Decentralised fault-tolerant control of tethered spacecraft formation: an interconnected system approach

被引：12

作者：

Zhang, Zejun ^{[1
]}

Yang, Hao ^{[1
]}

Jiang, Bin ^{[1
]}

Cocquempot, Vincent ^{[2
]}

Cheng, Yuehua ^{[3
]}

机构：

[1] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing, Jiangsu, Peoples R China

[2] Univ Lille, CNRS, Centrale Lille, Ctr Rech Informat Signal & Automat Lille,UMR 9189, F-59000 Lille, France

[3] Nanjing Univ Aeronaut & Astronaut, Coll Astronaut, Nanjing, Jiangsu, Peoples R China

来源：

IET CONTROL THEORY AND APPLICATIONS | 2017年 / 11卷 / 17期

基金：

中国国家自然科学基金;

关键词：

decentralised control; fault tolerant control; interconnected systems; space vehicles; multi-robot systems; nonlinear systems; stability; space tethers; decentralised fault-tolerant control; interconnected system; three-inline array tethered spacecraft formation control; nonlinear model; formation stability; LARGE-SCALE SYSTEMS; ATTITUDE-CONTROL; FLEXIBLE SPACECRAFT; ACCOMMODATION; SATELLITES; REDUCTION; DYNAMICS;

D O I：

10.1049/iet-cta.2017.0485

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

In this study, a novel control strategy of a three-inline array tethered spacecraft formation is proposed, based on a simplified non-linear model around the equilibrium point. The formation stability is analysed by using an interconnected system approach which deeply reveals the coupling characteristic among three spacecraft. It is shown that both individual control laws of spacecraft and the coupling effects can achieve the stability. The problems of fault-tolerant control and fault propagation are further discussed. Simulation results validate the effectiveness of the proposed methods.

引用

页码：3047 / 3055

页数：9

共 37 条

[1]

Alfriend KT, 2010, SPACECRAFT FORMATION FLYING: DYNAMICS, CONTROL, AND NAVIGATION, P1, DOI 10.1016/B978-0-7506-8533-7.00206-2

[2]

[Anonymous], INT J CONTROL

[3] A Hierarchical Architecture for Cooperative Fault Accommodation of Formation Flying Satellites in Deep Space [J].

Azizi, S. M. ;

Khorasani, K. .

2009 AMERICAN CONTROL CONFERENCE, VOLS 1-9, 2009, :4178-4183

[4] Hierarchical Fault Diagnosis and Fuzzy Rule-Based Reasoning for Satellites Formation Flight [J].

Barua, A. ;

Khorasani, K. .

IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2011, 47 (04) :2435-2456

[5]

Blanke M., 2006, Diagnosis and fault-tolerant control

[6] Retargeting dynamics of a linear tethered interferometer [J].

Bombardelli, C ;

Lorenzini, EC ;

Quadrelli, MB .

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2004, 27 (06) :1061-1067

[7] Nonlinear Attitude Control of a Tether-Connected Multi-Satellite in Three-Dimensional Space [J].

Chang, Insu ;

Park, Sang-Young ;

Choi, Kyu-Hong .

IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2010, 46 (04) :1950-1968

[8] Nonlinear model reduction and decentralized control of tethered formation flight [J].

Chung, Soon-Jo ;

Slotine, Jean-Jacques E. ;

Miller, David W. .

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2007, 30 (02) :390-400

[9] SMALL GAIN THEOREMS FOR LARGE SCALE SYSTEMS AND CONSTRUCTION OF ISS LYAPUNOV FUNCTIONS [J].

Dashkovskiy, Sergey N. ;

Rueffer, Bjoern S. ;

Wirth, Fabian R. .

SIAM JOURNAL ON CONTROL AND OPTIMIZATION, 2010, 48 (06) :4089-4118

[10] Finite-Time Attitude Tracking Control of Spacecraft With Application to Attitude Synchronization [J].

Du, Haibo ;

Li, Shihua ;

Qian, Chunjiang .

IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 2011, 56 (11) :2711-2717

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