THREE AXIS STABILIZATION SATELLITE MODELING AND ITS CONTROL SYSTEM | ||||
| The International Conference on Electrical Engineering | ||||
| Article 63, Volume 2, 2nd International Conference on Electrical Engineering ICEENG 1999, November 1999, Page 648-662 PDF (1.99 MB) | ||||
| Document Type: Original Article | ||||
| DOI: 10.21608/iceeng.1999.62585 | ||||
 View on SCiNiTO | ||||
| Authors | ||||
| Gamel M.I. Selim1; Ayman Elshabrawy2 | ||||
| 1Ph.D, Dept of radar and guidance ,Egyption armed force | ||||
| 2Msc, Egyptian armed force. | ||||
| Abstract | ||||
| Satellite control is considered as one of the most modern spacecraft technology. The main advantage of satellite is its ability to obtain a global look at large area of the earth's surface, therefor a system of three satellites in geosynchronous orbit can cover almost all of the earth's surface. This led to the application of satellites in several areas, such as communications by high frequency line-of -sight radio links, photography for meteorology, earth resources and navigation for aircraft and ships.This paper introduce the design and the computer simulate of the attitude control system for three axis stabilization satellite | ||||
| Keywords | ||||
| Satellite; Three axes stabilization | ||||
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