System identification of aerodynamic derivatives for VTOL UAV

The establishment of an Aircraft Dynamic Model is a prerequisite to design navigation and control systems. However, aerodynamic models are not easily obtained for small- scaled aircraft model such as Unmanned Aerial Vehicles (UAVs) Simulated models are important towards the development of effective...

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Bibliographic Details
Main Author: Matiin Muhammad Hanifah Marican
Other Authors: Basman Elhadidi
Format: Final Year Project
Language:English
Published: Nanyang Technological University 2021
Subjects:
Online Access:https://hdl.handle.net/10356/150919
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Institution: Nanyang Technological University
Language: English
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