摘要
讨论了空间飞行器大角度机动控制实验平台的实现方法,并给出了硬件结构原理和软件的设计流程。采用相平面法,设计了基于喷气系统的大角度姿态机动控制器,并进行了不同角度下的闭环姿态机动控制实验。
This article discusses the implementation method of experimental platform for spacecraft large-angle maneuver control. The hardware structural principle and the process of software design are given out. Then, the spacecraft large-angle maneuver controller, which is based on the gas injection system, is designed by using the control algorithm of phase-plane method. Furthermore,the experiments of closed loop attitude maneuver control are carried out, which are under different angles.
出处
《实验技术与管理》
CAS
北大核心
2009年第2期34-36,42,共4页
Experimental Technology and Management
基金
国防重点专业建设项目
关键词
大角度机动控制
喷气系统
DSP
相平面控制
large-angle maneuver control
gas injection system
DSP
phase-plane control