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
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
Received date: 2012-05-14
Online published: 2025-05-24
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
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.
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