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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| Format: | Thesis |
| Language: | English |
| Published: |
2020
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| Subjects: | |
| Online Access: | https://ir.uitm.edu.my/id/eprint/60049/1/60049.pdf |
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