Robust fault-tolerant control for spacecraft attitude stabilisation subject to input saturation

Author:

Hu Q.,Xiao B.,Friswell M.I.

Publisher

Institution of Engineering and Technology (IET)

Subject

Electrical and Electronic Engineering,Control and Optimization,Computer Science Applications,Human-Computer Interaction,Control and Systems Engineering

Cited by 99 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Adaptive Terminal Sliding Mode Fault-Tolerant Control of Spacecraft Based on the Left Attitude Error Function of SO(3);International Journal of Aerospace Engineering;2023-08-04

2. Adaptive finite-time sliding mode attitude tracking control laws for flexible spacecraft with actuator saturation;2023 2nd Conference on Fully Actuated System Theory and Applications (CFASTA);2023-07-14

3. Failure Identification Method and LMI-Based Control System for Small Spacecraft;Applied Sciences;2023-05-14

4. Passive fault‐tolerant control for discrete parameter system;IET Power Electronics;2023-05-02

5. Advanced fault detection and diagnosis in spacecraft attitude control systems: Current state and challenges;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2023-02-17

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