Results 31 to 40 of about 3,121 (160)

Flight Characteristics of Quad Rotor Helicopter with Tilting Rotor

open access: yesThe Journal of Instrumentation, Automation and Systems, 2014
A quad rotor helicopter (QRH), a type of unmanned aerial vehicle (UAV), uses a tilted attitude to generate a horizontal thrust component in the flying direction. In the case of autonomous control, the attitude control system is used to tilt the airframe against disturbances such as crosswinds.
Akitaka Imamura   +3 more
openaire   +1 more source

Design and Implementation of a Novel Tilt-Rotor Tri-Copter UAV Configuration

open access: yesEngineering Proceedings
Hover-capable unmanned aerial vehicles (UAVs), including rotary-wing UAVs such as unmanned helicopters, multi-rotor drones, and tilt-rotor UAVs, are widely employed due to their hovering capabilities.
Zishi Shen, Fan Liu
doaj   +1 more source

Hurdle-Hop Simulation of Tilt-Rotor Aircraft Based on Optimal Control Theory

open access: yesXibei Gongye Daxue Xuebao, 2020
Aiming at simulating the hurdle-hop of tilt-rotor aircraft in forward flight near the ground, two models of numerical simulation and analysis based on optimal control theory were proposed.

doaj   +1 more source

Keen Investigation of the Electromagnetic Scattering Characteristics of Tiltrotor Aircraft Based on Dynamic Calculation Method

open access: yesPhotonics, 2021
To study the radar characteristics of the tiltrotor aircraft when considering rotor rotation and tilting actions, a dynamic calculation method (DCM) based on physical optics and physical theory of diffraction is presented. The results show that the radar
Zeyang Zhou   +3 more
doaj   +1 more source

Aerodynamic Configuration and Stability Analysis of a Split-Type Tilt-Rotor Cargo Flying Vehicle

open access: yesAerospace
The flying car, academically known as electric vertical takeoff and landing (eVTOL) aircraft, is one of the core vehicles for low-altitude transportation. The split-type tilt-rotor cargo flying vehicle that is composed of tilt rotors, a fixed wing, and a
Songyang Li   +6 more
doaj   +1 more source

Wind farm modelling of tilted rotors

open access: yesJournal of Physics: Conference Series
Abstract This study explores the benefits of tilted rotors in wind farms, focusing on a 3x3 grid of 10MW turbines and a 153-turbine farm modelled after the Hollandse-Kust West site with 15MW turbines. Computational Fluid Dynamics models ranging from mid to higher order, including FarmFlow (Parabolic RANS), TNO-VBM (RANS), and NREL-SOWFA (
Vimalakanthan, K.   +2 more
openaire   +2 more sources

Effect of Rotor Tilt on the Gust Rejection Properties of Multirotor Aircraft

open access: yesDrones, 2022
In order to operate safely in windy and gusty conditions, multirotor VTOL aircraft require gust resilience. This paper shows that their gust rejection properties can be improved by applying a small amount of fixed outward rotor tilt. Standard aerodynamic
James F. Whidborne   +2 more
doaj   +1 more source

Horizontal Fixed Attitude Flight of Quad Rotor Helicopter with Tilting Rotor

open access: yesJournal of Robotics and Mechatronics, 2023
A quad rotor helicopter (QRH), a type of unmanned aerial vehicle (UAV), uses a tilted attitude to generate a horizontal thrust component in the flying direction. In the case of autonomous control, the attitude control system is used to tilt the airframe against disturbances such as crosswinds.
openaire   +1 more source

Wind Disturbance Rejection Control Of Tilt Rotor Aircraft In Transition Phase Based On Improved Active Disturbance Rejection Control

open access: yesJournal of Applied Science and Engineering, 2023
The tilt rotor aircraft is capable of both low-speed hovering and high-speed flight, which has a larger flight envelope. However, during its transition phase, due to the change of the mechanical structure, the dynamic characteristics of the rotor and the
Liben Yang   +3 more
doaj   +1 more source

Wind Field Disturbance Analysis and Flight Control System Design for a Novel Tilt-Rotor UAV

open access: yesIEEE Access, 2020
The wind field has a great influence on the control stability of Tilt-rotor unmanned aerial vehicle (UAV), especially during the take-off and landing phase.
Qian Zhang   +4 more
doaj   +1 more source

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