Optimal trajectories for a multiple rendezvous mission to asteroids-Reference-Cited by-同舟云学术

Optimal trajectories for a multiple rendezvous mission to asteroids

Published:1992-08 Issue:8-10 Volume:26 Page:587-597
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Bulirsch R.,Callies R.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference26 articles.

1. The AMSAT mission to the asteroid belt;Meinzer;IAF Paper 83-207,1983

2. Design and navigation accuracy assessment of an ion driven asteroids flyby and rendezvous mission launched by Ariane 4 APEX demonstration flight;Eckstein;DFVLR Internal Report GSOC 83-1,1983

3. Effects of changes in spacecraft design data on mission design and navigation accuracy of the AMSAT asteroid rendezvous mission;Eckstein;DFVLR Internal Report GSOC 84-1,1984

4. Mission options for the first SEPS application;Yen;AAS/AIAA Paper 81-186,1981

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