SATELLITE TRACKING SYSTEM

Miss. Chetana M. Patil, Miss. Samidha S. Virkud, Miss. Nisha B. Patil, Miss. Heena E. Mulani, Ms. Rupali Pande

Abstract


Satellites in nominally geostationary orbits possess diurnal motion which reasons the plain function of the spacecraft .The motion of the satellite tv for pc consequently must be tracked through the earth station antenna. This mission simulates the overall performance of satellite via measuring the parameters including Azimuth perspective, Elevation attitude, apogee, perigee inclination of orbital plane to equatorial plane, argument of ascending node, argument of periapsis, etc. Satellite revolving in the earth produces a beacon signal which is taken by the antenna, by this beacon signal the antenna understands where the satellite is residing in earth’s atmosphere. This is called as tracking of satellite by antenna of base station. In addition the project is working in step tracking mode means similar to the operation of the manual tracking scheme except that a small computer is used to perform the functions of the operator.


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References


Amol Dhumal, Yutika Patwa, Manali Shilimkar, ‘Tracking System For Satellite Communication’ ‘International Journal of Adavnace Research In Computer Engg & Technology’ Volume 3 issue 11, Nov 2014.

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Chang-Ho Cho, Sang-Hyo Lee, Tae-Yong Kwon and Cheol Lee, ‘ Antenna Control System Using Step Tracking Algorithm with H∞ Controller’ ‘International Journal Of Control, Automation and Systems’ Volume 1, No.1, March 2003.

G.J.Hawkins, D.J.Edwards, Prof. J.P.McGeehan, ‘Tracking system for satellite communications’.


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