Enviar artigo por via de e-mail CRITERIAOF ORBITALCONTROLTHRUSTER OPTIMALALLOCATIONON BOARD OFGEOSTATIONARY SPACECRAFT
- Autores: Ermoshkin Y.M.1, Urusov V.M.1, Yermoshkin Y.M1, Urusov VM1
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Afiliações:
- Edição: Volume 12, Nº 1 (2011)
- Páginas: 92-96
- Seção: Articles
- ##submission.datePublished##: 15.03.2011
- URL: https://journals.eco-vector.com/2712-8970/article/view/505742
- ID: 505742
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Resumo
During designing of new, especially long-life geostationary spacecrafts we face a problem of rational orbital control
thruster allocation. In this paper we consider the possible criteria for solution of such problem and the results of their
application.
thruster allocation. In this paper we consider the possible criteria for solution of such problem and the results of their
application.
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Bibliografia
- Effects of interaction of electric thruster jets and spacecraft solar battareies / M. P. Burgasov,A. B.Nadiradzer, A. A. Chirov [at al.] // European Space Power Conference ; Graz,Austria. 23-27Aug. 1993. (ESAWPP-054,Aug. 1993).
- Разработка и поставка пакета прикладных программ для расчета воздействия струй СПД и ТКД на элементы КА: отчет оНИР.Тема№208-97040.Моск. гос. авиационный ин-т.М., 2001.
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