Robust PID controller for flexible satellite attitude control under angular velocity and control torque constraint
Author:
Affiliation:
1. Xidian University, School of Aerospace Science and Technology Xi'an China
2. Harbin Institute of Technology, Research Center of Satellite Technology Harbin China
Funder
China Postdoctoral Science Foundation
National Natural Science Foundation of China
Publisher
Wiley
Subject
Control and Systems Engineering
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1002/asjc.1999
Reference30 articles.
1. Feedback control logic for spacecraft eigenaxis rotations under slew rate and control constraints
2. Quarternion feedback regulator for spacecraft eigenaxis rotations
3. A constrained optimal PID-like controller design for spacecraft attitude stabilization
4. Fine attitude control by reaction wheels using variable-structure controller
5. Robust decentralized attitude coordination control of spacecraft formation
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