Output-feedback asymptotic tracking control for rigid-body attitude via adaptive neural backstepping

被引:8
|
作者
Xia, Dongdong
Yue, Xiaokui [1 ]
Yin, Yuwan
机构
[1] Northwestern Polytech Univ, Sch Astronaut, Xian 710072, Peoples R China
基金
中国国家自然科学基金;
关键词
Rigid-body attitude; Asymptotic tracking; Output feedback; Adaptive neural backstepping; NONLINEAR-SYSTEMS; FUZZY CONTROL; SPACECRAFT; INPUT; IMMERSION; OBSERVERS;
D O I
10.1016/j.isatra.2022.10.042
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
In this note, a novel neural adaptive output-feedback control (NAOC) with asymptotic tracking performance for rigid-body attitude is investigated subject to inertia uncertainty, unavailability of the angular velocity and unknown external disturbance. First, by virtue of the combination of the first-order filter and the coordinate transformation, the original output feedback system with immeasurable angular velocity and unknown dynamics is converted into the full-state strict feedback system with mismatched disturbance. Second, aided by infinitely integrable inequality with saturation function, an innovative neural network (NN) based adaptive control scheme is proposed via backstepping technique. By adopting the model transformation and proposed algorithm, the asymptotic tracking performance of the transformed system and the attitude tracking system without angular velocity can be achieved simultaneously. Finally, comparative numerical simulations illustrate the efficacy of the developed algorithm. (c) 2022 ISA. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:104 / 113
页数:10
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