Results 41 to 50 of about 6,732 (195)
Automatika, 2020 This paper presents the dynamic modelling and control technique for a tilt-rotor aerial vehicle operating in bi-rotor mode. This kind of aircraft combines two flight envelopes, making it ideal for scenarios that require hovering, vertical take-off ...
Nada El Gmili +3 more
doaj +1 more source
Design, 3D FEM Simulation and Prototyping of a Permanent Magnet Spherical Motor
Actuators, 2021 In recent years, large tilt angles, uniform magnetic flux distributions, strong forces, and large torques for motors have increasingly become important for robotics, biomedical, and automotive applications that have multi-degrees of freedom (MDOFs ...
Umut Yusuf Gündoğar +1 more
doaj +1 more source
Turning flight simulation of tilt-rotor plane with fluid-rigid body interaction
Journal of Thermal Science and Technology, 2020 Six degrees of freedom turning flight simulation is presented for a tilt-rotor aircraft represented by V-22 Osprey, considering interaction of fluid and rigid body in a coupled manner.
Ayato TAKII +3 more
doaj +1 more source
Analysis of the influence of transition state control strategy on structural load of quad-tiltrotor
Hangkong gongcheng jinzhanThere are complex structural load changes in the rotor during the tilt-transition of quad-tiltrotor aircraft,which can directly affect the life of the rotor.
HE Yongtao +3 more
doaj +1 more source
Applied Sciences, 2020 The tilt tri-rotor unmanned aerial vehicle (UAV) has three flight modes: the hover mode, the transition mode, and the fixed-wing mode. Controller design in the hover mode is the premise of realizing stable flight of this kind of UAV.
Guang He +3 more
doaj +1 more source
TILT-ROTOR AERODYNAMICS ACTIVITIES DURING THE NICETRIP PROJECT
, 2014 The aerodynamic re-design and characterization of the Erica tilt-rotor aircraft, carried out by some Partners of the NICETRIP consortium, is presented. The re-design activities concern some specific aircraft components, like the fuselage/wing fairing, the wing airfoils, the blade cuff and the rotor spinner.
VIGEVANO, LUIGI +5 more
openaire +3 more sources
Mathematical modeling and vertical flight control of a tilt-wing UAV [PDF]
, 2012 This paper presents a mathematical model and vertical flight control algorithms for a new tilt-wing unmanned aerial vehicle (UAV). The vehicle is capable of vertical take-off and landing (VTOL).
Aksit, Mahmut Faruk +15 more
core +1 more source
Empirical Modeling of Tilt-Rotor Aerodynamic Performance
, 2021 There has been increasing interest into the performance of electric vertical takeoff and landing (eVTOL) aircraft. The propellers used for the eVTOL propulsion systems experience a broad range of aerodynamic conditions, not typically experienced by propellers in forward flight, that includes large incidence angles relative to the oncoming airflow ...
openaire +2 more sources
Asynchronous Tilt Transition Control of Quad Tilt Rotor UAV
DronesTo address the challenges inherent in the transition flight control of QTR UAVs, this paper proposes an asynchronous tilt transition control framework that integrates NDIC with an ESO.
Xuebing Li +4 more
doaj +1 more source
Cost characteristics of tilt-rotor, conventional air and high speed rail short-haul intercity passenger service [PDF]
The cost analysis done to support an assessment of the potential for a small tilt-rotor aircraft to operate in short-haul intercity passenger service is described in detail.
Morlok, Edward K. +1 more
core +1 more source