Adaptive finite-time sliding mode attitude tracking control laws for flexible spacecraft with actuator saturation
Author:
Affiliation:
1. Harbin Institute of Technology (Shenzhen), Nanshan District,Shenzhen,P. R. China,518055
2. Tsinghua University,Department of Precision Instrument,Beijing,P. R. China,100084
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10243163/10243123/10243177.pdf?arnumber=10243177
Reference24 articles.
1. Stabilization of the attitude of a rigid spacecraft with external disturbances using finite-time control techniques
2. A variable structure control with simple adaptation laws for upper bounds on the norm of the uncertainties;yoo;IEEE Transactions on Automatic Control,1992
3. Finite-Time Stability of Continuous Autonomous Systems
4. Attitude stabilization of rigid spacecraft with finite-time convergence
5. Adaptive Sliding Mode Control for Attitude Stabilization With Actuator Saturation
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