On asteroid retrieval missions enabled by invariant manifold dynamics-Reference-Cited by-同舟云学术

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On asteroid retrieval missions enabled by invariant manifold dynamics

Published:2021-06 Issue: Volume:183 Page:43-51
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Tyler Jack^ORCID,Wittig Alexander^ORCID

Funder

EPSRC

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference25 articles.

1. Investigation of vehicle reusability for human exploration of near-Earth asteroids using Sun–Earth libration point orbits;Zimmer;Acta Astronaut.,2013

2. Near-Earth object intercept trajectory design for planetary defense;Vardaxis;Acta Astronaut.,2014

3. Impact risk assessment and planetary defense mission planning for asteroid 2015 PDC;Vardaxis;Acta Astronaut.,2016

4. Directed energy missions for planetary defense;Lubin;Adv. Space Res.,2016

5. Mission concepts and operations for asteroid mitigation involving multiple gravity tractors;Foster;Acta Astronaut.,2013

Cited by 4 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. Long-term capture of asteroids to the Sun-Earth L1/L2 using a lunar flyby and station-keeping maneuvers;Advances in Space Research;2023-07

2. A multiple-vehicle strategy for near-Earth asteroid capture;Acta Astronautica;2022-10

3. Energy analysis of Sun-Earth stable manifolds with a lunar flyby and with application to capture asteroids;Acta Astronautica;2022-09

4. Strategies to capture asteroids to distant retrograde orbits in the Sun–Earth system;Acta Astronautica;2021-12

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