Finite-time ESO and Non-singular TSM Control Strategy for Trajectory Tracking of Hovercraft
Author:
Affiliation:
1. Harbin Engineering University,College of Intelligent Systems Science and Engineering,Harbin,Heilongjiang Province,China,150001
2. No.703 Research Institute of CSSC No.35 Honghu Road, Daoli District,Harbin City,China,150078
Funder
National Natural Science Foundation of China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/9976950/9976951/09977124.pdf?arnumber=9977124
Reference15 articles.
1. Adaptive Robust Finite-Time Trajectory Tracking Control of Fully Actuated Marine Surface Vehicles
2. Continuous Finite-Time Attitude Control for Rigid Spacecraft Based on Angular Velocity Observer
3. Observer-Based Output Feedback Attitude Stabilization for Spacecraft With Finite-Time Convergence
4. Attitude stabilization of rigid spacecraft with finite-time convergence
5. Velocity-free fault-tolerant control allocation for flexible spacecraft with redundant thrusters
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