Relative E/I vector-based optimal and suboptimal control for continuous low thrust formation reconfiguration in circular orbits-Reference-Cited by-同舟云学术

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Relative E/I vector-based optimal and suboptimal control for continuous low thrust formation reconfiguration in circular orbits

Published:2024-07 Issue: Volume:150 Page:109237
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Wang Jihe^ORCID,Ren Yuanyi^ORCID,Zeng Qiaoling,Zhang Chengxi^ORCID,Zhang Jinxiu^ORCID

Funder

Shenzhen Science and Technology Innovation Committee

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference36 articles.

1. E/I-vector separation for safe switching of the GRACE formation;Montenbruck;Aerosp. Sci. Technol.,2006

2. Proximity operations of formation-flying spacecraft using an eccentricity/inclination vector separation;D'Amico;J. Guid. Control Dyn.,2006

3. LISA satellite formation control;Bik;Adv. Space Res.,2007

4. Spaceborne autonomous formation-flying experiment on the PRISMA mission;D'Amico;J. Guid. Control Dyn.,2012

5. GPS-based relative navigation for the Proba-3 formation flying mission;Ardaens;Acta Astronaut.,2013

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