| 275 | 20 | 26 |
| Downloads | Citas | Reads |
Simulation analysis is taken for guidance control system of mass moment missile. First, simulation model is given. Second, analysis is done for the guidance control system of mass moment missile. Finally, analysis is made briefly by simulation for the interception miss distance.
[1] RaymondH .Byrne,R .R .Sturgis,R .D .Robinett.AMovingMassTrimControlSystemForRe entryVehicleGuidance[R].AIAA 963438CP .
[2] 周凤岐,等.弹道式导弹弹头变质心机动控制[J].宇航学报,2000,Vol21.
[3] 彭冠一,等.防空导弹武器系统制导控制系统设计(上)[M].北京:宇航出版社,1996.
[4] 张友安,胡云安.导弹控制和制导的非线性设计方法[M].北京:国防工业出版社,2003.
Basic Information:
DOI:10.16358/j.issn.1009-1300.2004.05.013
China Classification Code:TJ765.43
Citation Information:
[1]Liao Guobin, Yang Yuguang, Wang Lili (P.O.Box 3922, Beijing 100854, China).Simulation Research for Guidance-control System of Mass Moment Missile[J].Tactical Missile Technology,2004(05):49-53.DOI:10.16358/j.issn.1009-1300.2004.05.013.
2004-09-15
2004-09-15