摘要
本文介绍了球载硬Ｘ射线空间高能天文望远镜ＨＡＰＩ－４系统探测器平台即吊舱系统的状态空间模型。线性二次型最优控制器ＬＱＲ的设计方法及仿真结果，这些结果也可推广到其他似的球载升空平台，仿真结果表明，引入高性能控制算法可以大幅度改善控制系统的性能。
This paper introduces the state-space model of the detecting platform of the balloon-borne hard X-ray astronomical telescope HAPI-4 system. and its LQR designing method. simulating results. These results can also be used in other similar balloon-borne space platform. The simulating results indicate that the property of the control system will be greatly improved by using much effective controlling method.
出处
《计算机仿真》
CSCD
1998年第1期45-48,共4页
Computer Simulation
