4.6 Article

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

期刊

ACTA ASTRONAUTICA
卷 127, 期 -, 页码 226-234

出版社

PERGAMON-ELSEVIER SCIENCE LTD
DOI: 10.1016/j.actaastro.2016.05.019

关键词

Solar power satellite; Space solar power station; Attitude dynamics; Optimal control; LQR

资金

  1. National Natural Science Foundation of China [11502040, 11432010]
  2. Fundamental Research Funds for the Central Universities [DUT15LK31]

向作者/读者索取更多资源

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.

作者

我是这篇论文的作者
点击您的名字以认领此论文并将其添加到您的个人资料中。

评论

主要评分

4.6
评分不足

次要评分

新颖性
-
重要性
-
科学严谨性
-
评价这篇论文

推荐

暂无数据
暂无数据