A Hybrid Dynamical System Approach to the Impulsive Control of Spacecraft Rendezvous
Author:
Affiliation:
1. University of Sevilla,Sevilla,Spain
2. LAAS-CNRS,Toulouse,France
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx8/10590709/10590710/10590979.pdf?arnumber=10590979
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4. Tradeoff study for approach trajectory of active debris removal satellites considering safety, fuel consumption, and operation;Sasaki,2019
5. Orion Rendezvous, Proximity Operations and Docking Design and Analysis
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