摘要
作为多用途的靶弹 ,必须在大空域平飞 .针对研究对象 ,在高度控制系统设计中 ,引入多目标多约束的随机射线优化方法 .在约束条件一定的情况下 ,合理选择俯仰角稳定回路和高度稳定回路控制参数以及各种程序指令信号的大小和工作时间 ,使得靶弹的上升时间最短 ,超调量接近于零 .全弹道仿真结果表明 ,用这种优化方法所设计的高度控制系统能成功实现所要求的大空域平飞 .
Multirole target must horizontally fly over large air area.Based on the research object,the random radiation optimization of multitargets and multi-restrictions is introduced into the design of altitude control system.Under the condition that restrictions are given,azimuth angle stability loop and altitude stability loop control parameters,the size of various program command signal and working time are chosen reasonably so as to minimize the lifting time of target,and overshoot approximate to zero.All trajectory simulation results show that the designed altitude control system can achieve the object of flight over large airspace by the proposed method.
出处
《战术导弹技术》
2004年第3期51-53,46,共4页
Tactical Missile Technology
关键词
靶弹
高度控制系统
优化设计
目标函数
上升时间
target missile
altitude control system
optimization design
objective function
lifting time