Spacecraft Attitude Stabilization Control Under Actuator Faults and Input Saturation
Author:
Affiliation:
1. School of Robotics, Ningbo University of Technology,Zhejiang,China,315211
2. Nottingham University,Key Laboratory of More Electric Aircraft,Zhejiang,China,315211
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10505441/10505442/10505656.pdf?arnumber=10505656
Reference20 articles.
1. Sliding-mode-based attitude tracking control of spacecraft under reaction wheel uncertainties
2. Spacecraft attitude fault-tolerant stabilization against loss of actuator Effectiveness: A novel iterative learning sliding mode approach
3. Rotating Object Specific Tracking Based on Orbit-Attitude Coordinated Adaptive Control
4. Iterative Learning Disturbance Observer Based Attitude Stabilization of Flexible Spacecraft Subject to Complex Disturbances and Measurement Noises
5. Recent advances in precision measurement & pointing control of spacecraft
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