Digital compass for inertial navigation system / Nuridora Abdul Razak

This paper presents the design of a digital compass for Inertial Navigation System (INS). The compass application can be implemented as a functional building block in navigation tracking device. The design is simple and low cost, made it suitable to be embedded on the control system of an aircraft o...

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Bibliographic Details
Main Author:	Abdul Razak, Nuridora
Format:	Thesis
Language:	English
Published:	2006
Subjects:	Aeronautics Aeronautical engineering
Online Access:	https://ir.uitm.edu.my/id/eprint/68456/1/68456.pdf
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id	my-uitm-ir.68456
record_format	uketd_dc
spelling	my-uitm-ir.684562022-12-05T02:18:19Z Digital compass for inertial navigation system / Nuridora Abdul Razak 2006 Abdul Razak, Nuridora Aeronautics. Aeronautical engineering This paper presents the design of a digital compass for Inertial Navigation System (INS). The compass application can be implemented as a functional building block in navigation tracking device. The design is simple and low cost, made it suitable to be embedded on the control system of an aircraft or gliders, among others. Using magnetic sensor and accelerometer, the digital compass will give the heading and attitude of the aircraft which is the pitch and roll. It is programmed on the PIC18F2520 microcontroller using C language. The application is intended for the use in Malaysia with considering zero declination. 2006 Thesis https://ir.uitm.edu.my/id/eprint/68456/ https://ir.uitm.edu.my/id/eprint/68456/1/68456.pdf text en public degree Universiti Teknologi MARA (UiTM) Faculty of Electrical Engineering
institution	Universiti Teknologi MARA
collection	UiTM Institutional Repository
language	English
topic	Aeronautics Aeronautical engineering
spellingShingle	Aeronautics Aeronautical engineering Abdul Razak, Nuridora Digital compass for inertial navigation system / Nuridora Abdul Razak
description	This paper presents the design of a digital compass for Inertial Navigation System (INS). The compass application can be implemented as a functional building block in navigation tracking device. The design is simple and low cost, made it suitable to be embedded on the control system of an aircraft or gliders, among others. Using magnetic sensor and accelerometer, the digital compass will give the heading and attitude of the aircraft which is the pitch and roll. It is programmed on the PIC18F2520 microcontroller using C language. The application is intended for the use in Malaysia with considering zero declination.
format	Thesis
qualification_level	Bachelor degree
author	Abdul Razak, Nuridora
author_facet	Abdul Razak, Nuridora
author_sort	Abdul Razak, Nuridora
title	Digital compass for inertial navigation system / Nuridora Abdul Razak
title_short	Digital compass for inertial navigation system / Nuridora Abdul Razak
title_full	Digital compass for inertial navigation system / Nuridora Abdul Razak
title_fullStr	Digital compass for inertial navigation system / Nuridora Abdul Razak
title_full_unstemmed	Digital compass for inertial navigation system / Nuridora Abdul Razak
title_sort	digital compass for inertial navigation system / nuridora abdul razak
granting_institution	Universiti Teknologi MARA (UiTM)
granting_department	Faculty of Electrical Engineering
publishDate	2006
url	https://ir.uitm.edu.my/id/eprint/68456/1/68456.pdf
_version_	1783735780448927744

Digital compass for inertial navigation system / Nuridora Abdul Razak

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