A Nonlinear Observer-Based Approach to Robust Cooperative Tracking for Heterogeneous Spacecraft Attitude Control and Formation Applications

被引:54
作者
Wang, Bohui [1 ]
Chen, Weisheng [1 ]
Zhang, Bin [2 ]
Shi, Peng [3 ,4 ]
Zhang, Huiyan [5 ]
机构
[1] Xidian Univ, Sch Aerosp Sci & Technol, Xian 710071, Peoples R China
[2] Univ South Carolina, Dept Elect Engn, Columbia, SC 29208 USA
[3] Univ Adelaide, Sch Elect & Elect Engn, Adelaide, SA 5005, Australia
[4] Victoria Univ, Coll Engn & Sci, Melbourne, Vic 8001, Australia
[5] Chongqing Technol & Business Univ, Natl Res Base Intelligent Mfg Serv, Chongqing 400067, Peoples R China
基金
中国国家自然科学基金;
关键词
Attitude control; formation flying; heterogeneous spacecraft; nonlinear observer; robust cooperative tracking; MULTIAGENT SYSTEMS SUBJECT; LINEAR-SYSTEMS; ACTUATOR SATURATION; CONSENSUS; STABILIZATION; OUTPUT; SYNCHRONIZATION;
D O I
10.1109/TAC.2022.3143082
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This article proposes a nonlinear observer-based approach to address the robust cooperative tracking problem and application for heterogeneous spacecraft systems. By introducing appropriate assumptions, a weight average estimation is proposed to construct a class of distributed nonlinear observers for heterogeneous spacecraft systems with a target whose dynamics are available only to a few chasers. By synthesizing the observer dynamics among the neighbors, a novel cooperative tracking controller is developed to address nonidentical parameters both in model uncertainties and nonlinear dynamics. Then, the robust consensus tracking problem can be solved if the cooperative behaviors between the chasers and their observers can be achieved synchronically. A special case of the identical model uncertainty and nonlinear dynamics scenario is also discussed. As applications of the proposed nonlinear observer-based approaches, the controller and observer designs of heterogeneous spacecraft attitude control and formation flying systems are revisited. Numerical simulations with a nonlinear dynamic model of spacecraft attitude control and formation flying systems demonstrate the effectiveness of the proposed approaches.
引用
收藏
页码:400 / 407
页数:8
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