Optimized Data-Driven Prescribed Performance Attitude Control for Actuator Saturated Spacecraft
Author:
Affiliation:
1. School of Automation Science and Electrical Engineering, Beihang University, Beijing, China
2. School of Engineering, University of Warwick, Coventry, U.K.
3. School of Cyber Science and Technology, Beihang University, Beijing, China
Funder
National Natural Science Foundation of China
Natural Science Foundation of Zhejiang Province
Industry-University-Research Foundation of China
Hangzhou Qianjiang Distinguished Expert program
China Scholarship Council
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
Electrical and Electronic Engineering,Computer Science Applications,Control and Systems Engineering
Link
http://xplorestaging.ieee.org/ielx7/3516/10153806/10004739.pdf?arnumber=10004739
Reference32 articles.
1. Appointed-time fault-tolerant attitude tracking control of spacecraft with double-level guaranteed performance bounds
2. Fault-Tolerant Prescribed Performance Attitude Tracking Control for Spacecraft Under Input Saturation
3. Geometric Mechanics Based Nonlinear Model Predictive Spacecraft Attitude Control with Reaction Wheels
4. Optimal Nonlinear Tracking of Spacecraft Attitude Maneuvers
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