Design of Flight Control System for a Novel Tilt-Rotor UAV

This paper presents the control system design process of a novel tilt-rotor unmanned aerial vehicle (TRUAV). First, a new configuration scheme with the tilting rotors is designed. Then, the detailed nonlinear mathematical model is established, and the parameters are acquired from designed experiment...

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Bibliographic Details
Main Authors: Zaibin Chen, Hongguang Jia
Format: Article
Language:English
Published: Wiley 2020-01-01
Series:Complexity
Online Access:http://dx.doi.org/10.1155/2020/4757381
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