Decentralized adaptive sliding mode control for beam synchronization of tethered InSAR system

被引:6
作者
Zhang, Jinxiu [1 ]
Zhang, Zhigang [1 ]
Wu, Baolin [1 ]
机构
[1] Harbin Inst Technol, Res Ctr Satellite Technol, Harbin 150080, Peoples R China
基金
中国国家自然科学基金;
关键词
Tethered InSAR system; Beam synchronization; Total zero Doppler steering; Decentralized adaptive control; ATTITUDE-CONTROL; TANDEM-X; SAR; INTERFEROMETER; DYNAMICS;
D O I
10.1016/j.actaastro.2016.05.024
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Beam synchronization problem of tethered interferometric synthetic aperture radar (InSAR) is addressed in this paper. Two antennas of the system are carried by separate satellites connected through a tether to obtain a preferable baseline. A Total Zero Doppler Steering (TZDS) is implemented to mother-satellite to cancel the residual Doppler. Subsequently attitude reference trajectories for the two satellites are generated to achieve the beam synchronization and TZDS. Thereafter, a decentralized adaptive sliding mode control law is proposed to track these reference trajectories in the presence of model uncertainties and external disturbances. Finally, the stability of closed-loop system is proved by the corollary of Barbalat's Lemma. Simulation results show the proposed control law is effective to achieve beam synchronization of the system. (C) 2016 IAA. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:57 / 66
页数:10
相关论文
共 28 条
[1]  
Aslanov VS, 2012, WOODHEAD PUBL MECH E, P1, DOI 10.1533/9780857096005
[2]   Indirect robust adaptive fault-tolerant control for attitude tracking of spacecraft [J].
Cai, Wenchuan ;
Liao, X. H. ;
Song, Y. D. .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2008, 31 (05) :1456-1463
[3]   Propellant-free control of tethered formation flight, part 1: Linear control and experimentation [J].
Chung, Soon-Jo ;
Miller, David W. .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2008, 31 (03) :571-584
[4]   Attitude and antenna pointing design of bistatic radar formations [J].
D'Errico, M ;
Moccia, A .
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2003, 39 (03) :949-960
[5]  
Farley R.E., 2001, 4770 AIAA, P28
[6]  
Fiedler H., IEEE GEOSCI REMOTE S, P2
[7]   Nonlinear dynamics of the tethered subsatellite system in the station keeping phase [J].
Fujii, HA ;
Ichiki, W .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1997, 20 (02) :403-406
[8]   MODELING ISSUES RELATED TO RETRIEVAL OF FLEXIBLE TETHERED SATELLITE SYSTEMS [J].
KIM, E ;
VADALI, SR .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1995, 18 (05) :1169-1176
[9]  
Klinkrad H., P ESA WORKSH SPAC WE, P19
[10]  
Kojima H., J GUID CONTROL DYN, P34