Robust optimal sun-pointing control of a large solar power satellite

被引:27
|
作者
Wu, Shunan [1 ]
Zhang, Kaiming [1 ]
Peng, Haijun [2 ]
Wu, Zhigang [1 ]
Radice, Gianmarco [3 ]
机构
[1] Dalian Univ Technol, Sch Aeronaut & Astronaut, Dalian 116024, Peoples R China
[2] Dalian Univ Technol, Dept Engn Mech, Dalian 116024, Peoples R China
[3] Univ Glasgow, Sch Engn, Glasgow G12 8QQ, Lanark, Scotland
基金
中国国家自然科学基金;
关键词
Solar power satellite; Space solar power station; Attitude dynamics; Optimal control; LQR; ATTITUDE;
D O I
10.1016/j.actaastro.2016.05.019
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The robust optimal sun-pointing control strategy for a large geostationary solar power satellite (SPS) is addressed in this paper. The SPS is considered as a huge rigid body, and the sun-pointing dynamics are firstly proposed in the state space representation. The perturbation effects caused by gravity gradient, solar radiation pressure and microwave reaction are investigated. To perform sun-pointing maneuvers, a periodically time-varying robust optimal LQR controller is designed to assess the pointing accuracy and the control inputs. It should be noted that, to reduce the pointing errors, the disturbance rejection technique is combined into the proposed LQR controller. A recursive algorithm is then proposed to solve the optimal LQR control gain. Simulation results are finally provided to, illustrate the performance of the proposed closed-loop system. (C) 2016 IAA. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:226 / 234
页数:9
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