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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
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.
CAI Zongping , CHEN Qi , MA Qingliang , CAO Chuangfeng , YIN Xiaojing . Guaranteed Cost Controller Design of Spacecraft Wide Angle Attitude Maneuver Based on Sum-of-squares Optimization[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2013 , 33(1) : 39 -43 . DOI: 10.15892/j.cnki.djzdxb.2013.01.015
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