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。采用轨迹跟踪PD控制算法,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 discussed the implementation method of experimental platform for spacecraft large-angle maneuver control. The hardware structural principle and the process of software design were given out. The spacecraft large-angle maneuver controller, which is based on the gas injection system, was designed by using the control algorithm of trajectory tracking and PD control. Furthermore,the experiments of closed loop attitude maneuver control under different angles were carried out.
出处
《实验室研究与探索》
CAS
2008年第1期22-25,共4页
Research and Exploration In Laboratory
基金
国防重点专业建设项目
关键词
大角度机动
喷气系统
DSP
轨迹跟踪
large-angle maneuver
gas injection system
DSP
trajectory tracking
