],"study_design_scores_gemma":[0.00005162336,0.0002472681,0.02065932,0.00001003233,0.00002122558,0.000107881,0.0002123612,0.9614697,0.01124058,0.005575858,0.0003855488,0.00001854291],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.9860578,0.0001299385,0.008587426,0.00004271114,0.0000214143,0.000005713232,0.00008744046,0.00003402255,0.005033473],"genre_scores_gemma":[0.9990326,0.00002201937,0.0001136223,0.000002182443,0.000005220263,0.000001286457,0.0000347551,0.000003024551,0.0007852654],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.003117525,"threshold_uncertainty_score":0.007319808,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W4396799773","doi":"10.1061/jaeeez.aseng-5416","title":"Finite-Time Guidance and Control for Uncrewed Receiver Aircraft in Aerial Refueling Rendezvous","year":2024,"lang":"en","type":"article","venue":"Journal of Aerospace Engineering","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":4,"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":"Rendezvous; Aerospace engineering; Aeronautics; Automotive engineering; Engineering; Control (management); Environmental science; Computer science; Marine engineering; Control theory (sociology); Spacecraft","authors":[{"name":"Wenbi Zhao","is_ca":false},{"name":"Yaohong Qu","is_ca":false},{"name":"Ziquan Yu","is_ca":false},{"name":"Youmin Zhang","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.003906425231099761,"gpt":0.1891917823866736,"spread":0.1852853571555738,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000307093,0.0004408844,0.0004034665,0.0001775273,0.0003130859,0.0005886396,0.000627415,0.0005432799,0.0005330747],"category_scores_gemma":[0.0005498577,0.0001873374,0.0003369507,0.0001414254,0.0006847343,0.0004675239,0.0006600734,0.0005193974,0.00007502895],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.000418489,"about_ca_system_score_gemma":0.0005439591,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.00706517,"about_ca_topic_score_gemma":0.003684104,"domain_scores_codex":[0.9997558,0.00003592354,0.00001128863,0.00007615494,0.00008939651,0.00003143519],"domain_scores_gemma":[0.9998184,0.00005824562,0.0000524693,0.00001487841,0.00004353427,0.00001257528],"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":[0.0001424024,0.00003007227,0.0009577593,0.0001608543,0.0000350936,0.0003291502,0.00031049,0.9234267,0.03153351,0.01109134,0.0003192624,0.03166335],"study_design_scores_gemma":[0.00001195929,0.00008898154,0.0002615652,0.00000508859,0.000007981295,0.00002686363,0.00002758316,0.9961919,0.002063291,0.0008184332,0.0004901033,0.000006267052],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.1070865,0.0004484557,0.8889928,0.0001133868,0.00004346787,0.00002320293,0.0000175819,0.0001386052,0.003136069],"genre_scores_gemma":[0.9840186,0.0001570814,0.01400403,0.00001810483,0.00001210148,0.00002951444,0.00002640596,0.000006789059,0.001727413],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.00706517,"threshold_uncertainty_score":0.0140481,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W4398222327","doi":"10.1007/s11071-024-09693-7","title":"Fractional-order super-twisting sliding mode attitude control for elastic refueling boom with exogenous disturbances","year":2024,"lang":"en","type":"article","venue":"Nonlinear Dynamics","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"Concordia University","funders":"Aeronautical Science Foundation of China; Natural Sciences and Engineering Research Council of Canada; National Natural Science Foundation of China","keywords":"Boom; Control theory (sociology); Order (exchange); Mode (computer interface); Sliding mode control; Control (management); Structural engineering; Computer science; Engineering; Economics; Physics; Nonlinear system; Finance; Artificial intelligence","authors":[{"name":"Wenbi Zhao","is_ca":false},{"name":"Yaohong Qu","is_ca":false},{"name":"Ziquan Yu","is_ca":false},{"name":"Youmin Zhang","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.005367800518172754,"gpt":0.2162783118203346,"spread":0.2109105113021618,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002434182,0.00044739,0.0005434101,0.0002124263,0.0004456468,0.0004468675,0.0004152709,0.0003317141,0.001205141],"category_scores_gemma":[0.0003532438,0.0001419907,0.0003604434,0.0002152973,0.0003995963,0.0003489882,0.0004071735,0.0003601623,0.00008755917],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0002468814,"about_ca_system_score_gemma":0.0002594361,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.003699828,"about_ca_topic_score_gemma":0.002994974,"domain_scores_codex":[0.9999106,0.0000133212,0.000005395118,0.00002009172,0.00002448508,0.00002623876],"domain_scores_gemma":[0.9998734,0.00003316975,0.00002714403,0.00001547322,0.00004012021,0.00001057947],"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":[0.0007539658,0.00009387994,0.001300556,0.0003484785,0.00009118093,0.0004531772,0.0002976106,0.8175614,0.06864765,0.01473279,0.001207351,0.09451196],"study_design_scores_gemma":[0.000006769415,0.00009952487,0.0003117608,0.000003589843,0.00000722676,0.00001344324,0.00001059096,0.9973212,0.001189329,0.0007872799,0.0002450555,0.000004208106],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.2401049,0.0004444368,0.7506431,0.0001577876,0.0002511716,0.00002623695,0.00003623795,0.0002139227,0.008122275],"genre_scores_gemma":[0.9952797,0.00007566865,0.003562586,0.00001331151,0.00001384795,0.00000850074,0.00001301098,0.000003728525,0.001029635],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.003699828,"threshold_uncertainty_score":0.007356584,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W4400005519","doi":"10.18280/jesa.570323","title":"Design, Modeling, and Control of Tiltable Tri-Rotors UAV","year":2024,"lang":"fr","type":"article","venue":"Journal Européen des Systèmes Automatisés","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":false,"ca_fund":false,"ca_venue":true,"about_ca":false},"ca_institutions":"","funders":"","keywords":"Control (management); Computer science; Engineering; Artificial intelligence","authors":[{"name":"Abdullah Mohammed Yahia","is_ca":false},{"name":"Ahmed Alkamachi","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.01494235508452398,"gpt":0.2220491696659961,"spread":0.2071068145814721,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002138951,0.0007491711,0.0006432002,0.0003375322,0.0004147795,0.0009439987,0.0008770486,0.0006869579,0.001361375],"category_scores_gemma":[0.0002009856,0.0003395756,0.0006124796,0.0002435438,0.0004547728,0.0003854069,0.0006529235,0.0006246447,0.0005773228],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0004141513,"about_ca_system_score_gemma":0.0006723528,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.004872376,"about_ca_topic_score_gemma":0.003055421,"domain_scores_codex":[0.999823,0.00002453929,0.00001106809,0.00004170625,0.00007365203,0.00002596188],"domain_scores_gemma":[0.9999051,0.00001001418,0.00003853536,0.00001117659,0.00002742921,0.000007766142],"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":[0.00008583106,0.00003774775,0.0008483106,0.000212158,0.00003993152,0.0004729865,0.0001481477,0.9239841,0.04365197,0.007831641,0.0007180008,0.02196924],"study_design_scores_gemma":[0.00001503287,0.0001611802,0.0005140737,0.00001236184,0.00001502244,0.0001060412,0.00002620137,0.9934366,0.002709324,0.0006812969,0.002312365,0.00001046605],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.04324492,0.001090618,0.9384161,0.0002181264,0.0001175599,0.0001593203,0.0001487404,0.0005360327,0.01606861],"genre_scores_gemma":[0.937573,0.001123243,0.05309812,0.00006244717,0.00004491279,0.0003659941,0.0001606407,0.00004920817,0.007522538],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.004872376,"threshold_uncertainty_score":0.00968802,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W1967127150","doi":"10.4236/wjm.2013.32010","title":"Development of Analytical Model for Modular Tank Vehicle Carrying Liquid Cargo","year":2013,"lang":"en","type":"article","venue":"World Journal of Mechanics","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Université Laval; Université du Québec à Chicoutimi","funders":"","keywords":"Slosh dynamics; Modular design; Engineering; Fuel tank; Vehicle dynamics; Automotive engineering; Computer science; Marine engineering; Simulation; Mechanical engineering; Aerospace engineering","authors":[{"name":"M. Toumi","is_ca":true},{"name":"Mohamed Bouazara","is_ca":true},{"name":"Marc J. Richard","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.01381196012921934,"gpt":0.2073648673885076,"spread":0.1935529072592883,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000176033,0.0005492116,0.0005905227,0.0005058766,0.0005152205,0.0006373971,0.001194717,0.0009560739,0.002846325],"category_scores_gemma":[0.0002996263,0.0003427112,0.0008192218,0.0003105353,0.0003286645,0.0006029647,0.0005432249,0.0005438762,0.0007630108],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0005809615,"about_ca_system_score_gemma":0.0009138702,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.008649901,"about_ca_topic_score_gemma":0.004237772,"domain_scores_codex":[0.9998934,0.00001970868,0.000005203428,0.00001944743,0.00004342462,0.00001874906],"domain_scores_gemma":[0.9999055,0.0000204791,0.00001511758,0.000006947002,0.00004641144,0.000005609033],"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":[0.00001956585,0.00001484331,0.0003815831,0.00008658402,0.00001109087,0.0002357095,0.00009038344,0.973251,0.006873748,0.01105095,0.0005829328,0.007401673],"study_design_scores_gemma":[0.000004543072,0.00002048834,0.00008376338,0.000009682113,0.000005396205,0.00004174227,0.00002164198,0.9954495,0.0007884996,0.001684195,0.001884335,0.000006189589],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"methods","genre_scores_codex":[0.04723765,0.0006545913,0.9273834,0.0002033961,0.00008679037,0.0001252618,0.000430378,0.0007040551,0.02317458],"genre_scores_gemma":[0.8820065,0.001432033,0.089686,0.00006967822,0.00006796832,0.0005157059,0.0005709648,0.0001392091,0.02551209],"genre_candidate":"methods","genre_consensus":"methods","teacher_disagreement_score":0.008649901,"threshold_uncertainty_score":0.0171991,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W1974254889","doi":"10.1115/imece2008-67103","title":"Dynamic Stability Analysis of Aerial Refueling Hose/Drogue System by Finite Element Method","year":2008,"lang":"en","type":"article","venue":"","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"University of Toronto; York University","funders":"","keywords":"Finite element method; Vortex; Wake; Instability; Airflow; Point (geometry); Tension (geology); Vibration; Stability (learning theory); Engineering; Structural engineering; Flow (mathematics); Aerospace engineering; Mechanics; Marine engineering; Physics; Acoustics; Computer science; Mechanical engineering; Classical mechanics; Mathematics","authors":[{"name":"Zheng Zhu","is_ca":true},{"name":"S. A. Meguid","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.007489199914806762,"gpt":0.2112618393934906,"spread":0.2037726394786839,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002661037,0.0003112965,0.0004661733,0.0003591426,0.0003360824,0.0003238212,0.000449148,0.0006240918,0.002684147],"category_scores_gemma":[0.000577582,0.000227674,0.0004885379,0.0001446276,0.0003855937,0.0003902545,0.0003639785,0.0003473263,0.000332506],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0002950752,"about_ca_system_score_gemma":0.0004768996,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.005051049,"about_ca_topic_score_gemma":0.00267738,"domain_scores_codex":[0.999869,0.00002870973,0.000006342423,0.00001891639,0.00006065251,0.00001641114],"domain_scores_gemma":[0.9997734,0.0001035579,0.00003132167,0.00001644302,0.00006639949,0.000008779719],"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":[0.0000494955,0.0000202436,0.001077435,0.00005337122,0.00001760162,0.00006487851,0.0001139075,0.9625493,0.0205317,0.002848112,0.0001171547,0.0125568],"study_design_scores_gemma":[0.000001842423,0.0000103143,0.0001246023,0.000002403999,0.000001538888,0.000005752405,0.00001020089,0.9986683,0.000857242,0.0001491122,0.0001664575,0.000002214723],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.1993048,0.000190035,0.7936662,0.0001220405,0.00002388533,0.00004760037,0.00007974444,0.0002930048,0.006272643],"genre_scores_gemma":[0.9420187,0.0001523453,0.05335851,0.00002648847,0.000009246219,0.0001122824,0.00007630904,0.00004068437,0.004205409],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.005051049,"threshold_uncertainty_score":0.01004326,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2610528573","doi":"10.1515/scjme-2017-0006","title":"The Investigation of the Cavitation Phenomenon in the Laval Nozzle with Full and Partial Surface Wetting","year":2017,"lang":"en","type":"article","venue":"Strojnícky časopis/Journal of Mechanical Engineering","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":false,"ca_fund":false,"ca_venue":false,"about_ca":true},"ca_institutions":"","funders":"National Supercomputing Centre Singapore; Grantová Agentura České Republiky; Ministerstvo Školství, Mládeže a Tělovýchovy","keywords":"Wetting; Nozzle; Cavitation; Mechanics; Materials science; Flow (mathematics); Mechanical engineering; Composite material; Physics; Engineering","authors":[{"name":"Jana Jablonská","is_ca":false},{"name":"Milada Kozubková","is_ca":false},{"name":"Barbora Zavadilová","is_ca":false},{"name":"Lukáš Zavadil","is_ca":false},{"name":"Simona Fialová","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.006393821328843502,"gpt":0.1867344360984974,"spread":0.1803406147696539,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003525747,0.0001436855,0.0002976538,0.0002146324,0.000162189,0.0002692075,0.000230687,0.0003115307,0.0005133455],"category_scores_gemma":[0.0008930461,0.0001138216,0.0002728153,0.0001641509,0.0004042546,0.0002641812,0.0002418348,0.0002037422,0.00003883478],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0001999589,"about_ca_system_score_gemma":0.0001638173,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.0009231999,"about_ca_topic_score_gemma":0.0003949644,"domain_scores_codex":[0.9997939,0.00003071684,0.000008207683,0.00003530753,0.0000937984,0.00003802534],"domain_scores_gemma":[0.9995321,0.0002318783,0.00008041183,0.00003605367,0.00008742516,0.00003212845],"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":[0.0001913302,0.00002638873,0.004019154,0.00008344142,0.0000228962,0.000542879,0.0001163866,0.01030476,0.9767069,0.0005919454,0.00006632196,0.007327707],"study_design_scores_gemma":[0.00003797767,0.0009084598,0.04737619,0.00001444585,0.00003709328,0.001108567,0.0001172861,0.2312663,0.7174104,0.0003706577,0.001308425,0.00004411965],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.9932505,0.0002015557,0.005910906,0.00001391711,0.000006105874,0.000007886274,0.00001917604,0.00003145819,0.0005584431],"genre_scores_gemma":[0.9988133,0.00004110257,0.0009188848,0.000002520949,0.00000294958,0.000002724109,0.0000160775,0.000004261978,0.000198193],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.0009231999,"threshold_uncertainty_score":0.001864612,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W3204383421","doi":"10.4271/01-15-01-0002","title":"Linearization of Aircraft Landing Equations of Motion with Airframe Flexibility Effects","year":2021,"lang":"en","type":"article","venue":"SAE International Journal of Aerospace","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":3,"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":"Airframe; Flexibility (engineering); Aeronautics; Linearization; Aerospace engineering; Landing gear; Equations of motion; Motion (physics); Computer science; Engineering; Mathematics; Physics; Classical mechanics; Nonlinear system; Artificial intelligence","authors":[{"name":"Terrin Stachiw","is_ca":true},{"name":"Fidel Khouli","is_ca":true},{"name":"Robert Langlois","is_ca":true},{"name":"Fred F. Afagh","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.005858741463946701,"gpt":0.2182005198152002,"spread":0.2123417783512535,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002491354,0.0006101825,0.0003548642,0.0003573258,0.0002767655,0.0007064278,0.000582016,0.0006284111,0.004664496],"category_scores_gemma":[0.000545818,0.0003735999,0.0008304652,0.0002020368,0.0004190756,0.0007459778,0.0008290096,0.0009656014,0.001392364],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0005788358,"about_ca_system_score_gemma":0.0006339457,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.01498282,"about_ca_topic_score_gemma":0.008071358,"domain_scores_codex":[0.9998354,0.00003510314,0.000008551501,0.00002646108,0.00007444741,0.00001997438],"domain_scores_gemma":[0.999823,0.00004990271,0.00003658042,0.00002672419,0.0000570567,0.000006718458],"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":[0.00001953805,0.00002955635,0.0007647147,0.00007875261,0.00001978401,0.0001912529,0.000281555,0.9342995,0.01379839,0.03586144,0.001900982,0.01275449],"study_design_scores_gemma":[0.00000622535,0.00001593115,0.0002730009,0.000009644715,0.000004985307,0.00003220745,0.00003361482,0.99156,0.001698975,0.003683314,0.002671435,0.00001057297],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.06202353,0.0002636339,0.8936737,0.0004559445,0.00009172977,0.000121162,0.000458263,0.0008547053,0.04205727],"genre_scores_gemma":[0.868319,0.0006374343,0.05989265,0.0003515498,0.00005801216,0.0002831444,0.0006263611,0.0003305783,0.06950127],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.01498282,"threshold_uncertainty_score":0.02979124,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W3111079617","doi":"10.18280/ijsse.100503","title":"Safety Analysis and Simulation Validation of Hose Whipping Phenomenon in Air Refueling","year":2020,"lang":"en","type":"article","venue":"International Journal of Safety and Security Engineering","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":false,"ca_fund":false,"ca_venue":true,"about_ca":false},"ca_institutions":"","funders":"National Natural Science Foundation of China","keywords":"Engineering; Swing; Automotive engineering; Simulation; Mechanical engineering","authors":[{"name":"Lijie Cui","is_ca":false},{"name":"Jiping Cong","is_ca":false},{"name":"Hao Chen","is_ca":false},{"name":"Bo Ren","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.005434711199499085,"gpt":0.2058960790646623,"spread":0.2004613678651632,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005878169,0.0005356562,0.0003876486,0.0005524473,0.0004642274,0.0003489156,0.0006328492,0.0005658527,0.001578317],"category_scores_gemma":[0.001107035,0.0001686129,0.0006545965,0.0002202783,0.0003613588,0.0005136739,0.0004090715,0.0004794866,0.0001317447],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0004044498,"about_ca_system_score_gemma":0.0006013119,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.008848309,"about_ca_topic_score_gemma":0.003792665,"domain_scores_codex":[0.9996835,0.0000768413,0.00001853872,0.00004708194,0.0001088006,0.00006520803],"domain_scores_gemma":[0.9993319,0.0002734386,0.00008186981,0.00008023334,0.0002008537,0.00003176864],"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":[0.0001773987,0.0001306853,0.008271789,0.0001548697,0.00003275405,0.0002501055,0.0001766009,0.9677009,0.01251247,0.001675227,0.0003580761,0.008559139],"study_design_scores_gemma":[0.00001475502,0.0001476964,0.001312951,0.000005751415,0.00001347447,0.00001494704,0.00005153291,0.9922106,0.00572324,0.0002288829,0.0002682747,0.000007838173],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.9256774,0.0001542831,0.06731081,0.00009822276,0.00006258436,0.00009557173,0.0002912508,0.0006214641,0.005688378],"genre_scores_gemma":[0.9960639,0.00005285233,0.003142514,0.000005970599,0.000002511374,0.00003488552,0.0001008913,0.00001074231,0.0005857531],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.008848309,"threshold_uncertainty_score":0.01759362,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W4408696783","doi":"10.1109/itsc58415.2024.10919698","title":"Flight Path Optimization with Optimal Control Method","year":2024,"lang":"en","type":"article","venue":"","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"University of British Columbia; University of Toronto","funders":"","keywords":"Path (computing); Computer science; Control (management); Optimal control; Mathematical optimization; Mathematics; Artificial intelligence; Computer network","authors":[{"name":"Gaofeng Su","is_ca":false},{"name":"Xi Cheng","is_ca":false},{"name":"Siyuan Feng","is_ca":false},{"name":"Ke Liu","is_ca":false},{"name":"Jilin Song","is_ca":true},{"name":"Jianan Chen","is_ca":true},{"name":"Chen Zhu","is_ca":false},{"name":"Hui Lin","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.001980598226972714,"gpt":0.1770216877411218,"spread":0.175041089514149,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008000985,0.001262326,0.001173456,0.0007348386,0.0003631844,0.000783656,0.0008142211,0.001075448,0.004252424],"category_scores_gemma":[0.001570575,0.0004399161,0.0006133518,0.0005928201,0.0007406072,0.0005399743,0.0008841847,0.001066832,0.0004749923],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0007227427,"about_ca_system_score_gemma":0.001663941,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.008498983,"about_ca_topic_score_gemma":0.003440931,"domain_scores_codex":[0.9994503,0.0002264879,0.00001867771,0.00008297641,0.000166825,0.00005475829],"domain_scores_gemma":[0.9995826,0.0002579308,0.00003728198,0.00001994803,0.0000870766,0.00001513066],"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":[0.00002080186,0.00001360593,0.00005413126,0.00005875601,0.0000118098,0.00001535343,0.00001525241,0.9737916,0.0003884939,0.01260164,0.0005255067,0.01250309],"study_design_scores_gemma":[0.000007394538,0.00001524083,0.00002565901,0.000005737224,0.000002589143,0.000003815381,0.000002704734,0.9958449,0.0001038356,0.003147341,0.0008378383,0.000003018025],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.002116238,0.0003191749,0.9914623,0.0001097363,0.00005999436,0.00005973283,0.00004518159,0.000144876,0.005682766],"genre_scores_gemma":[0.5367809,0.001003209,0.4470339,0.0002583481,0.0002057585,0.001074474,0.0003310149,0.0002521836,0.01306017],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.008498983,"threshold_uncertainty_score":0.01689905,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W3018203150","doi":"10.26467/2079-0619-2020-23-2-33-46","title":"Experimental research of single - rotor helicopter unintentional yaw rotation","year":2020,"lang":"en","type":"article","venue":"Civil Aviation High TECHNOLOGIES","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Bell Helicopter Textron (Canada)","funders":"","keywords":"Rotor (electric); Rotation (mathematics); Yaw; Aeronautics; Aerospace engineering; Automotive engineering; Engineering; Computer science; Mechanical engineering; Artificial intelligence","authors":[{"name":"V. V. Efimov","is_ca":false},{"name":"V. A. Ivchin","is_ca":true},{"name":"Олег Евгеньевич Чернигин","is_ca":false},{"name":"Константин Олегович Чернигин","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.03987907996651476,"gpt":0.2558214664268069,"spread":0.2159423864602921,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004674679,0.0005242492,0.0002680302,0.0002813087,0.0003147103,0.0002044159,0.0003157718,0.0003398,0.002824001],"category_scores_gemma":[0.0009681373,0.0001962298,0.0003544262,0.0001288651,0.0004056942,0.0003046301,0.0003502207,0.0004978378,0.0002612581],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.00008999365,"about_ca_system_score_gemma":0.0002573396,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.0004007375,"about_ca_topic_score_gemma":0.0005494913,"domain_scores_codex":[0.9996213,0.00006460134,0.00003457954,0.00008977592,0.0001051692,0.00008458888],"domain_scores_gemma":[0.999078,0.0003320308,0.0001325397,0.0001669599,0.0002028808,0.00008754644],"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":[0.002135373,0.002874626,0.006101661,0.0004114442,0.000034841,0.000493265,0.0005091319,0.002497135,0.9727237,0.0004225197,0.0002253086,0.01157108],"study_design_scores_gemma":[0.0003094469,0.09626175,0.05398886,0.0001244178,0.0001484567,0.0008318239,0.001771889,0.01196507,0.8306108,0.0003966368,0.003514577,0.00007634872],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.9969016,0.00007286764,0.002186469,0.00001562854,0.00002881895,0.00007987153,0.0001208003,0.00001973164,0.0005741686],"genre_scores_gemma":[0.9949228,0.0002187466,0.003201946,0.00001970895,0.000009583122,0.000121406,0.0001895405,0.000006607377,0.001309606],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.002824001,"threshold_uncertainty_score":0.009447277,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null}]}