A new method for solving reachable domain of spacecraft with a single impulse
Author:
Funder
National Natural Science Foundation of China
Chang Jiang Scholars Program
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference20 articles.
1. Tracking control of spacecraft formation flying with collision avoidance;Hu;Aero. Sci. Technol.,2015
2. Relative position coordinated control for spacecraft formation flying with communication delays;Ran;Acta Astronaut.,2017
3. Autonomous trajectory planning for rendezvous and proximity operations by conic optimization;Lu;J. Guid. Contr. Dynam.,2013
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4. Application of Indirect Multi-Stage Reachable Set Determination Algorithm for Low-Thrust Spacecraft Trajectory Optimization;AIAA SCITECH 2024 Forum;2024-01-04
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