A novel calculation method for low-thrust transfer trajectories in the Earth-Moon restricted three-body problem-Reference-Cited by-同舟云学术

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A novel calculation method for low-thrust transfer trajectories in the Earth-Moon restricted three-body problem

Published:2024-04 Issue: Volume:147 Page:109048
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Du Chongrui,Song Liangjun^ORCID,Zhang Jiye^ORCID,Liu Yi

Publisher

Elsevier BV

Reference46 articles.

1. Spacecraft survivability in the natural debris environment near the stable earth-moon Lagrange points;Boone;Adv. Space Res.,2021

2. Low-thrust transfers in the earth-moon system, including applications to libration point orbits;Ozimek;J. Guid. Control Dyn.,2010

3. Deployment and retrieval of a rotating triangular tethered satellite formation near libration points;Cai;Acta Astronaut.,2014

4. Analytical solution of the optimal steering law for non-ideal solar sail;Niccolai;Aerosp. Sci. Technol.,2017

5. Low-thrust trajectory design for near-earth asteroid supply delivery and resource transportation mission using high-power solar electric propulsion;Xie;Aerosp. Sci. Technol.,2023

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