卫星单轴太阳翼驱动系统建模与控制技术综述

李朋; 许瑞栋; 张家腾; 高智刚; 周军

doi:doi:10.19912/j.0254-0096.tynxb.2024-1172

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卫星单轴太阳翼驱动系统建模与控制技术综述

更新时间：2025-12-02

- 卫星单轴太阳翼驱动系统建模与控制技术综述
- Vol. 46, Issue 6, Pages: 142-151(2025)
- 作者机构：
- 作者简介：
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- DOI：doi:10.19912/j.0254-0096.tynxb.2024-1172
  CLC： TM921
- Published Online：07 July 2025，
  
  Published：2025
- 稿件说明：
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李朋, 许瑞栋, 张家腾, et al. 卫星单轴太阳翼驱动系统建模与控制技术综述[J]. 2025, 46(6): 142-151.
DOI：

李朋, 许瑞栋, 张家腾, et al. 卫星单轴太阳翼驱动系统建模与控制技术综述[J]. 2025, 46(6): 142-151. DOI： doi:10.19912/j.0254-0096.tynxb.2024-1172.

摘要

针对目前卫星单轴太阳翼驱动系统面临的复杂问题

从系统建模、控制方法及地面验证等多角度全面梳理国内外的技术进展。首先分析太阳翼驱动系统的结构、原理和工作模式;进而针对其负载特性分别总结刚性和柔性太阳翼的动力学建模方法

并针对非线性所带来的转速和角度控制难点探讨单一控制和复合控制策略

对各类算法作对比分析;然后介绍为提高地面试验验证的准确性所采用的微重力模拟和负载特性模拟方法。对未来航天器太阳翼驱动系统的研究动向进行总结与展望。

Abstract

In view of the complex problems currently faced by the satellite single-axis solar array drive system

the technological progress at home and abroad is comprehensively reviewed from multiple perspectives such as system modeling

control methods and ground verification. Firstly

the structure

operation principle and working mode of SADA are analyzed. Then

according to the load characteristics of SADA

the dynamic modeling methods of rigid and flexible solar wings are summarized

and the single control and composite control strategies are discussed for the difficulties of speed and angle control caused by nonlinearity

and various algorithms are compared and analyzed. Also

the microgravity simulation and load characteristic simulation methods adopted to improve the accuracy of SADA ground test verification are introduced. Finally

the research trend of future spacecraft SADA is summarized and prospected.

关键词

Keywords

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