Adaptive Fault-Tolerant Control of Spacecraft Attitude Dynamics with Actuator Failures-Reference-Cited by-同舟云学术

Adaptive Fault-Tolerant Control of Spacecraft Attitude Dynamics with Actuator Failures

Published:2015-10 Issue:10 Volume:38 Page:2033-2042
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Han Yu¹,Biggs James D.²,Cui Naigang¹

Affiliation:

1. School of Astronautics, Harbin Institute of Technology, 150001 Harbin, People’s Republic of China

2. Department of Mechanical and Aerospace Engineering, University of Strathclyde, Glasgow, Scotland G1 1XJ, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.G000921

Reference21 articles.

1. BedingfieldK. L.LeachR. D.AlexanderM. B. “Spacecraft System Failures and Anomalies Attributed to the Natural Space Envirment,” NASA Reference Publ. 1390, 1996.

2. A study of on-orbit spacecraft failures

3. Finite-time fault tolerant attitude stabilization control for rigid spacecraft

4. Indirect Robust Adaptive Fault -Tolerant Control for Attitude Tracking of Spacecraft

5. Adaptive Fault-Tolerant Tracking Control of Near-Space Vehicle Using Takagi–Sugeno Fuzzy Models

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