Perching aircraft dynamics and control optimization

This final year project covers the optimization of aircraft perching maneuver through geometric reconfiguration or morphing. A novel Unmanned Aerial Vehicle (UAV) model which adopts canard configuration and variable-incidence outer wings is specially designed for the analysis of perching maneuver. A...

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Bibliographic Details
Main Author: Mau, Zao Min.
Other Authors: Go Tiauw Hiong
Format: Final Year Project
Language:English
Published: 2009
Subjects:
Online Access:http://hdl.handle.net/10356/16202
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Institution: Nanyang Technological University
Language: English

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