Tracking control of spacecraft formation flying with collision avoidance

被引:123
作者
Hu, Qinglei [1 ,2 ]
Dong, Hongyang [2 ]
Zhang, Youmin [3 ]
Ma, Guangfu [2 ]
机构
[1] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China
[2] Harbin Inst Technol, Dept Control Sci & Engn, Harbin 150001, Peoples R China
[3] Concordia Univ, Dept Mech & Ind Engn, Montreal, PQ H3G 1M8, Canada
基金
中国国家自然科学基金;
关键词
Formation flying; Collision avoidance; Target tracking; Adaptive control; SLIDING-MODE CONTROL; ADAPTIVE FORMATION CONTROL; ARTIFICIAL POTENTIALS; SATELLITE FORMATION; RELATIVE DYNAMICS; ORBITS; RECONFIGURATION; GUIDANCE; MOTION;
D O I
10.1016/j.ast.2014.12.031
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Study results of developing formation control system for multi-spacecraft that requires avoiding obstacles and maintaining the formation configuration are presented. In particular, nonlinear adaptive feedback control law is developed by employing special potential functions and a kind of time-varying sliding manifold, to enable the spacecraft formation in a specific configuration by taking into account the obstacle avoidance requirement while tracking a moving target in a way of cooperation or not. Moreover, capability for handling multiple tasks by the proposed control system is demonstrated in the presence of disturbances and parametric uncertainties. The stability proof is based on a Lyapunov-like analysis and the properties of the proposed potential functions. Numerical simulation of the proposed method is presented to demonstrate the advantages with respect to obstacle avoidance, fast tracking and formation flying configuration reconstruction capability. (C) 2015 Elsevier Masson SAS. All rights reserved.
引用
收藏
页码:353 / 364
页数:12
相关论文
共 37 条
[1]   Satellite Formation and Reconfiguration with Restricted Control Interval [J].
Bando, Mai ;
Ichikawa, Akira .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2010, 33 (02) :607-615
[2]   Periodic Orbits of Nonlinear Relative Dynamics and Satellite Formation [J].
Bando, Mai ;
Ichikawa, Akira .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2009, 32 (04) :1200-1208
[3]   A coordination architecture for spacecraft formation control [J].
Beard, RW ;
Lawton, J ;
Hadaegh, FY .
IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2001, 9 (06) :777-790
[4]   Safe trajectories for autonomous rendezvous of spacecraft [J].
Breger, Louis ;
How, Jonathan P. .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2008, 31 (05) :1478-1489
[5]   Analytical solution to optimal relocation of satellite formation flying in arbitrary elliptic orbits [J].
Cho, Hancheol ;
Park, Sang-Young ;
Yoo, Sung-Moon ;
Choi, Kyu-Hong .
AEROSPACE SCIENCE AND TECHNOLOGY, 2013, 25 (01) :161-176
[6]   On synchronization and collision avoidance for mechanical systems [J].
Chopra, Nikhil ;
Stipanovic, Dusan M. ;
Spong, Mark W. .
2008 AMERICAN CONTROL CONFERENCE, VOLS 1-12, 2008, :3713-+
[7]   Adaptive nonlinear control of multiple spacecraft formation flying [J].
de Queiroz, MS ;
Kapila, V ;
Yant, QG .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2000, 23 (03) :385-390
[8]   Resolution of conflicts involving many aircraft via semidefinite programming [J].
Frazzoli, E ;
Mao, ZH ;
Oh, JH ;
Feron, E .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2001, 24 (01) :79-86
[9]   Target tracking using artificial potentials and sliding mode control [J].
Gazi, V. ;
Ordonez, R. .
INTERNATIONAL JOURNAL OF CONTROL, 2007, 80 (10) :1626-1635
[10]   Swarm aggregations using artificial potentials and sliding-mode control [J].
Gazi, V .
IEEE TRANSACTIONS ON ROBOTICS, 2005, 21 (06) :1208-1214