GEOSTATIONARY SPACECRAFT ORBIT SLAVING AND MANEUVER: THRUSTERS ON DRIVES INSTALLATION SCHEME


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In this article we consider increase of application of geostationary SC orbit slaving and maneuver thrusters, particularly for creation of control moments for slaving and maneuver system of SC simultaneously with orbit correction procedures. We analyze thrusters on drives installation scheme, which provides for alteration of engine position against spacecraft (pointing mechanism). We also present possible method for orbit slaving procedures with the account of control moments creation decision. And we analyze merits and demerits of the given and the other slaving and maneuver approaches.

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Bibliografia

  1. Проведение ориентации и коррекции орбиты геостационарного КА: схема с неподвижным закреплением двигателей коррекции / Ю. М. Ермошкин, В. А. Раевский, В. М. Урусов // Вестник СибГАУ. Красноярск, 2009. Вып. 4(25). С. 99. 2.
  2. Electric propulsion thruster pointing mechanism (TPM) for Eurostar 3000: design and development test results / M. Falkner [et al.] // The 29th Int. electric propulsion conference (Princeton University, Okt. 31, Nov. 4, 2005). IEPC-2005-001.
  3. Lubberstedt H., Miesner Th., Winkler A. Solely EP based Orbit Control System on Small GEO Satellite // The 30th International Electric Propulsion Conference (Florence, Sept. 17-20, 2007). IEPC-2007-274.

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Declaração de direitos autorais © Ermoshkin Y.M., Raevskiy V.A., Urusov V.M., Yermoshkin Y.M., Raevsky V.A., Urusov V.M., 2010

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Este artigo é disponível sob a Licença Creative Commons Atribuição 4.0 Internacional.

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