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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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Bibliographic Details
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
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Summary: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.