{"meta":{"page":1,"per_page":50,"max_per_page":100,"total":7,"total_is_capped":false,"direct_labels_cover":0,"predictions_cover":7,"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":"6c7a0987d484","filters":{"venue":"Astrodynamics"}},"results":[{"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,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"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","authors":[{"name":"Chonggang Du","is_ca":false},{"name":"Zheng Zhu","is_ca":true},{"name":"Changqing Wang","is_ca":false},{"name":"Aijun Li","is_ca":false},{"name":"Tuanjie Li","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.03843581368599566,"gpt":0.2760665828942689,"spread":0.2376307692082732,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004220122,0.0004590472,0.0003786639,0.0002880808,0.0003734603,0.0004372566,0.0003261247,0.0007207374,0.001347521],"category_scores_gemma":[0.001688035,0.0002048922,0.0003455995,0.0001489694,0.0003768483,0.0005813936,0.0005009639,0.0003837289,0.0001344742],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0002318542,"about_ca_system_score_gemma":0.0003144332,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.007469512,"about_ca_topic_score_gemma":0.004598329,"domain_scores_codex":[0.9998653,0.00004492974,0.000006235298,0.00001633125,0.0000322663,0.00003493646],"domain_scores_gemma":[0.9993064,0.0003785758,0.00006485003,0.00006621788,0.0001475176,0.00003652437],"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":[0.0002763698,0.00007359254,0.001802302,0.0000467639,0.00002251664,0.00006048605,0.00002877962,0.9861484,0.005588021,0.000452107,0.0001200369,0.005380603],"study_design_scores_gemma":[0.000009195355,0.00006951257,0.001128689,0.000004190905,0.000009686073,0.000005336597,0.00001614217,0.9963706,0.002261427,0.00005966708,0.00006130806,0.00000424065],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.9608251,0.0001246722,0.03345288,0.0000797429,0.00002014264,0.00001708931,0.00007753649,0.0001702487,0.005232496],"genre_scores_gemma":[0.9992217,0.00001126674,0.0005994252,0.000002960002,8.906724e-7,0.000002766835,0.0000170356,0.000006046161,0.0001380098],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.007469512,"threshold_uncertainty_score":0.01485205,"prediction_status":"machine_predicted_unvalidated"},"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,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"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","authors":[{"name":"Yi Qi","is_ca":false},{"name":"Anton de Ruiter","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.005582740141833476,"gpt":0.2001693010177504,"spread":0.194586560875917,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001555963,0.0003330707,0.0001624497,0.0002456249,0.0002123837,0.0002498318,0.0002682434,0.0002147587,0.0007809243],"category_scores_gemma":[0.0005412615,0.00008269044,0.0001238111,0.0001327862,0.0002440887,0.0001827564,0.0002864155,0.0002163889,0.00007270165],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.00020526,"about_ca_system_score_gemma":0.0003301065,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.006099348,"about_ca_topic_score_gemma":0.003003194,"domain_scores_codex":[0.9999336,0.00001174435,0.000003333563,0.00001150604,0.0000277537,0.00001206837],"domain_scores_gemma":[0.9998216,0.00004483609,0.00005005287,0.00002187357,0.00004836752,0.00001331077],"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":[0.0002667586,0.00005711988,0.001842182,0.00007833092,0.00003585954,0.0001508091,0.000127486,0.8804079,0.03830699,0.003278474,0.0004722493,0.07497583],"study_design_scores_gemma":[0.00001550456,0.0001194823,0.0007629343,0.000003944233,0.000006585924,0.00001632951,0.0000208035,0.9935005,0.004905035,0.00024698,0.0003970497,0.000004774407],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.488578,0.0001954888,0.5066533,0.00008734801,0.00005882023,0.00004813163,0.0000246976,0.0005270003,0.003827291],"genre_scores_gemma":[0.9933686,0.00002213596,0.006082586,0.000005505222,0.000002728856,0.000008026697,0.000008137036,0.000007035346,0.0004951821],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.006099348,"threshold_uncertainty_score":0.0121277,"prediction_status":"machine_predicted_unvalidated"},"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,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"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","authors":[{"name":"Jinbang Huang","is_ca":true},{"name":"Arun K. Misra","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.003309042351124301,"gpt":0.2149989588349574,"spread":0.2116899164838331,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001202429,0.0002328835,0.0001449758,0.0001925162,0.0003600923,0.0001922999,0.0003495147,0.0002615372,0.00152697],"category_scores_gemma":[0.0003819724,0.00009250446,0.000086592,0.00007113714,0.0002811122,0.0002230271,0.0005816377,0.0003127088,0.0002855296],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0001542957,"about_ca_system_score_gemma":0.0002881605,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.0009887952,"about_ca_topic_score_gemma":0.001980489,"domain_scores_codex":[0.9999268,0.00001470858,0.000002068859,0.00001480433,0.00002096704,0.00002061972],"domain_scores_gemma":[0.9997258,0.00005690487,0.00005032203,0.00004897985,0.00005010768,0.00006797371],"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":[0.001731156,0.0002966763,0.005527377,0.000124762,0.00005242084,0.001140065,0.0005824838,0.07745022,0.8345276,0.004897265,0.002388003,0.07128199],"study_design_scores_gemma":[0.0003100241,0.005318216,0.01764941,0.00002958912,0.00004670128,0.0003946443,0.0003324009,0.8076773,0.1545877,0.001251181,0.01232749,0.00007546996],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.9328462,0.00004593129,0.06033912,0.0001520933,0.0001214147,0.0000445836,0.00004790454,0.0005129452,0.005889851],"genre_scores_gemma":[0.9943029,0.000009240987,0.004044185,0.00001506505,0.000004379833,0.00001772074,0.00001762699,0.00001345175,0.001575533],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.00152697,"threshold_uncertainty_score":0.005108237,"prediction_status":"machine_predicted_unvalidated"},"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,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"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","authors":[{"name":"Gefei Shi","is_ca":false},{"name":"Zheng Zhu","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.003971434670809477,"gpt":0.1857981663394294,"spread":0.1818267316686199,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001664636,0.0002576033,0.0004065343,0.0002012022,0.0008637256,0.0004185963,0.0006051392,0.0003388156,0.0016511],"category_scores_gemma":[0.0003065992,0.0001392551,0.000259693,0.000250878,0.0002989689,0.0005867349,0.0005338427,0.0002652849,0.0002172824],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0001984968,"about_ca_system_score_gemma":0.0003612366,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.002641372,"about_ca_topic_score_gemma":0.001600293,"domain_scores_codex":[0.9998362,0.00002350771,0.000006300822,0.00005025717,0.00004581072,0.00003786237],"domain_scores_gemma":[0.9998926,0.00002006699,0.00001427877,0.00002193274,0.00003294849,0.00001816326],"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":[0.002720359,0.0001767191,0.02803949,0.0003565985,0.0001026898,0.003398011,0.002478116,0.3796635,0.3619254,0.02007658,0.004907995,0.1961546],"study_design_scores_gemma":[0.00005141562,0.0006902489,0.009721092,0.00001966286,0.00009639473,0.0009633997,0.001226846,0.9254832,0.05506349,0.001974483,0.004649114,0.00006076386],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.8933455,0.0002280565,0.09568673,0.0001416533,0.0001112416,0.00001937811,0.00004672056,0.0003127033,0.01010795],"genre_scores_gemma":[0.9934326,0.00004774371,0.003587151,0.000008524366,0.000008425343,0.00000465729,0.00002751229,0.00001492462,0.002868579],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.002641372,"threshold_uncertainty_score":0.005523503,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"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,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"York University","funders":"","keywords":"Calibration; Line (geometry); Environmental science; Element (criminal law); Remote sensing; Geology; Mathematics; Statistics; Geometry","authors":[{"name":"Yuan Ren","is_ca":true},{"name":"Jinjun Shan","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.02763854529454853,"gpt":0.2880872221004843,"spread":0.2604486768059358,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004190107,0.0006439399,0.000405356,0.0006290711,0.0004473094,0.0004605045,0.001097171,0.0008229272,0.0009718006],"category_scores_gemma":[0.001083426,0.0003690012,0.0005609898,0.0008340719,0.0002016611,0.0009163277,0.0004636905,0.0006979503,0.0008390309],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.000595795,"about_ca_system_score_gemma":0.0007085226,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.01250704,"about_ca_topic_score_gemma":0.009895456,"domain_scores_codex":[0.9996724,0.00004355457,0.00001114785,0.0001313524,0.0001080464,0.00003345457],"domain_scores_gemma":[0.999671,0.0000515018,0.00002802503,0.0001010964,0.0001222073,0.00002622372],"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":[0.0004806623,0.0004220136,0.2133332,0.0002775425,0.0003495281,0.0003442743,0.0005329428,0.5281081,0.1166377,0.005509132,0.008807028,0.1251979],"study_design_scores_gemma":[0.0001219015,0.00004782131,0.08422942,0.00002425189,0.00008413048,0.000100883,0.00006244384,0.8869036,0.02156237,0.001775928,0.00502259,0.00006462884],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.7165551,0.0004998948,0.2579236,0.0003969463,0.0003036419,0.0001524728,0.005829593,0.007008972,0.01132987],"genre_scores_gemma":[0.954201,0.0001445682,0.04137824,0.00006441083,0.00002578705,0.00007489001,0.003049018,0.0002424644,0.0008196075],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.01250704,"threshold_uncertainty_score":0.02486849,"prediction_status":"machine_predicted_unvalidated"},"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,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"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","authors":[{"name":"Jun Yang Li","is_ca":true},{"name":"M. Reza Emami","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.004454323153669872,"gpt":0.208135113655453,"spread":0.2036807905017831,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005313394,0.0009459695,0.001046308,0.001249235,0.0007011453,0.001024558,0.001426451,0.001021438,0.004130464],"category_scores_gemma":[0.002102128,0.0007873133,0.001078585,0.001179251,0.001621544,0.001464238,0.002147742,0.001504163,0.0005585129],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.000826186,"about_ca_system_score_gemma":0.00100197,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.005337269,"about_ca_topic_score_gemma":0.004912251,"domain_scores_codex":[0.9995209,0.0001363218,0.00002257389,0.0001081226,0.0001739953,0.00003821426],"domain_scores_gemma":[0.9996137,0.0002030979,0.00004616534,0.0000380145,0.00007765067,0.00002136703],"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":[0.0000208552,0.00001746972,0.0001123537,0.00005015567,0.00001984046,0.0000442356,0.00006145687,0.8132814,0.001000977,0.1543587,0.001132508,0.02990017],"study_design_scores_gemma":[0.000006885726,0.00003637373,0.00007561471,0.00001021289,0.000007215842,0.00002396235,0.00001811124,0.9134308,0.0003130764,0.08342325,0.002644093,0.00001041463],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":null,"genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.001336495,0.0001385349,0.9955044,0.0001119448,0.00004045683,0.00001290075,0.00002032153,0.00005362666,0.002781331],"genre_scores_gemma":[0.4445774,0.001351839,0.5419406,0.0001901657,0.000321325,0.0002525783,0.0002205905,0.0002697143,0.01087582],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.005337269,"threshold_uncertainty_score":0.01381773,"prediction_status":"machine_predicted_unvalidated"},"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,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"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)","authors":[{"name":"Basel A. M. Omran","is_ca":false},{"name":"Michael C.F. Bazzocchi","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.005991320499227445,"gpt":0.201647958388649,"spread":0.1956566378894215,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002250933,0.0003576227,0.0003398899,0.0002372257,0.0002886628,0.0004915941,0.0002712847,0.0004694864,0.001694261],"category_scores_gemma":[0.000701544,0.0002707932,0.0003119718,0.0003559157,0.0002956959,0.0002990476,0.0003989458,0.0003676267,0.0002770664],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0005323992,"about_ca_system_score_gemma":0.0008666443,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.006724799,"about_ca_topic_score_gemma":0.006204396,"domain_scores_codex":[0.9999248,0.00001844802,0.0000019202,0.00001178949,0.00002668395,0.00001641727],"domain_scores_gemma":[0.9998618,0.00005528357,0.0000237896,0.000007769273,0.0000394338,0.00001177767],"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":[0.00003270254,0.000008803223,0.0003724504,0.00001662938,0.000008698224,0.00001942302,0.00002621853,0.9898908,0.001601502,0.001334958,0.000201521,0.006486205],"study_design_scores_gemma":[0.00000840035,0.00005087188,0.0002988352,0.000003341409,0.000004421999,0.000007334151,0.00003398063,0.9979476,0.0006578913,0.0005862433,0.0003985199,0.000002609455],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.3145242,0.0003620218,0.6602787,0.0005200228,0.00004987762,0.00008135239,0.0001924723,0.0002253691,0.02376604],"genre_scores_gemma":[0.9597024,0.0001469488,0.03578844,0.0000343782,0.00001262628,0.00007493974,0.0001000041,0.00004944724,0.004090894],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.006724799,"threshold_uncertainty_score":0.01337135,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null}]}