摘要
讨论了为实现导引规律,将某些有关质心运动的参数由描写姿态运动的参数来代替,从而解决了某些控制设备不能测量质心运动参数的困难,简化了控制系统。经理论推导与仿真,证明此方法是可行的。
Some parameters related to mass-center motion which can be replaced by parameters describing attitude motion to implement a guidance law are discussed. The difficulty in certain case is resolved, concerning some control device incapable of measuring mass-center motion, and control system is simplified. The feasibility of the new method is proved by means of theoretical derivation and mathematical simulation
出处
《战术导弹技术》
1998年第3期33-36,共4页
Tactical Missile Technology
