Synthesizing Spacecraft Orbits with High Inclinations Using Venusian Gravity Assists View Full Text


Ontology type: schema:ScholarlyArticle     


Article Info

DATE

2019-01

AUTHORS

Yu. F. Golubev, A. V. Grushevskii, V. V. Koryanov, A. G. Tuchin, D. A. Tuchin

ABSTRACT

An adaptive, semi-analytical, and geometrically clear method for synthesis of sequences of Venusian gravity-assist maneuvers setting the desired inclination of a spacecraft orbit is proposed. The geometric constraint on the maximum possible inclination of a spacecraft orbit, which depends on the asymptotic spacecraft velocity relative to Venus, and the dynamic constraint (arising when a gravity-assist maneuver is performed) on the angle of rotation of the vector of asymptotic velocity relative to Venus are considered simultaneously. More... »

PAGES

24-26

References to SciGraph publications

Journal

TITLE

Doklady Physics

ISSUE

1

VOLUME

64

Author Affiliations

Identifiers

URI

http://scigraph.springernature.com/pub.10.1134/s1028335819010087

DOI

http://dx.doi.org/10.1134/s1028335819010087

DIMENSIONS

https://app.dimensions.ai/details/publication/pub.1113204512


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