导弹与制导技术

基于平方和优化的飞行器大角度姿态机动保性能控制器设计

  • 蔡宗平 ,
  • 陈琦 ,
  • 马清亮 ,
  • 曹创锋 ,
  • 殷小静
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  • 1 第二炮兵工程大学控制工程系, 西安 710025
    2 96121部队, 辽宁盘锦 124000
    3 96616部队, 北京 100000

蔡宗平(1964-),男,陕西岐山人,教授,硕士研究生导师,研究方向:制导与控制。

收稿日期: 2012-05-14

  网络出版日期: 2025-05-24

Guaranteed Cost Controller Design of Spacecraft Wide Angle Attitude Maneuver Based on Sum-of-squares Optimization

  • CAI Zongping ,
  • CHEN Qi ,
  • MA Qingliang ,
  • CAO Chuangfeng ,
  • YIN Xiaojing
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  • 1 Department of Control Engineering, The Second Artillery Engineering University, Xi' an 710025, China
    2 No. 96121 Unit, Liaoning Panjin 124000, China
    3 No. 96616 Unit, Beijing100000, China

Received date: 2012-05-14

  Online published: 2025-05-24

摘要

研究飞行器大角度姿态机动状态反馈保性能控制器设计问题。采用修正的Rodrigues参数建立了飞行器姿态控制运动模型,将非线性的飞行器姿态系统模型转化为线性参数可变模型(LPV模型)。将平方和优化技术和Lyapunov理论相结合,给出了飞行器大角度姿态机动保性能控制器设计方法。仿真结果表明了所提方法的有效性。

本文引用格式

蔡宗平 , 陈琦 , 马清亮 , 曹创锋 , 殷小静 . 基于平方和优化的飞行器大角度姿态机动保性能控制器设计[J]. 弹箭与制导学报, 2013 , 33(1) : 39 -43 . DOI: 10.15892/j.cnki.djzdxb.2013.01.015

Abstract

The problem of state feedback guaranteed controller design for large angle attitude maneuver was investigated. By using modified Rodrigues parameters, the attitude dynamics of the spacecraft was represented in terms of linear parameter varying (LPV) systems. The state feedback guaranteed cost controller design approach was proposed by combining Lyapunov theory and sum of squares (SOS) optimization. Simulation results demonstrate the effectiveness of the proposed design approach.

参考文献

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