基于欧拉角的分导飞行器多模型自适应姿态控制

钟震;段广仁;姜苍华

系统科学与数学 ›› 2008, Vol. 28 ›› Issue (7) : 769-779.

PDF(695 KB)
PDF(695 KB)
系统科学与数学 ›› 2008, Vol. 28 ›› Issue (7) : 769-779. DOI: 10.12341/jssms10210
论文

基于欧拉角的分导飞行器多模型自适应姿态控制

    钟震,段广仁,姜苍华
作者信息 +

Multiple Model Adaptive Control of Post-Boost Vehicles Based on Euler Angles

    ZHONG Zhen, DUAN Guangren, JIANG Canghua
Author information +
文章历史 +

摘要

基于欧拉角的变换得到了刚体飞行器的一种多模型自适应控制律,它能解决转动惯量不确定并随时发生突变的分导飞行器的姿态控制问题.该控制策略可以有效地检测出转动惯量发生突变,并及时切换到最合适的控制器.通过理论分析证明了该控制策略的闭环全局渐近稳定.数值仿真表明该方案的有效性.

Abstract

Based on the transformation of Euler angles, an indirect adaptive control scheme for post-boost vehicles using multiple models and switching is obtained, which can detect the abrupt change of inertia effectively and then switch to the current best controller. Theoretical analysis demonstrates that the overall control system is globally asymptotically stable. A numerical simulation is employed to illustrate the effectiveness of the proposed scheme.

关键词

自适应控制 / 姿态控制 / 多模型 / 切换控制.

Key words

Adaptive control / attitude control / multiple models / switch control.

引用本文

导出引用
钟震 , 段广仁 , 姜苍华. 基于欧拉角的分导飞行器多模型自适应姿态控制. 系统科学与数学, 2008, 28(7): 769-779. https://doi.org/10.12341/jssms10210
ZHONG Zhen , DUAN Guangren , JIANG Canghua. Multiple Model Adaptive Control of Post-Boost Vehicles Based on Euler Angles. Journal of Systems Science and Mathematical Sciences, 2008, 28(7): 769-779 https://doi.org/10.12341/jssms10210
中图分类号: 93C40   
PDF(695 KB)

197

Accesses

0

Citation

Detail

段落导航
相关文章

/