Finite‐time fault tolerant attitude control for over‐activated spacecraft subject to actuator misalignment and faults-Reference-Cited by-同舟云学术

Finite‐time fault tolerant attitude control for over‐activated spacecraft subject to actuator misalignment and faults

Published:2013-11 Issue:16 Volume:7 Page:2007-2020
ISSN:1751-8652
Container-title:IET Control Theory & Applications
language:en
Short-container-title:IET Control Theory & Applications

Author:

Zhang Aihua¹²,Hu Qinglei²,Friswell Michael I.³

Affiliation:

1. College of Engineering, Bohai UniversityJinzhou121013People's Republic of China

2. Department of Control Science and EngineeringHarbin Institute of TechnologyHarbin150001People's Republic of China

3. College of Engineering, Swansea UniversitySingleton ParkSwanseaSA2 8PPUK

Funder

National Natural Science Foundation of China

Heilongjiang Youth Development Foundation

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

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1049/iet-cta.2013.0133

Reference48 articles.

1. Optimal Nonlinear Tracking of Spacecraft Attitude Maneuvers

2. Inverse optimal adaptive control for attitude tracking of spacecraft

3. Adaptive output feedback sliding-mode manoeuvring and vibration control of flexible spacecraft with input saturation

4. Sliding mode control using modified Rodrigues parameters

5. Nonlinear Adaptive Control of Spacecraft Maneuvers

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