Fixed-Time Inverse Optimal Attitude Tracking Control for Rigid Spacecraft
Author:
Affiliation:
1. Harbin Institute of Technology (Shenzhen),Shenzhen,P. R. China,518055
Funder
National Natural Science Foundation of China
Natural Science Foundation of Guangdong Province
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/9901509/9901494/09902441.pdf?arnumber=9902441
Reference16 articles.
1. Extended State Observer based robust attitude control of spacecraft with input saturation
2. Observer-based fault-tolerant attitude tracking control for rigid spacecraft with actuator saturation and faults
3. Fixed-Time Attitude Tracking Control for Spacecraft With Input Quantization
4. Suboptimal Repointing Maneuver of a staring-mode spacecraft with one DOF for final attitude
5. Continuous finite-time extended state observer based fault tolerant control for attitude stabilization
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