Finite-Time Contractive Control of Spacecraft Rendezvous System
Author:
Affiliation:
1. School of Astronautics, Harbin Institute of Technology, Harbin 150001, China
2. Beijing Institute of Control Engineering, Beijing 100190, China
3. School of Information and Automation, Qilu University of Technology, Jinan 250353, China
Abstract
Funder
National Natural Science Foundation of China
Publisher
MDPI AG
Subject
General Mathematics,Engineering (miscellaneous),Computer Science (miscellaneous)
Link
https://www.mdpi.com/2227-7390/11/8/1871/pdf
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4. Robust control for autonomous spacecraft evacuation with model uncertainty and upper bound of performance with constraints;Sheng;Math. Prob. Eng.,2014
5. Guaranteed cost output tracking control for autonomous homing phase of spacecraft rendezvous;Yang;J. Aerosp. Eng.,2011
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