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UAV Roadmap Overview [PDF]

open access: yes, 2006
Schmitt, Dirk-Roger
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A back-stepping control strategy for the Tri-rotor UAV

2012 24th Chinese Control and Decision Conference (CCDC), 2012
Over the last decade, the use of Unmanned Aerial Vehicles (UAVs) has increased dramatically in both military surveillance and in civilian search and rescue operations.
Gaurav Raina
exaly   +2 more sources

Coupled CFD/MBD Method for a Tilt Tri-rotor UAV in Conversion of Flight Modes

International Journal of Computational Fluid Dynamics, 2020
Aerodynamic characteristics of tilt-rotor UAVs are usually simulated by computational fluid dynamics (CFD) only, and the fuselage/wing is fixed in simulations.
Guilin Wen, Hanfeng Yin
exaly   +2 more sources

Modeling and attitude control of a tilt tri-rotor UAV

2017 36th Chinese Control Conference (CCC), 2017
The tilt tri-rotor UAV which combines the advantages of both rotary wing and fixed wing vehicle, offers the capability of hover, vertical take-off and landing and fast forward movement. Because of the complex structure and aerodynamics, the modeling and control of tilt tri-rotor UAV reamians a problem.
Li Yu, Daibing Zhang
exaly   +2 more sources

Simulation verification of Flight Control of a tilt tri-rotor UAV Using X-plane

2020 39th Chinese Control Conference (CCC), 2020
In order to realize the rapid verification of the control algorithm of the tilt tri-rotor UAV, this paper presents the design and implementation of the SIL(software in the loop) simulation system using X-plane software. Firstly, According to the actual parameters of the designed tilt tri-rotor UAV, a full scale digital model that can simulate actual ...
Xiangke Wang
exaly   +2 more sources

Immersion and Invariance-based Sliding Mode Attitude Control of Tilt Tri-rotor UAV in Helicopter Mode

International Journal of Control, Automation and Systems, 2020
In this paper, we propose an immersion and invariance-based sliding mode controller for a tilt tri-rotor unmanned aerial vehicle subjects to parameter perturbation, unmodeled dynamics, and external disturbances. The control scheme is divided into three parts, including the disturbance observer, the attitude controller, and the control allocation ...
Li Yu, Guang He, Xiangke Wang
exaly   +2 more sources

Modeling and Controller Design of a Tilt Tri-Rotor UAV

Lecture Notes in Mechanical Engineering, 2022
Vu Dinh Quy   +3 more
exaly   +2 more sources

Tilt Tri-Rotor UAV Attitude Control in Hover Mode

Lecture Notes in Electrical Engineering, 2023
Zhihao Cai, Jiang Zhao, Ningjun Liu
exaly   +2 more sources

Sliding Mode Control for the hovering flight of a Tilt tri-rotor UAV

2022 11th International Conference on Control, Automation and Information Sciences (ICCAIS), 2022
Le Thi Tuyet Nhung   +3 more
exaly   +3 more sources

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