宇航学报 ›› 2020, Vol. 41 ›› Issue (6): 633-646.doi: 10.3873/j.issn.1000-1328.2020.06.001

• 综述 • 上一篇    下一篇

飞行器控制的伪线性系统方法——第一部分:综述与问题

段广仁   

  1. 哈尔滨工业大学控制理论与制导技术研究中心,哈尔滨 150001
  • 收稿日期:2020-03-15 修回日期:2020-05-10 出版日期:2020-06-15 发布日期:2020-06-25
  • 基金资助:
    国家自然科学基金重大项目(61690210,61690212);国家自然科学基金(61333003);机器人与系统国家重点实验室自主计划任务(HIT)(SKLRS201716A)

Quasi Linear System Approaches for Flight Vehicle Control——Part 1: An Overview and Problems

DUAN Guang ren   

  1. Center for Control Theory and Guidance Technology, Harbin Institute of Technology, Harbin 150001, China
  • Received:2020-03-15 Revised:2020-05-10 Online:2020-06-15 Published:2020-06-25

摘要: 首先将非线性控制方法归纳成三类:基于李雅普诺夫泛函的设计方法、基于最优控制思想的设计方法和以线性为主导的设计方法,并对此三类方法进行了简略的综述。然后进一步在此类划分的框架下概述了飞行器控制的非线性方法,并引入了伪线性系统的概念。最后介绍了卫星姿态与轨道控制、飞行器制导与控制中的六类典型飞行器控制问题的二阶伪线性系统描述。

关键词: 飞行器控制, 伪线性系统, 姿态控制, 轨道控制, 空间交会与拦截

Abstract: This paper firstly classifies the nonlinear control approaches into three categories: the approaches based on Lyapunov function selection, the approaches based on optimal control schemes, and the approaches based on linear approximation and domination, and gives a brief overview on each category. Along with this classification, an overview on the nonlinear flight control approaches is also provided, and the concept of quasi-linear systems is then introduced. Finally, the second-order quasi-linear system descriptions of six typical control problems arising from the fields of satellite attitude and orbit control as well as vehicle guidance and control are provided.

Key words: Flight vehicle control, Quasi-linear systems, Attitude control, Orbit control, Space rendezvous and interception

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