Finite-Time Attitude Optimization Maneuver Control for Coupled Spacecraft Under Attitude Measurement Errors and Actuator Faults
Author:
Affiliation:
1. School of Electrical Engineering and Information, Tianjin University, Tianjin, China
2. Science and Technology on Space Intelligent Control Laboratory, Beijing Institute of Control Engineering, Beijing, China
Funder
National Natural Science Foundation of China
Science and Technology on Space Intelligent Control Laboratory
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
Electrical and Electronic Engineering,Computer Science Applications,Human-Computer Interaction,Control and Systems Engineering,Software
Link
http://xplorestaging.ieee.org/ielx7/6221021/10102641/09959968.pdf?arnumber=9959968
Reference32 articles.
1. Multivariable Finite Time Attitude Control for Quadrotor UAV: Theory and Experimentation
2. Finite-Time Distributed Attitude Synchronization for Multiple Spacecraft With Angular Velocity and Input Constraints
3. Unmanned Aerial Vehicles: Control Methods and Future Challenges
4. Adaptive Multivariable Reentry Attitude Control of RLV With Prescribed Performance
5. Sliding order and sliding accuracy in sliding mode control
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