Spacecraft Anti-Unwinding Attitude Control with Actuator Nonlinearities and Velocity Limit
Author:
Affiliation:
1. Beihang University, 100191 Beijing, People’s Republic of China
2. Harbin Institute of Technology, 150001 Harbin, People’s Republic of China
3. Swansea University, Swansea, Wales SA2 8PP, 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.G000980
Reference20 articles.
1. Robust Adaptive Variable Structure Control of Spacecraft Under Control Input Saturation
2. Robust Tracking Control Design for Spacecraft Under Control Input Saturation
3. Globally Stabilizing Saturated Attitude Control in the Presence of Bounded Unknown Disturbances
4. Robust fault-tolerant control for spacecraft attitude stabilisation subject to input saturation
5. Backstepping Control Design with Actuator Torque Bound for Spacecraft Attitude Maneuver
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4. Composite anti-unwinding attitude control of spacecraft under actuator saturation and angular velocity limits;Advances in Space Research;2023-07
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