Neural-network-assisted optimization of a close-range multi-spacecraft rendezvous mission based on a multi-impulse maneuvering strategy-Reference-Cited by-同舟云学术

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Neural-network-assisted optimization of a close-range multi-spacecraft rendezvous mission based on a multi-impulse maneuvering strategy

Published:2023-09 Issue:5 Volume:72 Page:1829-1843
ISSN:0273-1177
Container-title:Advances in Space Research
language:en
Short-container-title:Advances in Space Research

Author:

Yan Huida,Guo Yanning,Li Chuanjiang,Song Bin

Funder

National Natural Science Foundation of China

China Aerospace Science and Technology Corporation

Publisher

Elsevier BV

Subject

Space and Planetary Science,Aerospace Engineering,General Earth and Planetary Sciences,Atmospheric Science,Geophysics,Astronomy and Astrophysics

Reference33 articles.

1. Optimal servicing of geosynchronous satellites;Alfriend;J. Guidance Control Dyn.,2006

2. A review of impending small satellite formation flying missions;Bandyopadhyay,2015

3. Two-phase framework for near-optimal multi-target lambert rendezvous;Bang;Adv. Space Res.,2018

4. Necessary and sufficient conditions for optimal impulsive rendezvous with linear equations of motion;Carter;Dyn. Control,2000

5. Multiple space debris collecting mission: optimal mission planning;Cerf;J. Optim. Theory Appl.,2015

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