Geo satellite attitude and orbit control: fixed orbit control thrasters


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Аннотация

The paper describes the enhanced application ofhigh-economical electro-jet orbit control thrusters for geostationary satellites; in particular, generation of controlling moments to the benefit of satellite attitude determination and control subsystems in the course of orbit control maneuvers ongoing. The scheme with thrusters fixed on a satellite body is analyzed. Possible orbit control session procedures are proposed on the basis of controlling moments generation. Advantages and disadvantages of the proposed approach are analyzed.

Об авторах

Yu M Ermoshkin

V A Raevsky

V M Urusov

Список литературы

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© Ermoshkin Y.M., Raevsky V.A., Urusov V.M., 2009

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Эта статья доступна по лицензии Creative Commons Attribution 4.0 International License.