Controllable Trade-Off Between Performance and Constrained Input for Vibration Suppression in Flexible Space Structures
Author:
Affiliation:
1. Agency for Science, Technology, and Research, Singapore Institute of Manufacturing Technology, Singapore
2. Tsinghua University, Beijing, China
3. National University of Singapore, Singapore
Funder
National Natural Science Foundation of China
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Link
http://xplorestaging.ieee.org/ielx7/7/10552647/10418999.pdf?arnumber=10418999
Reference55 articles.
1. Attitude Stabilization Control of Flexible Satellites With High Accuracy: An Estimator-Based Approach
2. Modeling and Control of Spacecraft with Multiple Active Pointing Ultra-Quiet Platforms
3. DOB-Based Neural Control of Flexible Hypersonic Flight Vehicle Considering Wind Effects
4. Integrated nonlinear optimal control of spacecraft in proximity operations
5. Velocity-Free Trajectory Tracking and Active Vibration Control of Flexible Space Manipulator
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