摘要
针对防空导弹大攻角飞行这样一个非线形、时变、耦合系统,提出了一种基于模型参考时变全程滑态变结构控制方法,分别针对滚动通道、俯仰/偏航耦合通道进行了设计分析,最后进行了六自由度仿真,得到了满意的结果。
Based on the time-varying sliding-mode variable structure control theory, a new design method for the nonlinear, time-varying and coupling system of flying phrase with large angle of attack is proposed. Design for roll channel and pitch/yaw coupling channel is also analyzed respectively. Finally, the 6-DOF simulation results prove the outstanding feature of this design.
出处
《航天控制》
CSCD
北大核心
2006年第2期14-16,21,共4页
Aerospace Control
关键词
变结构控制
大攻角飞行
六自由度仿真
Variable structure control Large angle-of-attack flying Six-degree of freedom simulation
