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Abstract: <br /> <br /> <br /> <br /> <br /> Development of flight simulation by using joystick to control the elevator software (In Flight Modelling Software/IFMS) has been studied in this thesis. This software can be used as a tool to predict the flight character...

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Main Author: (NIM. 235 97 015), Hernawati
Format: Theses
Language:Indonesia
Online Access:https://digilib.itb.ac.id/gdl/view/8121
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Institution: Institut Teknologi Bandung
Language: Indonesia
id id-itb.:8121
spelling id-itb.:81212017-09-27T15:37:08Z#TITLE_ALTERNATIVE# (NIM. 235 97 015), Hernawati Indonesia Theses INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/8121 Abstract: <br /> <br /> <br /> <br /> <br /> Development of flight simulation by using joystick to control the elevator software (In Flight Modelling Software/IFMS) has been studied in this thesis. This software can be used as a tool to predict the flight characteristics of a testing aircraft. <br /> <br /> <br /> <br /> <br /> The IFMS was developed through functionality approach in requirements analysis by using SA/RT method. TOOD method is used for design which determines the object by translate the SA/RT model. Development tool for design implementation by using Microsoft Developer Studio97 Visual C++ version 5.0. with Windows 95 as operating system environment. <br /> <br /> <br /> <br /> <br /> Software tests were done for unit test, and integration test by using black box method, which establishes that the software meet its requirements. Validation test was done by comparing the IFMS execution result and the existing software (PC-offline) execution result, which establishes the IFMS is valid. text
institution Institut Teknologi Bandung
building Institut Teknologi Bandung Library
continent Asia
country Indonesia
Indonesia
content_provider Institut Teknologi Bandung
collection Digital ITB
language Indonesia
description Abstract: <br /> <br /> <br /> <br /> <br /> Development of flight simulation by using joystick to control the elevator software (In Flight Modelling Software/IFMS) has been studied in this thesis. This software can be used as a tool to predict the flight characteristics of a testing aircraft. <br /> <br /> <br /> <br /> <br /> The IFMS was developed through functionality approach in requirements analysis by using SA/RT method. TOOD method is used for design which determines the object by translate the SA/RT model. Development tool for design implementation by using Microsoft Developer Studio97 Visual C++ version 5.0. with Windows 95 as operating system environment. <br /> <br /> <br /> <br /> <br /> Software tests were done for unit test, and integration test by using black box method, which establishes that the software meet its requirements. Validation test was done by comparing the IFMS execution result and the existing software (PC-offline) execution result, which establishes the IFMS is valid.
format Theses
author (NIM. 235 97 015), Hernawati
spellingShingle (NIM. 235 97 015), Hernawati
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author_facet (NIM. 235 97 015), Hernawati
author_sort (NIM. 235 97 015), Hernawati
title #TITLE_ALTERNATIVE#
title_short #TITLE_ALTERNATIVE#
title_full #TITLE_ALTERNATIVE#
title_fullStr #TITLE_ALTERNATIVE#
title_full_unstemmed #TITLE_ALTERNATIVE#
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url https://digilib.itb.ac.id/gdl/view/8121
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