J4 ›› 2015, Vol. 42 ›› Issue (5): 207-212.doi: 10.3969/j.issn.1001-2400.2015.05.034

• 研究论文 • 上一篇    

干扰抑制SDRE姿态控制方法

张银辉;杨华波;江振宇;张为华   

  1. (国防科学技术大学 航天科学与工程学院,湖南 长沙  410073)
  • 收稿日期:2015-05-06 出版日期:2015-10-20 发布日期:2015-12-03
  • 通讯作者: 张银辉
  • 作者简介:张银辉(1986-),男,国防科学技术大学博士研究生,E-mail: zhangyinhui_nudt@163.com.
  • 基金资助:

    国家自然科学基金资助项目(51105368)

Disturbance rejection SDRE attitude control

ZHANG Yinhui;YANG Huabo;JIANG Zhenyu;ZHANG Weihua   

  1. (College of Aerospace Science and Eng., National Univ. of Defense Tech., Changsha  410073, China)
  • Received:2015-05-06 Online:2015-10-20 Published:2015-12-03
  • Contact: ZHANG Yinhui

摘要:

针对导弹姿态控制面临的非线性、参数不确定与外界干扰等问题,研究基于非线性干扰观测器的干扰抑制状态相关的黎卡提方程姿态控制方法.首先,引入总干扰概念,将参数不确定与外界干扰等因素对系统的影响统一看作系统总干扰; 然后,通过设计总干扰补偿系数,实现具有非匹配干扰抑制能力的状态相关的黎卡提方程姿态控制系统设计; 最后,利用非线性干扰观测器得到系统总干扰的估计值.仿真结果表明,所设计的姿态控制方法能够有效跟踪期望攻角指令,同时对系统参数不确定与外界干扰具有较强的抑制能力.

关键词: 非线性干扰观测器, 状态相关的黎卡提方程, 姿态控制, 干扰抑制

Abstract:

The nonlinear disturbance observer based disturbance rejection SDRE attitude control is investigated for a general nonlinear missile with parameter uncertainties and external disturbances. Firstly, the total effects of the parameter uncertainties and external disturbances are regarded as the lumped disturbances. And then, a disturbance compensation gain is carefully designed, so that the disturbance rejection SDRE attitude control method is able to address the mismatched disturbances. Finally, the nonlinear disturbance observer is introduced to estimate the lumped disturbances. Simulation results have demonstrated the precise tracking performance and the disturbance rejection capability of the proposed method with respect to the parameter uncertainties and external disturbances.

Key words: nonlinear disturbance observer, state-dependent riccati equation(SDRE), attitude control, disturbance rejection

中图分类号: 

  • V448