Design of a Cislunar space navigation constellation based on special long-period orbits-Reference-Cited by-同舟云学术

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Design of a Cislunar space navigation constellation based on special long-period orbits

Published:2024-10 Issue:7 Volume:74 Page:3137-3156
ISSN:0273-1177
Container-title:Advances in Space Research
language:en
Short-container-title:Advances in Space Research

Author:

Gao Youtao^ORCID,Hu Chaoyong,Xin Yinghui,Jiang Kailun,Xu Bo,Wang Binghao,Zhou Jianhua

Publisher

Elsevier BV

Reference27 articles.

1. Five-impulse low-energy earth-moon transfer using manifolds;An;Adv. Space Res.,2024

2. High accuracy GNSS based navigation in GEO;Capuano;Acta Astronaut.,2017

3. Lunar orbits for telecommunication and navigation services;Cinelli;Astrodynamics,2024

4. Halo orbit dynamics and properties for a lunar global positioning system design;Circi;Mon. Not. R. Astron. Soc.,2014

5. Low energy transit orbits in the restricted three-body problems;Conley;SIAM. J. APPL. MATH.,1968

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