{"meta":{"query_hash":"97374602ab50","filters":{"venue":"AIAA/AAS Astrodynamics Specialist Conference and Exhibit"},"cohort_total":12,"direct_labels_cover":0,"predictions_cover":12,"exported":12,"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/97374602ab50","api":"https://metacan.xera.ac/api/v1/cohort?venue=AIAA%2FAAS+Astrodynamics+Specialist+Conference+and+Exhibit"},"results":[{"id":"W2099439413","doi":"10.2514/6.2006-6653","title":"Attitude Dynamics of a Rigid Body around the Lagrangian Points","year":2006,"lang":"en","type":"article","venue":"AIAA/AAS Astrodynamics Specialist Conference and Exhibit","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Dynamics (music); Lagrangian; Computer science; Rigid body dynamics; Classical mechanics; Rigid body; Physics; Theoretical physics; Acoustics","score_opus":0.004713155061768184,"score_gpt":0.19225550481853815,"score_spread":0.18754234975676998,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2099439413","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.88989747,0.0004131873,0.069224514,0.00204699,0.00082215987,0.00060786353,0.0004543146,0.0002447932,0.0362887],"genre_scores_gemma":[0.9982399,0.00015287143,0.00040289926,0.00006353418,0.00044944714,0.000023250916,0.00016220585,0.000054824814,0.00045109805],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9982387,0.00003735229,0.00051523023,0.00034949233,0.00032543475,0.0005337956],"domain_scores_gemma":[0.9990198,0.00008171927,0.00013161573,0.00051620154,0.00014447802,0.0001061961],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00021889935,0.0003825019,0.00046996865,0.00012778735,0.0001708634,0.0002223202,0.00039434034,0.00016506489,0.00008090562],"category_scores_gemma":[0.000015841606,0.0003252441,0.0001581515,0.00025269855,0.00028914516,0.00018313751,0.00008624477,0.0003295651,0.000018168173],"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":[0.00010391426,0.00020232073,0.05849794,0.00018205735,0.0003359705,0.0000458287,0.00035995603,0.005680884,0.008321248,0.91513646,0.0011830786,0.009950362],"study_design_scores_gemma":[0.0011674381,0.00010297203,0.050127115,0.00009275535,0.00013640258,0.000031568707,0.0005367107,0.9276063,0.00010740774,0.01651529,0.0029617841,0.00061429484],"about_ca_topic_score_codex":0.00086562574,"about_ca_topic_score_gemma":0.011593969,"teacher_disagreement_score":0.92192537,"about_ca_system_score_codex":0.00013034919,"about_ca_system_score_gemma":0.000060318584,"threshold_uncertainty_score":0.99991995},"labels":[],"label_agreement":null},{"id":"W2120274407","doi":"10.2514/6.2006-6523","title":"Practical, Model-Free, Completely Robust Learning Control using Reversed Time Input Runs","year":2006,"lang":"en","type":"article","venue":"AIAA/AAS Astrodynamics Specialist Conference and Exhibit","topic":"Iterative Learning Control Systems","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lakehead University","funders":"","keywords":"Computer science; Control (management); Control theory (sociology); Artificial intelligence","score_opus":0.020971132774480403,"score_gpt":0.22863042700991357,"score_spread":0.20765929423543317,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2120274407","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.28396237,0.00009606889,0.6940094,0.00055207964,0.00038387981,0.0006226696,0.00015512094,0.0005693428,0.019649038],"genre_scores_gemma":[0.98588675,0.000014031328,0.011787099,0.00008178099,0.0008131955,0.000017743745,0.00012649312,0.000104470986,0.0011684572],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99738634,0.00019347548,0.0006866926,0.00055147894,0.0004194269,0.0007625829],"domain_scores_gemma":[0.9986827,0.00018310944,0.00022599768,0.00047088493,0.00026266745,0.00017468339],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0004001327,0.0005215721,0.00075795717,0.0001973408,0.0003886878,0.00056772184,0.00027908888,0.00024156328,0.00016053111],"category_scores_gemma":[0.00014851682,0.00057222584,0.00013380156,0.00022561017,0.00020862326,0.00054184144,0.00009981108,0.0008132935,0.0000801601],"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":[0.00006920477,0.00004312424,0.0029883436,0.00006530253,0.000101522186,0.00004820466,0.00019564273,0.9434429,0.030428214,0.02038689,0.0019620834,0.0002685707],"study_design_scores_gemma":[0.0017802685,0.000079633406,0.0010240751,0.0001182481,0.000090810514,0.000048064885,0.000108579596,0.99266195,0.000035755675,0.00048822878,0.0029955115,0.0005688564],"about_ca_topic_score_codex":0.00034037846,"about_ca_topic_score_gemma":0.00029780032,"teacher_disagreement_score":0.7019244,"about_ca_system_score_codex":0.00024149726,"about_ca_system_score_gemma":0.00012710704,"threshold_uncertainty_score":0.9996729},"labels":[],"label_agreement":null},{"id":"W2129225051","doi":"10.2514/6.2006-6759","title":"Second Order Relative Motion Model for Spacecraft Under J2 Perturbations","year":2006,"lang":"en","type":"article","venue":"AIAA/AAS Astrodynamics Specialist Conference and Exhibit","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"","keywords":"Spacecraft; Motion (physics); Order (exchange); Relative motion; Computer science; Physics; Control theory (sociology); Classical mechanics; Artificial intelligence; Astronomy","score_opus":0.009474280282039671,"score_gpt":0.20464696719655387,"score_spread":0.1951726869145142,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2129225051","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.09604083,0.000113373855,0.8881878,0.0009187721,0.00030232582,0.0004802934,0.0003720325,0.0001779037,0.013406662],"genre_scores_gemma":[0.98708534,0.00004673808,0.0059065362,0.00010117282,0.00039087253,0.00009897274,0.00035085628,0.000070148475,0.0059493477],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99853164,0.00001722089,0.00036660364,0.00041497356,0.00018459816,0.00048493518],"domain_scores_gemma":[0.9991725,0.00007818123,0.00008371056,0.00028749654,0.00026246128,0.000115620096],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.000114578026,0.00035825445,0.0003548969,0.00014477012,0.00023198791,0.0002208792,0.00014437835,0.00020989278,0.00014612601],"category_scores_gemma":[0.000021011647,0.00038146463,0.0001172796,0.00017964891,0.00010968939,0.00038306377,0.00003754203,0.00025140264,0.00001307064],"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":[0.00004289729,0.000076185126,0.0009435646,0.0000648242,0.00012213999,0.0000028782774,0.00040038777,0.2032305,0.012669731,0.7785415,0.0018591863,0.002046215],"study_design_scores_gemma":[0.00088490144,0.000039854644,0.002899438,0.000023328796,0.00006227938,0.000004470514,0.00019134031,0.9470334,0.000030283334,0.047137864,0.0012980207,0.00039481663],"about_ca_topic_score_codex":0.00007391889,"about_ca_topic_score_gemma":0.0045860447,"teacher_disagreement_score":0.8910445,"about_ca_system_score_codex":0.00015259921,"about_ca_system_score_gemma":0.0000791175,"threshold_uncertainty_score":0.99986374},"labels":[],"label_agreement":null},{"id":"W2144419833","doi":"10.2514/6.2004-5205","title":"Spacecraft Slew-Stare-Slew with Vibration Reduction: Simulation and Ground Experiments","year":2004,"lang":"en","type":"article","venue":"AIAA/AAS Astrodynamics Specialist Conference and Exhibit","topic":"Dynamics and Control of Mechanical Systems","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Spacecraft; Reduction (mathematics); Slew rate; Vibration; Computer science; Cost reduction; Environmental science; Aerospace engineering; Control theory (sociology); Physics; Engineering; Acoustics; Electrical engineering; Mathematics; Artificial intelligence","score_opus":0.012204723002102813,"score_gpt":0.22282610730884517,"score_spread":0.21062138430674235,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2144419833","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8541052,0.000225411,0.1413634,0.0004841516,0.00052142754,0.0004354537,0.00002770558,0.00017922443,0.002658057],"genre_scores_gemma":[0.9979958,0.000083917075,0.0012258248,0.000032156935,0.0004156934,0.000025816984,0.000068270456,0.0000401057,0.00011239651],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987051,0.000020675285,0.00032056906,0.00037558167,0.00026303323,0.0003150777],"domain_scores_gemma":[0.9994072,0.00001863657,0.00008344989,0.00022652083,0.00009400423,0.00017022311],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0000955425,0.00029346911,0.00031774343,0.00008034782,0.00016536721,0.0003329135,0.00009542287,0.0001358485,0.000038018374],"category_scores_gemma":[0.000007517076,0.00027978473,0.00003989025,0.00012825019,0.00008266708,0.00045411102,0.000037466383,0.00017808347,0.000008468786],"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":[0.0004365963,0.00020791388,0.0016912699,0.0002588385,0.00038386913,0.00005836071,0.002766619,0.5502618,0.033252407,0.38268813,0.00006832762,0.027925884],"study_design_scores_gemma":[0.0045308764,0.000709119,0.008998485,0.00037552186,0.0001291625,0.00009365213,0.0022934694,0.9701664,0.00046633944,0.008905255,0.0021196946,0.001212028],"about_ca_topic_score_codex":0.00019040884,"about_ca_topic_score_gemma":0.00047721856,"teacher_disagreement_score":0.41990462,"about_ca_system_score_codex":0.00016932044,"about_ca_system_score_gemma":0.000045597786,"threshold_uncertainty_score":0.9999654},"labels":[],"label_agreement":null},{"id":"W2151925466","doi":"10.2514/6.2002-4522","title":"Dynamics and Control of a Manipulator with Slewing and Deployable Links","year":2002,"lang":"en","type":"article","venue":"AIAA/AAS Astrodynamics Specialist Conference and Exhibit","topic":"Dynamics and Control of Mechanical Systems","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of British Columbia","funders":"","keywords":"Dynamics (music); Manipulator (device); Computer science; Control (management); Control theory (sociology); Mobile manipulator; Control engineering; Vehicle dynamics; Robot; Engineering; Mobile robot; Aerospace engineering; Artificial intelligence; Physics","score_opus":0.008337766688797795,"score_gpt":0.17380353523646816,"score_spread":0.16546576854767037,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2151925466","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8971582,0.0009871889,0.09592509,0.00048204072,0.00020109807,0.0004436157,0.00012943399,0.00013937836,0.0045339568],"genre_scores_gemma":[0.99851686,0.00043721692,0.00064227474,0.000053120835,0.00012532828,0.00001607481,0.00001202976,0.000049551054,0.00014752321],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9985862,0.000025993308,0.00041485517,0.00036023027,0.000218638,0.00039407663],"domain_scores_gemma":[0.99926794,0.00006889093,0.000105038016,0.00024387003,0.00009983856,0.00021440642],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00015428707,0.000318811,0.00057427137,0.00009375869,0.00010215947,0.00017249609,0.00012866387,0.00022343446,0.000036958747],"category_scores_gemma":[0.00001688623,0.000291632,0.000046001263,0.00011108117,0.00014174901,0.00019424531,0.00005448404,0.00033283848,0.0000026562557],"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":[0.00027169343,0.00019210952,0.064973794,0.0010276167,0.00082025595,0.00011470521,0.0010695382,0.0046965852,0.009593075,0.81780535,0.00010021493,0.09933509],"study_design_scores_gemma":[0.0016996282,0.00022160773,0.0038695626,0.00015972921,0.00009763549,0.000052129184,0.0002758739,0.9920436,0.000024405681,0.0010001238,0.00019321172,0.00036250518],"about_ca_topic_score_codex":0.00014016556,"about_ca_topic_score_gemma":0.0011781952,"teacher_disagreement_score":0.987347,"about_ca_system_score_codex":0.00006657375,"about_ca_system_score_gemma":0.000015146779,"threshold_uncertainty_score":0.99995357},"labels":[],"label_agreement":null},{"id":"W2312276444","doi":"10.2514/6.2002-4520","title":"Attitude Dynamics of Satellites Orbiting Small Bodies","year":2002,"lang":"en","type":"article","venue":"AIAA/AAS Astrodynamics Specialist Conference and Exhibit","topic":"Astro and Planetary Science","field":"Physics and Astronomy","cited_by":30,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Astrobiology; Dynamics (music); Rotational dynamics; Computer science; Remote sensing; Aerospace engineering; Geology; Physics; Engineering","score_opus":0.021678669337936038,"score_gpt":0.2107977987264093,"score_spread":0.18911912938847325,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2312276444","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9208013,0.00016425783,0.011075154,0.00042575476,0.0002494316,0.00020187104,0.00046837848,0.000042160766,0.06657169],"genre_scores_gemma":[0.99373955,0.00007268928,0.00405158,0.000038267986,0.0003596179,0.000005205386,0.00026318608,0.000017125201,0.0014527885],"study_design_codex":"observational","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9982739,0.000045683937,0.0004707605,0.0004633883,0.00024085079,0.00050538575],"domain_scores_gemma":[0.9990072,0.00010931005,0.00025920867,0.0003217127,0.00013509316,0.00016746967],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00016860249,0.0003159747,0.0004301486,0.00010073899,0.00022914763,0.00015796027,0.0003362056,0.00006862908,0.0017029254],"category_scores_gemma":[0.000013306242,0.00030769332,0.00010848677,0.00015325345,0.00036814855,0.00026192793,0.00012958587,0.00025846722,0.00004996652],"study_design_candidate":"observational","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":[0.000021573109,0.00014154275,0.693115,0.000051441046,0.00008991662,0.000009371194,0.0010946788,0.0002859902,0.0012046128,0.22528951,0.00018797097,0.07850836],"study_design_scores_gemma":[0.0030253215,0.0009750389,0.3685628,0.00071777863,0.00039445044,0.000049634447,0.012657246,0.5746979,0.0016336673,0.0254058,0.00858582,0.0032945438],"about_ca_topic_score_codex":0.0007161552,"about_ca_topic_score_gemma":0.00079163007,"teacher_disagreement_score":0.5744119,"about_ca_system_score_codex":0.000024256628,"about_ca_system_score_gemma":0.000041406,"threshold_uncertainty_score":0.99993753},"labels":[],"label_agreement":null},{"id":"W2314893112","doi":"10.2514/6.2002-4516","title":"Spacecraft Vibration Reduction Following Orbit Adjustment Thruster Firing","year":2002,"lang":"en","type":"article","venue":"AIAA/AAS Astrodynamics Specialist Conference and Exhibit","topic":"Dynamics and Control of Mechanical Systems","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Spacecraft; Aerospace engineering; Reduction (mathematics); Vibration; Orbit (dynamics); Computer science; Ion thruster; Astrobiology; Physics; Engineering; Acoustics","score_opus":0.012384891216481465,"score_gpt":0.19568561940328005,"score_spread":0.1833007281867986,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2314893112","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8541911,0.001714823,0.0828286,0.0019241653,0.006047716,0.0010327889,0.000054706565,0.00072938367,0.051476713],"genre_scores_gemma":[0.99723595,0.00031189754,0.0006261696,0.00005409754,0.0008904358,0.000036409143,0.00003775284,0.000049188606,0.00075810734],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.998358,0.00003321135,0.00044225095,0.00039772963,0.0003088497,0.0004599203],"domain_scores_gemma":[0.9993582,0.000022863731,0.00008226038,0.00030586123,0.000054478456,0.00017638376],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00015554,0.00032589943,0.00038663304,0.000102908125,0.00015796468,0.0002773396,0.00016464309,0.00017148908,0.00031434296],"category_scores_gemma":[0.000013697661,0.00033609365,0.00014615714,0.00014998313,0.000036119778,0.0004168067,0.00005799272,0.00026226483,0.00007695616],"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":[0.00014577052,0.0004790355,0.0041417796,0.00060274196,0.0012417913,0.00016770816,0.0039505144,0.039833184,0.1449235,0.3137489,0.0076975315,0.48306757],"study_design_scores_gemma":[0.0010414508,0.00013188868,0.0020414763,0.00017973733,0.00009583972,0.000033272805,0.0004654712,0.98958725,0.00016700522,0.0016001085,0.004035783,0.0006207057],"about_ca_topic_score_codex":0.000049703787,"about_ca_topic_score_gemma":0.00022258131,"teacher_disagreement_score":0.94975406,"about_ca_system_score_codex":0.00017942037,"about_ca_system_score_gemma":0.00001265784,"threshold_uncertainty_score":0.9999091},"labels":[],"label_agreement":null},{"id":"W2316717142","doi":"10.2514/6.2004-5401","title":"Optimization of a Low-Thrust Salvage Mission from a Highly Inclined Geostationary Transfer Orbit to a Geostationary Orbit","year":2004,"lang":"en","type":"article","venue":"AIAA/AAS Astrodynamics Specialist Conference and Exhibit","topic":"Spacecraft Dynamics and Control","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"","keywords":"Geostationary orbit; Medium Earth orbit; Orbit (dynamics); Aerospace engineering; Geocentric orbit; Remote sensing; Synchronous orbit; Low earth orbit; Orbit determination; Geology; Geodesy; Satellite; Astrobiology; Computer science; Physics; Engineering","score_opus":0.005901957267565455,"score_gpt":0.20038915701522178,"score_spread":0.19448719974765633,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2316717142","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5161565,0.00009986568,0.47994202,0.0010815143,0.00027177198,0.00045425436,0.0006865084,0.00013115299,0.0011764322],"genre_scores_gemma":[0.9870627,0.000259346,0.010929802,0.00022193465,0.0002438588,0.000034827313,0.0011083273,0.000070772396,0.00006845289],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99798435,0.00003277664,0.0006533579,0.0004884505,0.0003879207,0.0004531257],"domain_scores_gemma":[0.99892634,0.00008511097,0.000076937155,0.00034220616,0.0003037798,0.0002656075],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00012781435,0.00039855173,0.00050843135,0.0002578566,0.00015128733,0.000117467534,0.00023612494,0.0002031056,0.00039375786],"category_scores_gemma":[0.000044272438,0.0004296555,0.0001031708,0.00038925893,0.00009399311,0.0003275378,0.00006736781,0.0002482614,0.000020748714],"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":[0.00038914406,0.00021153467,0.0012451812,0.00013411019,0.00017392497,0.00005602494,0.0021227947,0.91765153,0.042412944,0.028154543,0.00015938708,0.007288852],"study_design_scores_gemma":[0.0035758992,0.00031972575,0.015383797,0.0003671641,0.00012212813,0.00001109765,0.000882152,0.97224104,0.00081483426,0.004837692,0.0005676311,0.00087683205],"about_ca_topic_score_codex":0.0006918065,"about_ca_topic_score_gemma":0.00074110925,"teacher_disagreement_score":0.4709062,"about_ca_system_score_codex":0.00016624211,"about_ca_system_score_gemma":0.00020187971,"threshold_uncertainty_score":0.9998155},"labels":[],"label_agreement":null},{"id":"W2320936932","doi":"10.2514/6.2008-7378","title":"Mechanics of a Very Long Tethered System","year":2008,"lang":"en","type":"article","venue":"AIAA/AAS Astrodynamics Specialist Conference and Exhibit","topic":"Fluid Dynamics Simulations and Interactions","field":"Engineering","cited_by":2,"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":"Computer science","score_opus":0.013038399428595443,"score_gpt":0.20707937364644416,"score_spread":0.19404097421784872,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2320936932","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8512092,0.00013015723,0.13230628,0.00003571431,0.0007341374,0.00020627251,0.00014366687,0.00021655473,0.015018007],"genre_scores_gemma":[0.9980325,0.00025011515,0.0011938389,0.000009685448,0.00015302468,0.000011145792,0.00006149117,0.00003759509,0.00025061404],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988677,0.000021316773,0.00042633596,0.00022827118,0.00018539923,0.00027100445],"domain_scores_gemma":[0.99926144,0.000050395287,0.00010099104,0.0003181312,0.00016730686,0.000101722224],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00007702191,0.0002252155,0.00033686747,0.00015840198,0.00015390207,0.000047324225,0.00015357742,0.00012077331,0.00009443144],"category_scores_gemma":[0.000020644884,0.00024157265,0.000095153766,0.00019715424,0.00008291313,0.0002383283,0.00005006177,0.0002057203,0.000021661555],"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":[0.00012253426,0.00024269067,0.020209901,0.0007384492,0.00049589097,0.00013899866,0.0023167522,0.20703797,0.02185039,0.738453,0.0012585327,0.0071348967],"study_design_scores_gemma":[0.0003900663,0.0000669234,0.007706043,0.00013240962,0.0000357072,0.000089047215,0.0005119804,0.98982877,0.00021331088,0.0003122363,0.000433203,0.0002803012],"about_ca_topic_score_codex":0.00010921173,"about_ca_topic_score_gemma":0.00032145108,"teacher_disagreement_score":0.7827908,"about_ca_system_score_codex":0.00011819248,"about_ca_system_score_gemma":0.000058309135,"threshold_uncertainty_score":0.9851047},"labels":[],"label_agreement":null},{"id":"W2324906028","doi":"10.2514/6.2006-6664","title":"Pseudo-Doppler Velocity Navigation for Lidar-Based Planetary Exploration","year":2006,"lang":"en","type":"article","venue":"AIAA/AAS Astrodynamics Specialist Conference and Exhibit","topic":"Aerospace Engineering and Energy Systems","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"NGC Aerospace (Canada)","funders":"Canadian Space Agency","keywords":"Lidar; Doppler effect; Remote sensing; Computer science; Geodesy; Geology; Physics; Astronomy","score_opus":0.011364559854871703,"score_gpt":0.19595862082014934,"score_spread":0.18459406096527764,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2324906028","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5558473,0.000082149454,0.44019958,0.0002160698,0.0007822361,0.0002915042,0.00017760815,0.0004160948,0.0019874738],"genre_scores_gemma":[0.9923874,0.000019645633,0.0046768067,0.000016779579,0.0009096333,0.0000756945,0.001611294,0.000050452294,0.00025225905],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.998848,0.00001545313,0.00032389825,0.00028549143,0.00017596403,0.0003511629],"domain_scores_gemma":[0.9995061,0.000044798922,0.00006068294,0.00021552177,0.00008577226,0.00008713088],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00012402274,0.00028029943,0.00028425103,0.000079624726,0.00013649397,0.00015736022,0.000106873806,0.00015632174,0.000019979549],"category_scores_gemma":[0.000008699745,0.00030704762,0.00006617133,0.000120218254,0.00005364634,0.00027675583,0.000013286903,0.00015192854,0.000012688755],"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":[0.00005944093,0.00005814453,0.0028511782,0.0003494934,0.00005509613,0.000010074267,0.0002469068,0.94351095,0.00785742,0.035825863,0.004938201,0.004237253],"study_design_scores_gemma":[0.0007571317,0.0000911874,0.0044209417,0.00012191198,0.000033510616,0.000009347373,0.00015831784,0.9845956,0.0011236902,0.0010479903,0.0071369153,0.0005034854],"about_ca_topic_score_codex":0.00033295254,"about_ca_topic_score_gemma":0.00062603207,"teacher_disagreement_score":0.43654016,"about_ca_system_score_codex":0.00008797212,"about_ca_system_score_gemma":0.000036586483,"threshold_uncertainty_score":0.9999382},"labels":[],"label_agreement":null},{"id":"W2327902065","doi":"10.2514/6.2004-5308","title":"Dynamics of a Multi-Tethered Satellite Formation","year":2004,"lang":"en","type":"article","venue":"AIAA/AAS Astrodynamics Specialist Conference and Exhibit","topic":"Space Satellite Systems and Control","field":"Engineering","cited_by":19,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Orbital plane; Orbit (dynamics); Circular orbit; Satellite; Physics; Plane (geometry); Dynamics (music); Spin (aerodynamics); Motion (physics); Stability (learning theory); Spinning; Aerospace engineering; Classical mechanics; Geometry; Computer science; Engineering; Mathematics; Mechanical engineering; Acoustics","score_opus":0.011240215669219998,"score_gpt":0.20963534007080634,"score_spread":0.19839512440158633,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2327902065","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7682425,0.0012772095,0.21664332,0.00053826335,0.00069390313,0.00070998404,0.00023666325,0.0003122553,0.011345913],"genre_scores_gemma":[0.99666935,0.00079731934,0.002055029,0.000021974885,0.00014273798,0.000016858872,0.00010577805,0.000040134513,0.00015084514],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.998657,0.00002263284,0.0005029046,0.00023942126,0.00021129817,0.00036676603],"domain_scores_gemma":[0.9992876,0.000021501037,0.00012376123,0.0003046088,0.00014041954,0.00012211804],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00014513326,0.00028587825,0.00041789422,0.00013462131,0.000072307965,0.00010224435,0.00016927776,0.00015977028,0.000037076126],"category_scores_gemma":[0.000014245402,0.00028881207,0.00010169024,0.00018104739,0.00010908137,0.00031626163,0.000036120447,0.00019068019,0.000024433944],"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":[0.00018839758,0.00029689324,0.009276939,0.0011602859,0.00041617372,0.0000536361,0.0073093856,0.036014665,0.047975425,0.60618895,0.00004834778,0.29107088],"study_design_scores_gemma":[0.008589723,0.00047182714,0.03009983,0.00094286795,0.00021128023,0.00011987025,0.008281923,0.92440766,0.0053266287,0.014099127,0.005426626,0.0020226627],"about_ca_topic_score_codex":0.00029032808,"about_ca_topic_score_gemma":0.004461993,"teacher_disagreement_score":0.888393,"about_ca_system_score_codex":0.00017088327,"about_ca_system_score_gemma":0.000047117923,"threshold_uncertainty_score":0.9999564},"labels":[],"label_agreement":null},{"id":"W2328964884","doi":"10.2514/6.2004-4987","title":"Lidar-Based Rendezvous Navigation for MSR","year":2004,"lang":"en","type":"article","venue":"AIAA/AAS Astrodynamics Specialist Conference and Exhibit","topic":"Astro and Planetary Science","field":"Physics and Astronomy","cited_by":8,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Canadian Space Agency","funders":"Centre National d’Etudes Spatiales; National Aeronautics and Space Administration","keywords":"Rendezvous; Lidar; Computer science; Remote sensing; Environmental science; Geology; Aerospace engineering; Engineering","score_opus":0.012328873775617977,"score_gpt":0.23531648129401322,"score_spread":0.22298760751839525,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2328964884","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.71980304,0.000022429824,0.2697286,0.00087911845,0.00038976764,0.00044975133,0.00053854793,0.00005679523,0.008131953],"genre_scores_gemma":[0.9900575,0.000002384452,0.007627873,0.00010668426,0.0006591351,0.000029551853,0.0012108987,0.000017861137,0.00028808715],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99848163,0.000021982622,0.00031055819,0.0004923404,0.00022859336,0.00046488486],"domain_scores_gemma":[0.9991837,0.00005897253,0.00016146233,0.00027720068,0.00013365102,0.0001849783],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00016976698,0.00027310738,0.0002767201,0.00006893013,0.0003317179,0.00022976416,0.00023992006,0.000069734655,0.00022436224],"category_scores_gemma":[0.00000809008,0.00027089246,0.00010629587,0.00015333669,0.00018799538,0.00028993384,0.00003799087,0.0001894073,0.00003460615],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":"theoretical_or_conceptual","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000284971,0.00036789052,0.1189535,0.00008804607,0.00010887649,0.000017252683,0.0009962871,0.009788342,0.0070180837,0.7752527,0.0006014971,0.08652253],"study_design_scores_gemma":[0.027285632,0.004903685,0.32737362,0.0016116265,0.00082492724,0.00006823577,0.009511739,0.17499365,0.014407868,0.34664053,0.08457139,0.0078071076],"about_ca_topic_score_codex":0.00062202144,"about_ca_topic_score_gemma":0.00016426071,"teacher_disagreement_score":0.4286122,"about_ca_system_score_codex":0.000040567542,"about_ca_system_score_gemma":0.00027245615,"threshold_uncertainty_score":0.9999743},"labels":[],"label_agreement":null}]}