Finite-time control for autonomous rendezvous and docking under safe constraint

被引：24

作者：

Guo, Yong ^{[1
]}

Zhang, Dawei ^{[2
]}

Li, Ai-jun ^{[1
]}

Song, Shenmin ^{[3
]}

Wang, Chang-qing ^{[1
]}

Liu, Zongming ^{[4
]}

机构：

[1] Northwestern Polytech Univ, Sch Automat, Xian 710072, Shaanxi, Peoples R China

[2] Shanghai Inst Satellite Engn, Shanghai 201109, Peoples R China

[3] Harbin Inst Technol, Ctr Control Theory & Guidance Technol, Harbin 150001, Peoples R China

[4] Shanghai Inst Spaceflight Control Technol, Shanghai 201109, Peoples R China

来源：

AEROSPACE SCIENCE AND TECHNOLOGY | 2021年 / 109卷

基金：

中国博士后科学基金; 中国国家自然科学基金;

关键词：

Rendezvous and docking; Finite-time control; Artificial potential function; Sliding mode control; Collision avoidance; SLIDING MODE CONTROL; COLLISION-AVOIDANCE; PROXIMITY OPERATIONS; TRACKING CONTROL; SPACECRAFT; OPTIMIZATION; TRAJECTORIES; GUIDANCE; POSITION;

D O I：

10.1016/j.ast.2020.106380

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The finite-time controller under safe constraint is designed for the non-cooperative space autonomous rendezvous and docking by using the artificial potential function. To facilitate the establishment of the obstacle avoidance model, the elliptic cissoid is used to describe the final approaching corridor. Combining the model with the artificial potential function, a sliding mode surface that is finite-time stable is first developed to dealing with the problem of collision avoidance. Then, the finite-time controller that can make the chaser spacecraft do not collide with other space objects around the noncooperative target spacecraft and large stationary physical attachments of the non-cooperative target spacecraft is proposed. Finally, the validity of the controller is proved by numerical simulations. (c) 2020 Elsevier Masson SAS. All rights reserved.

引用

页数：7

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