Active vibration suppression and attitude tracking for flexible spacecraft without intelligent materials
Author:
Affiliation:
1. China University of Mining and Technology,School of Information and Control Engineering,Xuzhou,China,221009
2. Beijing Institute of Precision Mechatronics and Controls,Beijing,China,100076
Funder
National Natural Science Foundation of China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10032843/10032844/10033830.pdf?arnumber=10033830
Reference20 articles.
1. Positive position feedback (PPF) controller for suppression of nonlinear system vibration
2. Consensus positive position feedback control for vibration attenuation of smart structures
3. Finite-time sliding mode attitude control for rigid spacecraft without angular velocity measurement;shikai;Journal of the Franklin Institute,2017
4. Fixed-Time Leader–Follower Output Feedback Consensus for Second-Order Multiagent Systems
5. Active fault tolerant control system design for spacecraft attitude maneuvers with actuator saturation and faults;qiang;IEEE Transactions on Industrial Electronics,2018
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