Mission design for a halo orbiter of the earth-Reference-Cited by-同舟云学术

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Mission design for a halo orbiter of the earth

Published:1976-08-16 Issue: Volume: Page:
ISSN:
Container-title:Astrodynamics Conference
language:
Short-container-title:

Author:

FARQUHAR R.¹,MUHONEN D.¹,RICHARDSON D.²

Affiliation:

1. NASA, Goddard Space Flight Center, Greenbelt, Md.

2. Computer Sciences Corp., Silver Spring, Md.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1976-810

Reference11 articles.

Cited by 6 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. Design and analysis of quasi-halo orbits and optimal transfers from the Earth under different Sun–Earth frameworks using differential evolution;Journal of Astrophysics and Astronomy;2023-08-29

2. Rapid accessibility evaluation for ballistic lunar capture via manifolds: A Gaussian process regression application;Astrodynamics;2022-04-19

3. Analysis of nominal halo orbits in the Sun–Earth system;Archive of Applied Mechanics;2021-09-04

4. Stationkeeping controllers for Earth–Moon L1 and L2 libration points halo orbits;Journal of the Brazilian Society of Mechanical Sciences and Engineering;2021-06-15

5. EQUULEUS Trajectory Design;The Journal of the Astronautical Sciences;2020-01-24

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