On novel adaptive saturated deployment control of tethered satellite system with guaranteed output tracking prescribed performance

被引:28
作者
Wei, Caisheng [1 ]
Luo, Jianjun [1 ]
Gong, Baichun [2 ]
Wang, Mingming [1 ]
Yuan, Jianping [1 ]
机构
[1] Northwestern Polytech Univ, Natl Key Lab Aerosp Flight Dynam, Xian 710072, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut, Sch Astronaut, Nanjing 210016, Jiangsu, Peoples R China
基金
国家自然科学基金重大项目;
关键词
Prescribed performance; Event-triggered control; Tethered satellite; Actuator saturation; SLIDING MODE CONTROL; PREDICTIVE CONTROL; NONLINEAR-SYSTEMS; TENSION CONTROL; CONTROL LAW; DYNAMICS;
D O I
10.1016/j.ast.2018.01.014
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In this paper, a novel model-free adaptive saturated control approach for deployment of the tethered satellite system (TSS) is developed based on time- and event-triggered mechanisms with consideration of the tether length constraint, actuator saturation and unknown external disturbance. Firstly, an appropriate output prescribed performance function is selected to quantitatively analyze the transient and steadystate performance of the deployment control system. Then, a strict-feedback system is established via an output transformation based on which two new model-free adaptive saturated control schemes are developed. Compared with the existing works, the primary advantage of the proposed approach is that the output tracking performance of the TSS can be guaranteed a priori with excellent disturbance rejection capability. Meanwhile, it is the first time that the event-triggered prescribed performance control scheme is proposed both in theoretic and application views, which dramatically reduces the frequency of controller updating and makes the corresponding designed schemes more applicable in practice. Finally, two group of illustrative examples are employed to validate the effectiveness of the proposed control approach. (C) 2018 Elsevier Masson SAS. All rights reserved.
引用
收藏
页码:58 / 73
页数:16
相关论文
共 38 条
[1]   ITAE Optimal Sliding Modes for Third-Order Systems With Input Signal and State Constraints [J].
Bartoszewicz, Andrzej ;
Nowacka-Leverton, Aleksandra .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 2010, 55 (08) :1928-1932
[2]   Robust Adaptive Control of Feedback Linearizable MIMO Nonlinear Systems With Prescribed Performance [J].
Bechlioulis, Charalampos P. ;
Rovithakis, George A. .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 2008, 53 (09) :2090-2099
[3]   A review of space tether research [J].
Cartmell, M. P. ;
McKenzie, D. J. .
PROGRESS IN AEROSPACE SCIENCES, 2008, 44 (01) :1-21
[4]   An Event-Triggered Approach for Load Frequency Control With Supplementary ADP [J].
Dong, Lu ;
Tang, Yufei ;
He, Haibo ;
Sun, Changyin .
IEEE TRANSACTIONS ON POWER SYSTEMS, 2017, 32 (01) :581-589
[5]   Nonlinear optimal control of tethered satellite systems using tether offset in the presence of tether failure [J].
Godard ;
Kumar, K. D. ;
Tan, B. .
ACTA ASTRONAUTICA, 2010, 66 (9-10) :1434-1448
[6]   Study on the stability of Tethered Satellite System [J].
He, Yong ;
Liang, Bin ;
Xu, Wenfu .
ACTA ASTRONAUTICA, 2011, 68 (11-12) :1964-1972
[7]   Periodic Event-Triggered Control for Linear Systems [J].
Heemels, W. P. M. H. ;
Donkers, M. C. F. ;
Teel, Andrew R. .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 2013, 58 (04) :847-861
[8]   Fractional order sliding mode control for tethered satellite deployment with disturbances [J].
Kang, Junjie ;
Zhu, Zheng H. ;
Wang, Wei ;
Li, Aijun ;
Wang, Changqing .
ADVANCES IN SPACE RESEARCH, 2017, 59 (01) :263-273
[9]   Prescribed performance tracking for flexible joint robots with unknown dynamics and variable elasticity [J].
Kostarigka, Artemis K. ;
Doulgeri, Zoe ;
Rovithakis, George A. .
AUTOMATICA, 2013, 49 (05) :1137-1147
[10]   Review of dynamics and control of nonelectrodynamic tethered satellite systems [J].
Kumar, K. D. .
JOURNAL OF SPACECRAFT AND ROCKETS, 2006, 43 (04) :705-720