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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| Format: | Thesis |
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2016
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| Online Access: | http://eprints.uthm.edu.my/8892/ http://eprints.uthm.edu.my/8892/1/AHMAD_ESHTIWEY_ALAIAN.pdf |