Control system development for unconventional aerobatic unmanned aerial vehicle with variable incidence wing

This final year project covers the design and development processes of control system for unconventional unmanned aerial vehicle (UAV). An aerobatic aircraft is designed to be equipped with variable incidence wing with an expectation to be able to perform both conventional aerobatic maneuvers as wel...

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Bibliographic Details
Main Author: Pham, Kim Hoan.
Other Authors: Go Tiauw Hiong
Format: Final Year Project
Language:English
Published: 2010
Subjects:
Online Access:http://hdl.handle.net/10356/40046
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Institution: Nanyang Technological University
Language: English

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