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Design And Analysis Of Safest Geo Satellite Launching And Tracking System

Tengku Jalil, Tengku Nur Amirah (2016) Design And Analysis Of Safest Geo Satellite Launching And Tracking System. Project Report. UTeM, Melaka, Malaysia. (Submitted)

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Abstract

Satellite is any object that orbit or around the earth. There are three types of satellite orbit which are low earth orbit (LEO), medium earth orbit (MEO) and geostationary orbit (GEO). The satellite need to pass through three stages of orbit in order to reach the final destination. During the launching, a launch vehicle brings the spacecraft together and the launch vehicle leave the launch platform whether on land, sea or in the air until the spacecraft is separated and safely on its way. Tracking of satellite will be done at earth station to make sure the spacecraft not slip out of orbit. This project proposes the design and analysis of launching and tracking satellite and then compare the result of calculation and simulation. The project is mainly focus on the study literature of satellite technology of launching and tracking system. The calculation involved the parameter that affect the launching/ tracking system such as speed, time taken every segment, process stage by stages, stability, tracking and other related parameter. The project outcome is to overcome the lack of knowledge about satellite in FTK.

Item Type: Final Year Project (Project Report)
Uncontrolled Keywords: Signal processing, Artificial satellites in telecommunication, Electronic news gathering
Subjects: T Technology > T Technology (General)
T Technology > TK Electrical engineering. Electronics Nuclear engineering
Divisions: Library > Final Year Project > FTK
Depositing User: Mohd Hannif Jamaludin
Date Deposited: 19 Feb 2018 06:20
Last Modified: 19 Feb 2018 06:20
URI: http://digitalcollection.utem.edu.my/id/eprint/20383

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