{"meta":{"query_hash":"00b1af9f5bfa","filters":{"venue":"International Journal of Aerospace System Science and Engineering"},"cohort_total":2,"direct_labels_cover":0,"predictions_cover":2,"exported":2,"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/00b1af9f5bfa","api":"https://metacan.xera.ac/api/v1/cohort?venue=International+Journal+of+Aerospace+System+Science+and+Engineering"},"results":[{"id":"W3137833708","doi":"10.1504/ijasse.2021.10036566","title":"Rotation vector and directional cosine matrix in problems of satellite attitude control","year":2021,"lang":"en","type":"article","venue":"International Journal of Aerospace System Science and Engineering","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":2,"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":"","keywords":"Trigonometric functions; Rotation matrix; Satellite; Matrix (chemical analysis); Rotation (mathematics); Direction cosine; Mathematics; Attitude control; Control (management); Computer science; Artificial intelligence; Physics; Engineering; Astronomy; Geometry; Control engineering; Materials science","score_opus":0.0034398311691432536,"score_gpt":0.20130805039147354,"score_spread":0.19786821922233028,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3137833708","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":[0.93729675,0.007845276,0.052530937,0.00022880526,0.0017705208,0.00012558537,0.000009443621,0.00005963158,0.00013303003],"genre_scores_gemma":[0.9984451,0.00029688774,0.0010831013,0.0000030227513,0.00014228164,0.000004962744,5.903957e-7,0.000013370933,0.000010708675],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987517,0.000012029452,0.0004146545,0.00012078747,0.0005349098,0.00016591555],"domain_scores_gemma":[0.99916136,0.00006893207,0.00010592974,0.00006703213,0.00050582265,0.000090910835],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006505871,0.000120241755,0.00026602377,0.00026065952,0.00002238953,0.00008825348,0.0001379859,0.00004446088,0.0000012763015],"category_scores_gemma":[0.000113189904,0.00011613273,0.00003719193,0.00031217939,0.000043514887,0.00036733353,0.000020679343,0.00013416458,5.9345746e-7],"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":[0.000014992802,0.000014782721,0.0094831465,0.00030817807,0.00009010904,0.000040930947,0.0004187759,0.5303568,0.45714068,0.0010860838,0.0000065124214,0.0010389653],"study_design_scores_gemma":[0.004330677,0.00015782149,0.20525077,0.0048639476,0.000054441825,0.002206683,0.0011168451,0.7451021,0.03533232,0.000016892925,0.0009888457,0.0005786386],"about_ca_topic_score_codex":0.000016255868,"about_ca_topic_score_gemma":0.000012054216,"teacher_disagreement_score":0.42180836,"about_ca_system_score_codex":0.00020083577,"about_ca_system_score_gemma":0.000064894804,"threshold_uncertainty_score":0.47357553},"labels":[],"label_agreement":null},{"id":"W4246155320","doi":"10.1504/ijasse.2021.114118","title":"Design and implementation of low-power low-cost quasi steady-state magnetoplasmadynamic propulsion using Ar-He and N&lt;SUB align=\"right\"&gt;2-He gas mixtures","year":2021,"lang":"en","type":"article","venue":"International Journal of Aerospace System Science and Engineering","topic":"Solar and Space Plasma Dynamics","field":"Physics and Astronomy","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"York University","funders":"York University","keywords":"Propulsion; Steady state (chemistry); Power (physics); Nuclear engineering; Chemistry; State (computer science); Materials science; Physics; Thermodynamics; Engineering; Computer science; Physical chemistry","score_opus":0.005058376984639479,"score_gpt":0.23544107968531194,"score_spread":0.23038270270067246,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4246155320","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":[0.88189924,0.0001319185,0.117248476,0.000117633215,0.0004488519,0.00011828182,0.000013474732,0.000005893385,0.000016246377],"genre_scores_gemma":[0.9952141,0.000035039062,0.004656101,0.0000053497147,0.000058413378,0.0000022204856,0.0000026524947,0.000011302477,0.000014793706],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987437,0.000028633549,0.00034263247,0.00018437006,0.0005068641,0.00019381315],"domain_scores_gemma":[0.99895644,0.000062536674,0.00026232016,0.00007532084,0.00053035043,0.000113048955],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00054100197,0.00014350362,0.00021052903,0.00018255225,0.00009567179,0.00027089124,0.00014112066,0.000027308879,0.0000068391078],"category_scores_gemma":[0.000017322329,0.0001240095,0.00003985125,0.0001781041,0.00007613618,0.000639323,0.0000729968,0.00011565253,3.6882753e-7],"study_design_candidate":"bench_or_experimental","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":[0.000040736668,0.000043890064,0.012967246,0.00013340433,0.00014913436,0.000042983287,0.0016292302,0.04077229,0.9406406,0.0009885363,0.000026036018,0.0025658766],"study_design_scores_gemma":[0.001876295,0.00018716171,0.01057238,0.0013885424,0.00009620825,0.00070230674,0.0058563002,0.70694816,0.2717509,0.00013150815,0.000051290917,0.00043898428],"about_ca_topic_score_codex":0.000034391327,"about_ca_topic_score_gemma":0.000010001335,"teacher_disagreement_score":0.66888976,"about_ca_system_score_codex":0.000091707705,"about_ca_system_score_gemma":0.00015503586,"threshold_uncertainty_score":0.50569606},"labels":[],"label_agreement":null}]}