Fault-Tolerant Tracking Control of Spacecraft with Attitude-Only Measurement Under Actuator Failures-Reference-Cited by-同舟云学术

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Fault-Tolerant Tracking Control of Spacecraft with Attitude-Only Measurement Under Actuator Failures

Published:2014-05 Issue:3 Volume:37 Page:838-849
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Xiao Bing¹,Hu Qinglei¹,Zhang Youmin²,Huo Xing³

Affiliation:

1. Department of Control Science and Engineering, Harbin Institute of Technology, 150001 Harbin, People’s Republic of China

2. Department of Mechanical and Industrial Engineering, Concordia University, Montreal, Quebec H3G 1M8, Canada

3. College of Engineering, Bohai University, 121000 Jinzhou, People’s Republic of China

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/10.2514/1.61369

Reference52 articles.

1. Optimal Nonlinear Tracking of Spacecraft Attitude Maneuvers

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

3. H-infinity Inverse Optimal Attitude-Tracking Control of Rigid Spacecraft

4. Adaptive Control of Uncertain Hamiltonian Multi-Input Multi-Output Systems: With Application to Spacecraft Control

5. Nonlinear observer and output feedback attitude control of spacecraft

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