{"meta":{"query_hash":"6c7a0987d484","filters":{"venue":"Astrodynamics"},"cohort_total":7,"direct_labels_cover":0,"predictions_cover":7,"exported":7,"export_cap":100000,"truncated":false,"label_status":"direct model label, unvalidated","prediction_status":"machine_predicted_unvalidated (Codex and Gemma teacher distillation)","score_status":"score_only:v0-immature-baseline","snapshot":{"source":"OpenAlex, pinned release, all 482 partitions","release":"2026-06-24","frame_built":"2026-07-12"},"permalink":"https://metacan.xera.ac/q/6c7a0987d484","api":"https://metacan.xera.ac/api/v1/cohort?venue=Astrodynamics"},"results":[{"id":"W2752043612","doi":"10.1007/s42064-017-0008-3","title":"Calibration of atmospheric density model using two-line element data","year":2017,"lang":"en","type":"article","venue":"Astrodynamics","topic":"Ionosphere and magnetosphere dynamics","field":"Physics and Astronomy","cited_by":3,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"York University","funders":"","keywords":"Calibration; Line (geometry); Environmental science; Element (criminal law); Remote sensing; Geology; Mathematics; Statistics; Geometry","score_opus":0.027638545294548532,"score_gpt":0.28808722210048426,"score_spread":0.26044867680593575,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2752043612","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.71655506,0.0004998948,0.25792363,0.00039694633,0.0003036419,0.0001524728,0.005829593,0.0070089716,0.0113298725],"genre_scores_gemma":[0.954201,0.00014456823,0.041378245,0.00006441083,0.000025787054,0.000074890006,0.0030490179,0.00024246438,0.0008196075],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996724,0.00004355457,0.0000111478475,0.00013135244,0.000108046435,0.000033454566],"domain_scores_gemma":[0.999671,0.000051501796,0.000028025031,0.00010109637,0.00012220733,0.000026223715],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00041901073,0.00064393994,0.000405356,0.00062907115,0.00044730943,0.0004605045,0.0010971705,0.0008229272,0.0009718006],"category_scores_gemma":[0.0010834262,0.00036900115,0.0005609898,0.0008340719,0.00020166107,0.0009163277,0.00046369052,0.00069795025,0.0008390309],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00048066233,0.00042201363,0.21333316,0.00027754248,0.00034952813,0.00034427427,0.0005329428,0.5281081,0.1166377,0.0055091316,0.008807028,0.12519795],"study_design_scores_gemma":[0.00012190154,0.00004782131,0.08422942,0.000024251885,0.00008413048,0.00010088304,0.00006244384,0.8869036,0.021562373,0.0017759278,0.00502259,0.00006462884],"about_ca_topic_score_codex":0.012507043,"about_ca_topic_score_gemma":0.009895456,"teacher_disagreement_score":0.012507043,"about_ca_system_score_codex":0.00059579505,"about_ca_system_score_gemma":0.0007085226,"threshold_uncertainty_score":0.024868488},"labels":[],"label_agreement":null},{"id":"W3128170399","doi":"10.1007/s42064-020-0097-2","title":"Trajectory correction for lunar flyby transfers to libration point orbits using continuous thrust","year":2021,"lang":"en","type":"article","venue":"Astrodynamics","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":13,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Trajectory; Ephemeris; Libration (molecule); Thrust; Spacecraft; Physics; Orbit (dynamics); Aerospace engineering; Geodesy; Computer science; Point (geometry); Geology; Mathematics; Astronomy; Geometry; Engineering; Satellite","score_opus":0.0055827401418334765,"score_gpt":0.20016930101775043,"score_spread":0.19458656087591697,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3128170399","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.48857796,0.00019548884,0.5066533,0.00008734801,0.000058820235,0.000048131635,0.000024697603,0.0005270003,0.0038272908],"genre_scores_gemma":[0.99336857,0.000022135957,0.0060825865,0.000005505222,0.0000027288559,0.000008026697,0.000008137036,0.000007035346,0.0004951821],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999336,0.000011744351,0.0000033335625,0.000011506039,0.000027753698,0.0000120683735],"domain_scores_gemma":[0.9998216,0.00004483609,0.00005005287,0.00002187357,0.000048367525,0.000013310765],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015559627,0.00033307073,0.00016244974,0.00024562486,0.00021238373,0.00024983182,0.00026824337,0.00021475871,0.00078092434],"category_scores_gemma":[0.00054126146,0.000082690436,0.0001238111,0.00013278617,0.00024408872,0.00018275635,0.00028641548,0.00021638886,0.00007270165],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00026675864,0.00005711988,0.0018421817,0.00007833092,0.000035859535,0.00015080908,0.00012748603,0.88040787,0.03830699,0.0032784743,0.00047224932,0.07497583],"study_design_scores_gemma":[0.000015504556,0.00011948228,0.00076293433,0.0000039442334,0.0000065859244,0.000016329508,0.0000208035,0.99350053,0.0049050353,0.00024697997,0.0003970497,0.0000047744074],"about_ca_topic_score_codex":0.006099348,"about_ca_topic_score_gemma":0.0030031935,"teacher_disagreement_score":0.006099348,"about_ca_system_score_codex":0.00020526,"about_ca_system_score_gemma":0.00033010647,"threshold_uncertainty_score":0.0121276975},"labels":[],"label_agreement":null},{"id":"W4380878712","doi":"10.1007/s42064-022-0156-y","title":"Orbital radius keeping of floating partial space elevator in cargo transposition","year":2023,"lang":"en","type":"article","venue":"Astrodynamics","topic":"Space Satellite Systems and Control","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"York University","funders":"","keywords":"RADIUS; Satellite; Orbital maneuver; Control theory (sociology); Transposition (logic); Computer science; Elevator; Orbital inclination; Physics; Simulation; Aerospace engineering; Engineering; Mathematics; Control (management); Spacecraft","score_opus":0.003971434670809477,"score_gpt":0.18579816633942942,"score_spread":0.18182673166861993,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4380878712","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8933455,0.00022805651,0.095686726,0.00014165333,0.00011124162,0.00001937811,0.000046720557,0.0003127033,0.0101079475],"genre_scores_gemma":[0.99343264,0.000047743706,0.003587151,0.000008524366,0.000008425343,0.00000465729,0.000027512295,0.000014924619,0.0028685795],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998362,0.000023507711,0.000006300822,0.000050257175,0.000045810717,0.00003786237],"domain_scores_gemma":[0.9998926,0.000020066986,0.000014278766,0.000021932738,0.000032948494,0.000018163259],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016646362,0.0002576033,0.00040653432,0.00020120225,0.00086372555,0.00041859635,0.0006051392,0.00033881562,0.0016510999],"category_scores_gemma":[0.0003065992,0.00013925512,0.00025969298,0.00025087805,0.0002989689,0.0005867349,0.00053384266,0.00026528494,0.0002172824],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0027203588,0.00017671907,0.028039493,0.00035659852,0.00010268975,0.0033980105,0.0024781164,0.37966347,0.36192542,0.020076577,0.0049079945,0.19615461],"study_design_scores_gemma":[0.00005141562,0.0006902489,0.009721092,0.000019662864,0.00009639473,0.00096339965,0.0012268465,0.92548317,0.055063486,0.0019744833,0.004649114,0.00006076386],"about_ca_topic_score_codex":0.0026413717,"about_ca_topic_score_gemma":0.0016002929,"teacher_disagreement_score":0.0026413717,"about_ca_system_score_codex":0.0001984968,"about_ca_system_score_gemma":0.00036123657,"threshold_uncertainty_score":0.005523503},"labels":[],"label_agreement":null},{"id":"W4392741529","doi":"10.1007/s42064-023-0190-4","title":"Evaluation of E-sail parameters on central spacecraft attitude stability using a high-fidelity rigid-flexible coupling model","year":2024,"lang":"en","type":"article","venue":"Astrodynamics","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":13,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"York University","funders":"","keywords":"Spacecraft; Solar sail; Coupling (piping); Aerospace engineering; Attitude control; Stability (learning theory); Angular velocity; Position (finance); Physics; Engineering; Computer science; Classical mechanics; Mechanical engineering","score_opus":0.03843581368599566,"score_gpt":0.2760665828942689,"score_spread":0.23763076920827322,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4392741529","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96082515,0.00012467222,0.033452876,0.0000797429,0.000020142636,0.000017089307,0.00007753649,0.00017024866,0.0052324957],"genre_scores_gemma":[0.9992217,0.000011266743,0.00059942517,0.0000029600023,8.9067237e-7,0.0000027668355,0.000017035603,0.0000060461607,0.00013800978],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998653,0.000044929737,0.000006235298,0.000016331254,0.0000322663,0.000034936464],"domain_scores_gemma":[0.99930644,0.00037857582,0.00006485003,0.00006621788,0.00014751755,0.000036524372],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00042201218,0.00045904724,0.0003786639,0.00028808083,0.0003734603,0.00043725665,0.00032612472,0.0007207374,0.0013475207],"category_scores_gemma":[0.0016880352,0.00020489217,0.00034559946,0.00014896938,0.00037684833,0.0005813936,0.0005009639,0.00038372885,0.00013447425],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00027636983,0.000073592535,0.0018023021,0.0000467639,0.000022516642,0.000060486054,0.00002877962,0.98614836,0.005588021,0.00045210702,0.00012003694,0.0053806035],"study_design_scores_gemma":[0.000009195355,0.00006951257,0.0011286894,0.000004190905,0.000009686073,0.000005336597,0.000016142169,0.99637055,0.0022614265,0.00005966708,0.00006130806,0.00000424065],"about_ca_topic_score_codex":0.0074695116,"about_ca_topic_score_gemma":0.0045983293,"teacher_disagreement_score":0.0074695116,"about_ca_system_score_codex":0.00023185415,"about_ca_system_score_gemma":0.00031443316,"threshold_uncertainty_score":0.014852047},"labels":[],"label_agreement":null},{"id":"W4399506329","doi":"10.1007/s42064-024-0225-5","title":"Controlled deployment of a long tether to operate as a partial space elevator","year":2024,"lang":"en","type":"article","venue":"Astrodynamics","topic":"Space Satellite Systems and Control","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Software deployment; Geostationary orbit; Aerospace engineering; Spacecraft; Elevator; Computer science; Controller (irrigation); Parametric statistics; Control theory (sociology); Simulation; Engineering; Satellite; Mathematics","score_opus":0.003309042351124301,"score_gpt":0.21499895883495743,"score_spread":0.21168991648383312,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399506329","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9328462,0.00004593129,0.06033912,0.0001520933,0.00012141475,0.000044583605,0.000047904537,0.0005129452,0.0058898507],"genre_scores_gemma":[0.99430287,0.000009240987,0.0040441854,0.000015065048,0.0000043798327,0.000017720738,0.00001762699,0.000013451753,0.0015755328],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999268,0.000014708576,0.0000020688592,0.000014804327,0.000020967036,0.00002061972],"domain_scores_gemma":[0.99972576,0.00005690487,0.000050322025,0.00004897985,0.000050107676,0.00006797371],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012024295,0.00023288347,0.00014497583,0.00019251622,0.0003600923,0.0001922999,0.0003495147,0.0002615372,0.0015269703],"category_scores_gemma":[0.00038197244,0.00009250446,0.000086592,0.00007113714,0.0002811122,0.00022302709,0.0005816377,0.0003127088,0.00028552965],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0017311561,0.0002966763,0.005527377,0.00012476198,0.00005242084,0.0011400651,0.0005824838,0.077450216,0.8345276,0.004897265,0.0023880033,0.07128199],"study_design_scores_gemma":[0.00031002407,0.005318216,0.017649414,0.00002958912,0.000046701276,0.00039464433,0.00033240087,0.80767727,0.15458767,0.0012511809,0.012327486,0.000075469965],"about_ca_topic_score_codex":0.0009887952,"about_ca_topic_score_gemma":0.0019804894,"teacher_disagreement_score":0.0015269703,"about_ca_system_score_codex":0.00015429567,"about_ca_system_score_gemma":0.00028816046,"threshold_uncertainty_score":0.0051082373},"labels":[],"label_agreement":null},{"id":"W4410757326","doi":"10.1007/s42064-024-0218-4","title":"Attitude trajectory design and optimization for planar space-based solar power arrays in molniya orbits","year":2025,"lang":"en","type":"article","venue":"Astrodynamics","topic":"Spacecraft Design and Technology","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"York University","funders":"","keywords":"Planar; Trajectory; Trajectory optimization; Space (punctuation); Aerospace engineering; Power (physics); Computer science; Control theory (sociology); Physics; Engineering; Computer graphics (images); Astronomy; Artificial intelligence; Control (management)","score_opus":0.0059913204992274455,"score_gpt":0.20164795838864896,"score_spread":0.1956566378894215,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4410757326","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.31452423,0.00036202176,0.6602787,0.0005200228,0.00004987762,0.00008135239,0.00019247232,0.00022536915,0.023766035],"genre_scores_gemma":[0.9597024,0.00014694882,0.035788443,0.0000343782,0.000012626283,0.000074939744,0.00010000407,0.00004944724,0.004090894],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999248,0.000018448018,0.0000019202002,0.000011789493,0.000026683947,0.00001641727],"domain_scores_gemma":[0.99986184,0.000055283574,0.000023789598,0.000007769273,0.0000394338,0.000011777672],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002250933,0.00035762275,0.00033988987,0.00023722574,0.00028866285,0.00049159414,0.0002712847,0.00046948643,0.0016942611],"category_scores_gemma":[0.000701544,0.00027079319,0.00031197182,0.0003559157,0.00029569594,0.0002990476,0.00039894582,0.0003676267,0.00027706643],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000032702545,0.000008803223,0.00037245045,0.000016629381,0.000008698224,0.000019423018,0.000026218535,0.9898908,0.0016015023,0.0013349582,0.00020152096,0.0064862054],"study_design_scores_gemma":[0.00000840035,0.00005087188,0.00029883525,0.0000033414094,0.0000044219987,0.000007334151,0.00003398063,0.99794763,0.00065789133,0.00058624335,0.00039851994,0.0000026094547],"about_ca_topic_score_codex":0.0067247986,"about_ca_topic_score_gemma":0.006204396,"teacher_disagreement_score":0.0067247986,"about_ca_system_score_codex":0.0005323992,"about_ca_system_score_gemma":0.00086664426,"threshold_uncertainty_score":0.013371348},"labels":[],"label_agreement":null},{"id":"W4412413117","doi":"10.1007/s42064-025-0273-5","title":"A geometric approach to optimal motion planning for close-range rendezvous and synchronization","year":2025,"lang":"en","type":"article","venue":"Astrodynamics","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"","keywords":"Rendezvous; Synchronization (alternating current); Computer science; Range (aeronautics); Motion planning; Motion (physics); Computer vision; Artificial intelligence; Computer network; Engineering; Aerospace engineering; Robot; Spacecraft","score_opus":0.004454323153669872,"score_gpt":0.20813511365545295,"score_spread":0.2036807905017831,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4412413117","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0013364946,0.00013853486,0.99550444,0.00011194484,0.00004045683,0.00001290075,0.000020321526,0.000053626656,0.0027813306],"genre_scores_gemma":[0.4445774,0.0013518388,0.54194057,0.00019016571,0.00032132497,0.0002525783,0.00022059053,0.00026971428,0.010875819],"study_design_codex":"simulation_or_modeling","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.9995209,0.0001363218,0.000022573886,0.00010812261,0.0001739953,0.000038214257],"domain_scores_gemma":[0.9996137,0.00020309785,0.000046165336,0.0000380145,0.00007765067,0.000021367032],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00053133944,0.00094596954,0.0010463084,0.0012492351,0.00070114527,0.0010245582,0.0014264514,0.0010214379,0.0041304636],"category_scores_gemma":[0.0021021282,0.00078731327,0.001078585,0.0011792509,0.0016215435,0.0014642384,0.0021477418,0.0015041628,0.0005585129],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000020855201,0.000017469716,0.00011235372,0.00005015567,0.000019840461,0.000044235596,0.00006145687,0.8132814,0.0010009767,0.1543587,0.0011325079,0.02990017],"study_design_scores_gemma":[0.000006885726,0.000036373734,0.000075614706,0.000010212892,0.000007215842,0.000023962348,0.000018111237,0.9134308,0.0003130764,0.08342325,0.0026440925,0.000010414632],"about_ca_topic_score_codex":0.0053372686,"about_ca_topic_score_gemma":0.004912251,"teacher_disagreement_score":0.0053372686,"about_ca_system_score_codex":0.000826186,"about_ca_system_score_gemma":0.00100197,"threshold_uncertainty_score":0.013817728},"labels":[],"label_agreement":null}]}