摘要
以大气层内反导导弹为研究目的,分析了直接力与气动力复合控制的必要性,给出了复合控制系统的控制模型,实现了对气动力和姿控直接力两个子系统的设计,并通过大量数字仿真实现对复合控制系统设计的合理性进行了验证。结果表明,复合控制系统较纯气动力控制系统的指令响应速度有较大提高。
The necessity of compound control of direct force and aerodynamics aiming at inner aerospace ATBM missile is analyzed. The model of compound control system is given. Double subsystems of aerodynamics and attitude direct force are designed, and the compound control system is validated by figure simulation. The design of the compound control system has higher injunction respond speed than aerodynamic control system.
出处
《现代防御技术》
北大核心
2010年第2期41-45,共5页
Modern Defence Technology
关键词
反导导弹
姿控直接力
复合控制
ATBM-missile
attitude control direct lateral force
compound control
