{"title":"巡航导弹飞行动力学","authors":"А.Д. Донской, С.Е. Сабо, М.А. Щиканов","doi":"10.21499/2409-1650-2021-27-1-30-40","DOIUrl":null,"url":null,"abstract":"Рассматривается система уравнений динамики полета крылатой ракеты с учетом всех факторов воздействия на ее движение в атмосфере.\n A system of equations for the dynamics of a cruise missile flight is considered, taking into account all factors affecting its movement in the atmosphere.","PeriodicalId":424160,"journal":{"name":"Informacionno-technologicheskij vestnik","volume":"22 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2021-03-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Dynamics of cruise missile flight\",\"authors\":\"А.Д. Донской, С.Е. Сабо, М.А. Щиканов\",\"doi\":\"10.21499/2409-1650-2021-27-1-30-40\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Рассматривается система уравнений динамики полета крылатой ракеты с учетом всех факторов воздействия на ее движение в атмосфере.\\n A system of equations for the dynamics of a cruise missile flight is considered, taking into account all factors affecting its movement in the atmosphere.\",\"PeriodicalId\":424160,\"journal\":{\"name\":\"Informacionno-technologicheskij vestnik\",\"volume\":\"22 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2021-03-15\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Informacionno-technologicheskij vestnik\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.21499/2409-1650-2021-27-1-30-40\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Informacionno-technologicheskij vestnik","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.21499/2409-1650-2021-27-1-30-40","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Рассматривается система уравнений динамики полета крылатой ракеты с учетом всех факторов воздействия на ее движение в атмосфере.
A system of equations for the dynamics of a cruise missile flight is considered, taking into account all factors affecting its movement in the atmosphere.
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