Learning-based adaptive prescribed performance control of postcapture space robot-target combination without inertia identifications

被引:43
|
作者
Wei, Caisheng [1 ]
Luo, Jianjun [1 ]
Dai, Honghua [1 ]
Bian, Zilin [2 ]
Yuan, Jianping [1 ]
机构
[1] Northwestern Polytech Univ, Natl Key Lab Aerosp Flight Dynam, Xian 710072, Shaanxi, Peoples R China
[2] NanChang HangKong Univ, Sch Informat Engn, Nanchang 330063, Jiangxi, Peoples R China
基金
国家自然科学基金重大项目; 中国国家自然科学基金;
关键词
Prescribed performance; Spacecraft; Adaptive dynamic programming; Nonlinear control; Space robot; UNCERTAIN NONLINEAR-SYSTEMS; ATTITUDE TAKEOVER CONTROL; FLEXIBLE SPACECRAFT; MULTIAGENT SYSTEMS; CONTROL SCHEME; POST-CAPTURE; FEEDBACK; DYNAMICS; OBJECT; APPROXIMATION;
D O I
10.1016/j.actaastro.2018.03.007
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In this paper, a novel learning-based adaptive attitude takeover control method is investigated for the post capture space robot-target combination with guaranteed prescribed performance in the presence of unknown inertial properties and external disturbance. First, a new static prescribed performance controller is developed to guarantee that all the involved attitude tracking errors are uniformly ultimately bounded by quantitatively characterizing the transient and steady-state performance of the combination. Then, a learning-based supplementary adaptive strategy based on adaptive dynamic programming is introduced to improve the tracking performance of static controller in terms of robustness and adaptiveness only utilizing the input/output data of the combination. Compared with the existing works, the prominent advantage is that the unknown inertial properties are not required to identify in the development of learning-based adaptive control law, which dramatically decreases the complexity and difficulty of the relevant controller design. Moreover, the transient and steady-state performance is guaranteed a priori by designer-specialized performance functions without resorting to repeated regulations of the controller parameters. Finally, the three groups of illustrative examples are employed to verify the effectiveness of the proposed control method.
引用
收藏
页码:228 / 242
页数:15
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