Finite-Time Attitude Control for Coupled Spacecraft with Input Constraints
Author:
Affiliation:
1. School of Information and Control Engineering, China University of Mining and Technology,Xuzhou,China,221116
2. Beijing Institute of Precision Mechatronics and Controls,Beijing,China,100076
Funder
National Natural Science Foundation of China
Fundamental Research Funds for the Central Universities
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10239690/10239711/10239769.pdf?arnumber=10239769
Reference15 articles.
1. Observer-Based NN Control for Nonlinear Systems With Full-State Constraints and External Disturbances
2. Anti-Windup Robust Backstepping Control for an Underactuated Reusable Launch Vehicle
3. Finite-Time Attitude Optimization Maneuver Control for Coupled Spacecraft Under Attitude Measurement Errors and Actuator Faults
4. Novel finite-time adaptive neural control of flexible spacecraft with actuator constraints and pre-scribed attitude tracking performance;tao;Acta Astronautica,2020
5. Input-to-state stability based adaptive control for spacecraft fly-around with input saturation;yu;IET Control Theory and Applications,2020
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