Detection system of near Earth objects based on the axial orbit in the Sun–Earth circular restricted three-body problem-Reference-Cited by-同舟云学术

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Detection system of near Earth objects based on the axial orbit in the Sun–Earth circular restricted three-body problem

Published:2023-07 Issue: Volume:208 Page:155-166
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Qi Yi,Tang Yuhua,Qiao Dong,Li Xiangyu^ORCID,Ding Ying^ORCID

Funder

National Natural Science Foundation of China

Beijing Institute of Technology

Beijing Institute of Technology Research Fund Program for Young Scholars

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference27 articles.

1. The trajectory, structure and origin of the Chelyabinsk asteroidal impactor;Borovička;Nature,2013

2. Quantifying the risk posed by potential Earth impacts;Chesley;Icarus,2002

3. Highly effective kinetic impact design for asteroid deflection missions exploiting impact-geometry maps;Yamaguchi;J. Guid. Control Dyn.,2020

4. Gravitational tractor for towing asteroids;Lu;Nature,2005

5. Impact hazard protection efficiency by a small kinetic impactor;Sanchez;J. Spacecr. Rockets,2013

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Cislunar L4 and L5 axial orbits and their applications;Acta Astronautica;2024-09

2. Expanded Families of Periodic Orbits for the Jupiter–Callisto System;Journal of Spacecraft and Rockets;2023-12-21

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