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

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 (FYP)
Language:English
Published: 2010
Subjects:
DRNTU::Engineering::Mechanical engineering::Control engineering
DRNTU::Engineering::Aeronautical engineering::Aircraft
Online Access:http://hdl.handle.net/10356/40046

Internet

http://hdl.handle.net/10356/40046

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