Email this article GEOSTATIONARY SPACECRAFT ATTITUDE AND ORBIT CONTROL BY MOTIONLESS ORBIT CONTROL THRUSTERS
- Authors: Yermoshkin Y.M1, Raevsky VA1, Urusov VM1
-
Affiliations:
- Issue: Vol 10, No 4 (2009)
- Pages: 100-105
- Section: Articles
- URL: https://journals.eco-vector.com/2712-8970/article/view/508597
- ID: 508597
Cite item
Full Text
Abstract
There is considered the application of the geostationary SC orbit control thrusters to attitude and orbit control together . It is analyzed the scheme of motionless thrusters. It is given the possible method to fulfill the orbit control thrusters firings with a control moments creation. It is considered the preferences and deficiencies of this method.
References
- Kozlov, A. The outcomes and outlooks of the EDB Fakel propulsion units as part of the NPO PM spacecraft / A. Kozlov // International cooperation in the future space missions involving electric propulsion : International Workshop (Svetlogorsk. Sept. 16-17, 2005). Svetlogorsk, 2005.
- Semenov, Yu. Electric Propulsion Subsystem development and application in Russia / Yu. Semenov, B. Sokolov, A. Borisenko [et al.] // Spacecraft Propulsion : 3rd International Conference (Cannes. 10-13 Oct. 2000). Cannes, 2005.
- Electric Propulsion Thruster Pointing Mechanism (TPM) For EUROSTAR 3000: Design & Development Test Results / M. Falkner [et al.] // IEPC-2005-001 : The 29th International Electric Propulsion Conference (Okt. 31-Nov . 4, 2005). Princeton University . Princeton, 2005.
Supplementary files
