2020
DOI: 10.1088/1755-1315/587/1/012037
|View full text |Cite
|
Sign up to set email alerts
|

Deimos rendezvous mission analysis and orbital design based on the Mars survey

Abstract: Imaging the Martian surface with a sun-synchronous orbit is a fundamental task of most current Mars exploration programs. In this paper, the Mars-Deimos multi-target orbit design is carried out for a small spacecraft that uses the spacecraft’s spare spacecraft to achieve a carrier launch. Due to the 92.7° inclination of the working orbit of the main detector, Deimos detection is carried out by means of a swept intersection: The working orbit is designed for a large elliptical orbit with a critical inclination … Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...

Citation Types

0
0
0

Publication Types

Select...

Relationship

0
0

Authors

Journals

citations
Cited by 0 publications
references
References 2 publications
0
0
0
Order By: Relevance

No citations

Set email alert for when this publication receives citations?