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

共 50 条

[1] Finite-time antisaturation control for spacecraft rendezvous and docking with safe constraint
Wu, Guan-qun
Song, Shen-Min
Sun, Jing-guang
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2019, 233 (06) : 2170 - 2184
[2] The Finite-time Robust Control for Spacecraft Rendezvous and Docking
Xu Ranran
Ji Haibo
Ma Yike
2014 33RD CHINESE CONTROL CONFERENCE (CCC), 2014, : 642 - 646
[3] Nonsingular Finite-Time Convergent Control for Spacecraft Rendezvous and Docking
Anand, Nikhil
Kumar, Shashi Ranjan
IFAC PAPERSONLINE, 2023, 56 (02): : 2007 - 2012
[4] Finite-Time Relative Pose Tracking Control for Uncertain Spacecraft Rendezvous and Docking
Sun, Liang
Wang, Jinwei
Jiang, Jingjing
PROCEEDINGS OF THE 33RD CHINESE CONTROL AND DECISION CONFERENCE (CCDC 2021), 2021, : 4397 - 4402
[5] Finite-Time Rendezvous Algorithms for Mobile Autonomous Agents
Hui, Qing
PROCEEDINGS OF THE 48TH IEEE CONFERENCE ON DECISION AND CONTROL, 2009 HELD JOINTLY WITH THE 2009 28TH CHINESE CONTROL CONFERENCE (CDC/CCC 2009), 2009, : 3063 - 3068
[6] Finite-Time Rendezvous Algorithms for Mobile Autonomous Agents
Hui, Qing
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 2011, 56 (01) : 207 - 211
[7] Finite-time attitude tracking control of air bearing table for spacecraft rendezvous and docking
Huang, Cheng
Wang, Yan
Chen, Xing-lin
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2018, 232 (01) : 96 - 110
[8] Relative Position and Attitude Coupled Control with Finite-time Convergence for Spacecraft Rendezvous and Docking
Xu Ranran
Ji Haibo
Li Kun
Kang Yu
Yang Kaihong
2015 54TH IEEE CONFERENCE ON DECISION AND CONTROL (CDC), 2015, : 3427 - 3432
[9] Finite-Time Autonomous Vehicle Path Tracking Control Based on State Constraint
Li, Pengxiang
Zhang, Sucai
Liu, Yan
IEEE ACCESS, 2024, 12 : 122274 - 122288
[10] Adaptive Finite-Time Control for Spacecraft Rendezvous under Unknown System Parameters
Liu, Yuan
Tang, Guojian
Li, Yuhang
Li, Hang
Ren, Jing
Zhang, Sai
INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2020, 2020

← 1 2 3 4 5 →