Neural‐network‐based adaptive finite‐time output constraint control for rigid spacecrafts-Reference-Cited by-同舟云学术

Neural‐network‐based adaptive finite‐time output constraint control for rigid spacecrafts

Published:2021-09-07 Issue: Volume: Page:
ISSN:1049-8923
Container-title:International Journal of Robust and Nonlinear Control
language:en
Short-container-title:Int J Robust Nonlinear Control

Author:

Xie Shuzong¹^ORCID,Tao Meiling²^ORCID,Chen Qiang¹^ORCID,Tao Liang²

Affiliation:

1. College of Information Engineering Zhejiang University of Technology Hangzhou China

2. Key Laboratory of Advanced Perception and Intelligent Control of High‐end Equipment Ministry of Education, Anhui Polytechnic University Wuhu China

Funder

National Natural Science Foundation of China

Natural Science Foundation of Anhui Province

Publisher

Wiley

Subject

Electrical and Electronic Engineering,Industrial and Manufacturing Engineering,Mechanical Engineering,Aerospace Engineering,Biomedical Engineering,General Chemical Engineering,Control and Systems Engineering

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1002/rnc.5766

Reference33 articles.

1. Attitude Tracking and Disturbance Rejection of Rigid Spacecraft by Adaptive Control

2. Adaptive Sliding Mode Control for Attitude Stabilization With Actuator Saturation

3. Robust stabilization of spacecraft attitude motion under magnetic control through time‐varying integral sliding mode

4. Event-Triggered Sliding Mode Control for Attitude Stabilization of a Rigid Spacecraft

5. Fuzzy Adaptive Fault-Tolerant Output Feedback Attitude-Tracking Control of Rigid Spacecraft

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