Email this article CRITERIAOF ORBITALCONTROLTHRUSTER OPTIMALALLOCATIONON BOARD OFGEOSTATIONARY SPACECRAFT
- Authors: Ermoshkin Y.M.1, Urusov V.M.1, Yermoshkin Y.M1, Urusov VM1
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Affiliations:
- Issue: Vol 12, No 1 (2011)
- Pages: 92-96
- Section: Articles
- Published: 15.03.2011
- URL: https://journals.eco-vector.com/2712-8970/article/view/505742
- ID: 505742
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Abstract
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.
Keywords
About the authors
Yuriy Mikhaylovich Ermoshkin
Email: erm@iss-reshetnev.ru
Vladimir Mikhaylovich Urusov
Yu M Yermoshkin
V M Urusov
References
- 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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