Adaptive Backstepping Control for Spacecraft Rendezvous on Elliptical Orbits Based on Transformed Variables Model

被引：8

作者：

Wang, Yu ^{[1
]}

Li, Kun ^{[1
]}

Yang, Kaihong ^{[1
]}

Ji, Haibo ^{[1
]}

机构：

[1] Univ Sci & Technol China, Dept Automat, Hefei 230026, Anhui, Peoples R China

来源：

INTERNATIONAL JOURNAL OF CONTROL AUTOMATION AND SYSTEMS | 2018年 / 16卷 / 01期

基金：

中国国家自然科学基金;

关键词：

Adaptive control; backstepping control; spacecraft rendezvous; transformed variables; SYSTEMS;

D O I：

10.1007/s12555-016-0696-0

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

This paper investigates the problem of relative motion control for spacecraft rendezvous on an arbitrary elliptical orbit. The simplified dynamic model describing the relative motion between the chaser spacecraft and the target spacecraft is established via using transformed variables. Due to the presence of time variant parameters in this novel model, robust control scheme and adaptive control scheme are designed to solve the rendezvous problem. Theoretical analyses and simulation results demonstrate the effectiveness of the proposed methods.

引用

页码：189 / 196

页数：8

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