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
格式: Thesis
语言:English
English
English
出版: 2016
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在线阅读:http://eprints.uthm.edu.my/818/1/24p%20AHMAD%20ESHTIWEY%20AHMAD%20ALAIAN.pdf
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