{"title":"设计并测试了飞行模型在单一修正平面中平衡时主质心惯性轴偏差角最小的算法","authors":"A. V. Klyuchnikov","doi":"10.31772/2587-6066-2020-21-1-70-77","DOIUrl":null,"url":null,"abstract":"","PeriodicalId":156619,"journal":{"name":"Siberian Journal of Science and Technology","volume":"46 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"ELABORATION AND TESTING OF THE ALGORITHM WHICH ENSURES AN ACHIEVEMENT OF MINIMAL DEVIATION ANGLE OF FLYING MODEL’S MAIN CENTROIDAL AXIS OF INERTIA DURING HER COUNTERBALANCING IN A SOLE CORRECTION FLATNESS\",\"authors\":\"A. V. Klyuchnikov\",\"doi\":\"10.31772/2587-6066-2020-21-1-70-77\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"\",\"PeriodicalId\":156619,\"journal\":{\"name\":\"Siberian Journal of Science and Technology\",\"volume\":\"46 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1900-01-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Siberian Journal of Science and Technology\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.31772/2587-6066-2020-21-1-70-77\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Siberian Journal of Science and Technology","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.31772/2587-6066-2020-21-1-70-77","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
ELABORATION AND TESTING OF THE ALGORITHM WHICH ENSURES AN ACHIEVEMENT OF MINIMAL DEVIATION ANGLE OF FLYING MODEL’S MAIN CENTROIDAL AXIS OF INERTIA DURING HER COUNTERBALANCING IN A SOLE CORRECTION FLATNESS