Motion Equations and Attitude Control in the Vertical Flight of a VTOL Bi-Rotor UAV: Part 2

被引:1
作者
Musoles, Jose Luis [1 ]
Garcia-Nieto, Sergio [1 ]
Simarro, Raul [1 ]
Ramos, Cesar [1 ]
机构
[1] Univ Politecn Valencia, Inst Automat Informat Ind, Camino Vera S-N, Valencia 46022, Spain
关键词
tilt rotors; non-linear dynamics; simulation; vertical take-off; fixed wing; aerodynamics; QUADROTOR; TRACKING;
D O I
10.3390/electronics13132497
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper gathers the dynamical modeling of an unmanned aircraft and the design and simulation of the control system, allowing it to perform a Vertical Take-Off (VTOL) maneuver, a fixed-wing (FW) flight and a transition between the two configurations using two tilting rotors (Bi-Tilt). These Unmanned Aerial Vehicles (UAVs) operating in this configuration are categorized as Hybrid UAVs, for their capability of having a dual flight envelope: flying like a multi-rotor and navigating like a traditional fixed-wing aircraft, allowing the drone to perform complex missions where these two flight configurations are essential. This work exhibits the Bi-Rotor non-linear dynamics, valid for both flight configurations, the design of the control algorithm for stability and navigation, and a simulation of a complete flight mission.
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页数:24
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