Email this article Geo satellite attitude and orbit control: fixed orbit control thrasters
- Authors: Ermoshkin Y.M1, Raevsky VA1, Urusov VM1
-
Affiliations:
- JCS Academician M. F. Reshetnev Information Satellite Systems, Russia, Zheleznogorsk
- Issue: Vol 10, No 5 (2009)
- Pages: 82-87
- Section: Articles
- URL: https://journals.eco-vector.com/2712-8970/article/view/508598
- ID: 508598
Cite item
Full Text
Abstract
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.
About the authors
Yu M Ermoshkin
JCS Academician M. F. Reshetnev Information Satellite Systems, Russia, ZheleznogorskJCS Academician M. F. Reshetnev Information Satellite Systems, Russia, Zheleznogorsk
V A Raevsky
JCS Academician M. F. Reshetnev Information Satellite Systems, Russia, ZheleznogorskJCS Academician M. F. Reshetnev Information Satellite Systems, Russia, Zheleznogorsk
V M Urusov
JCS Academician M. F. Reshetnev Information Satellite Systems, Russia, ZheleznogorskJCS Academician M. F. Reshetnev Information Satellite Systems, Russia, Zheleznogorsk
References
- Kozlov, A. The outcomes and outlooks of the EDB Fakel propulsion units as part of the NPO PM spacecraft / A. Kozlov // Intern. cooperation in the future space missions involving electric propulsion : Intern. Workshop (Svetlogorsk. Russia, Sept. 16-17). Svetlogorsk, 2005.
- Electric Propulsion Subsystem development and application in Russia /Yu. Semenov, B. Sokolov,A. Borisenko et al. // Spacecraft Propulsion : 3rd Intern. Conf. (Cannes. 10-13 Oct. 2000). Cannes, 2005.
- Electric Propulsion Thruster Pointing Mechanism (TPM) For EUROSTAR 3000 : Design & DevelopmentTest Results / M. Falkner et al. // IEPC-2005-001 : The 29th Intern. Electric Propulsion Conf. (Princeton University. Oct. 31-Nov. 4, 2005). Princeton, 2005.
- Lubberstedt H. Solely EP based Orbit Control System on Small GEO Satellite / H. Lubberstedt, Th. Miesner, A. Winkler // IEPC-2007-274 :The 30th Intern. Electric Propulsion Conf. (Florence, Italy. Sept. 17-20, 2007). Florence, 2007.
Supplementary files
