Optimised collision avoidance for an ultra-close rendezvous with a failed satellite based on the Gauss pseudospectral method

被引：46

作者：

Chu, Xiaoyu ^{[1
,3
]}

Zhang, Jingrui ^{[1
,3
]}

Lu, Shan ^{[2
]}

Zhang, Yao ^{[1
,3
]}

Sun, Yue ^{[2
]}

机构：

[1] Beijing Inst Technol, Beijing 100081, Peoples R China

[2] Shanghai Aerosp Control Technol Inst, Shanghai Key Lab Aerosp Intelligent Control Techn, Shanghai 201109, Peoples R China

[3] Shanghai Aerosp Control Technol Inst, Sch Aerosp Engn, Shanghai, Peoples R China

来源：

ACTA ASTRONAUTICA | 2016年 / 128卷

基金：

中国国家自然科学基金;

关键词：

Failed satellite; Collision avoidance; Ultra-close rendezvous; Measuring uncertainties; Gauss pseudospectral method; SPACECRAFT; NAVIGATION;

D O I：

10.1016/j.actaastro.2016.07.011

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper presents a trajectory planning algorithm to optimise the collision avoidance of a chasing spacecraft operating in an ultra-close proximity to a failed satellite. The complex configuration and the tumbling motion of the failed satellite are considered. The two-spacecraft rendezvous dynamics are formulated based on the target body frame, and the collision avoidance constraints are detailed, particularly concerning the uncertainties. An optimisation solution of the approaching problem is generated using the Gauss pseudospectral method. A closed-loop control is used to track the optimised trajectory. Numerical results are provided to demonstrate the effectiveness of the proposed algorithms. (C) 2016 IAA. Published by Elsevier Ltd. All rights reserved.

引用

页码：363 / 376

页数：14

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