摘要
在推导三通道稳定再入飞行器动力学方程的基础上,运用动态逆控制理论设计了三通道稳定模式下变质心再入飞行器的控制系统。仿真结果表明,所设计的控制系统能够有效地调整再入飞行器的飞行姿态并满足设计指标要求。
In this paper, basing on three-axis＇ s stable dynamic equations of moving centroid reentry vehicles, the dynamic inversion controller was designed under three-axis＇ s stable control mode. According to simulating resuit, we consider that the flight attitude can be validly adjusted and the requires of control system design can be performed.
出处
《飞行力学》
CSCD
北大核心
2009年第1期59-62,共4页
Flight Dynamics
基金
国家863计划资助项目(2007AA0137)
关键词
再入飞行器
变质心
姿态控制
动态逆
reentry vehicles
moving centroid
attitude control
dynamic inversion
