巡航导弹飞行动力学

А.Д. Донской, С.Е. Сабо, М.А. Щиканов
{"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}
引用次数: 0
查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
Dynamics of cruise missile flight
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.
求助全文
通过发布文献求助,成功后即可免费获取论文全文。 去求助
来源期刊
自引率
0.00%
发文量
0
期刊最新文献
Assessment of the Readiness of the Equipment of the Launch Space Complex at the Early Stages of its Creation The accuracy of measuring the information parameter of the signal by a tracking meter in aviation and rocket and space technology against the background of additive and multiplicative interference. Measurement of arrival time. Part III Problems of multiple use of liquid rocket propulsion systems Multiple sun-synchronous orbits for full coverage of the Earth Numerical and expert-oriented method of choosing the parameters of Sun-synchronous orbits for wide-scale monitoring Northern Russia regions
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 联系我们:info@booksci.cn
Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。
Copyright © 2023 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1