摘要
针对基于姿态控制的导弹控制系统,设计了纵向通道的控制指令,并在VC++6.0下进行了全弹道仿真。仿真结果表明,所设计的控制指令能够保证导弹完成大空域内的机动飞行。
For missile control system based on attitude control, lognitudinal control instructions were designed, whole trajectory simulation conducted in VC++6.0 Simulation shows that control instructions designed can ensure the maneuver flight in large airspace.
出处
《弹箭与制导学报》
CSCD
北大核心
2003年第3期1-3,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
大空域机动
反舰导弹
纵向通道
姿态控制
控制指令
设计
anti-ship missile
large airspace maneuvering
lognitudinal channel
control instruction design
