Flight dynamic stability performance of the baseline-ix blended-wing-body unmanned aerial system using flight simulator / Shahrean Zainurin

The flight quality or behaviour of a blended-wing-body (BWB) unmanned aerial system (UAS) could be gathered and evaluated through virtual simulation or software-in-theloop (SITL) simulation. This is done through a specific setup between a ground control station (GCS) software, Mission Planner and...

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Bibliographic Details
Main Author: Zainurin, Shahrean
Format: Thesis
Language:English
Published: 2020
Subjects:
Online Access:https://ir.uitm.edu.my/id/eprint/60049/1/60049.pdf
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