The decision problem of choosing the parameters of the orbital structure of the multi-purpose space systems

Аuthors

Kiyko A. S.

Company “Space special-purpose systems corporation “Kometa”, 5, Velozavodskaya str., Moscow, 115280, Russia

e-mail: galaktika7@list.ru

Abstract

The problem of choice of the orbital structure of the spacecraft with a long term of active existence in highly elliptical orbits multipurpose space system is consider in this article. The spacecraft solves the problem of monitoring of the Earth's surface and bring the information to subscribers of this space system. The author say that for choice the orbital structure may be used an approach, based on consideration of spatial-temporal characteristics of the system and the time of the maximum permitted degradation.

Keywords:

orbital structure; orbital parameters; evolution; spacecraft; method of estimating the characteristics

Download