Optimal Fixed-Time Sliding Mode Control for Spacecraft Constrained Reorientation
Author:
Affiliation:
1. School of Aeronautics and Astronautics, Sichuan University, Chengdu, China
2. Department of Applied Mathematics, Hong Kong Polytechnic University, Hong Kong, China
Funder
National Natural Science Foundation of China
Huiyan Project for Research on Innovation and Application of Space Science and Technology
National Key Laboratory of Space Intelligent Control
RGC Grant PolyU
Hong Kong Polytechnic University
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/ielx7/9/4601496/10354510.pdf?arnumber=10354510
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