Observer-Based Fault Diagnosis Incorporating Online Control Allocation for Spacecraft Attitude Stabilization under Actuator Failures

Author:

Hu Qinglei,Li Bo,Friswell Michael I.

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Aerospace Engineering

Cited by 12 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. Novel Iterative-Learning-Observer-Based Fault Detection for Dynamic Actuators;J GUID CONTROL DYNAM;2024

2. Improved time-variable transformer-based fault diagnosis method for satellite attitude control system;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2024-04-24

3. Synthesis of Nominal Reorientation Trajectories of a Small Satellite in Case of Failure of One Actuator;Mekhatronika, Avtomatizatsiya, Upravlenie;2023-10-31

4. Adaptive predefined-time prescribed performance control for spacecraft systems;Mathematical Biosciences and Engineering;2023

5. Fault-tolerant spacecraft attitude control: A critical assessment;Progress in Aerospace Sciences;2022-04

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