大空域机动反舰导弹纵向通道姿态控制指令设计  

Control Instruction Design for Large Airspace Maneuvering Anti-ship Missile Longitudinal Channel Attitude Control

作　　者：李聪颖[1] 顾文锦[1] 

机构地区：[1]海军航空工程学院,山东烟台264001

出　　处：《弹箭与制导学报》2003年第3期1-3,共3页Journal of Projectiles,Rockets,Missiles and Guidance

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.

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 

分 类 号：TJ761.14[兵器科学与技术—武器系统与运用工程] TJ765.23