Global Stabilization of Circular Orbit Rendezvous by Bounded Linear Feedback
Author:
Affiliation:
1. China University of Mining and Technology,School of Mathematics, Jiangsu Center for Applied Mathematics (CUMT),Xuzhou,China,221116
2. Nanjing Research Institute of Electronic Engineering,Nanjing,China
Funder
National Natural Science Foundation of China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx8/10595059/10595098/10595259.pdf?arnumber=10595259
Reference25 articles.
1. State Transition Matrices for Terminal Rendezvous Studies: Brief Survey and New Example
2. Optimal power-limited rendezvous with upper and lower bounds on thrust
3. Terminal Guidance System for Satellite Rendezvous
4. Leader-following adaptive consensus of multiple uncertain rigid spacecraft systems
5. Minimum sliding mode error feedback control for inner-formation satellite system with J 2 and small eccentricity
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