The development of a fixed wing aircraft analysis and design flight dynamic software
The present work focused on the development of computer software for flight dynamic analysis and controlling the behavior of a fixed-wing aircraft. For a given aircraft geometry, mass and inertia properties, and flight conditions, the software was designed in such a way to start the estimation of ae...
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主要作者: | Ahmad Alaian, Ahmad Eshtiwey |
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格式: | Thesis |
語言: | English English English |
出版: |
2016
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主題: | |
在線閱讀: | http://eprints.uthm.edu.my/818/1/24p%20AHMAD%20ESHTIWEY%20AHMAD%20ALAIAN.pdf http://eprints.uthm.edu.my/818/2/AHMAD%20ESHTIWEY%20AHMAD%20ALAIAN%20COPYRIGHT%20DECLARATION.pdf http://eprints.uthm.edu.my/818/3/AHMAD%20ESHTIWEY%20AHMAD%20ALAIAN%20WATERMARK.pdf |
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