Results 41 to 50 of about 3,121 (160)
International Journal of Aerospace Engineering, 2019 A computational method is developed in order to predict the unsteady aerodynamic characteristics of the tilt-rotor aircraft in conversion mode. In this approach, the rotor is modeled as an actuator disk so that the effect of individual blades can be ...
Hao Chen
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Identification of subsystems in a tilt-rotor
, 2022 The present work has been carried out in the framework of the PIANO project (Path Identification for Active Noise Control), funded by EU Horizon 2020 and Clean Sky JU under the Grant Agreement no. 885976.
Serra López, Roger|| +4 more
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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
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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
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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
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An Experimental Verification of Rotation about an Arbitrary Axis of Magnetostrictive Motor [PDF]
한국정밀공학회지, 2018 This paper presents an experimental observation of the rotation of a magnetostrictive motor about an arbitrary axis using a Terfenol-D rod and a helical magnetic field.
Ha Gyun Lee +2 more
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Tilt-rotor multivariable attitude control with rotor state feedback
IFAC-PapersOnLine, 2016 In this paper, a multi-objective optimization-based methodology for rotorcraft attitude control law design is applied to a tilt-rotor case; the framework allows to enforce requirements of stability, performance, control action moderation, and safety.
PANZA, SIMONE +3 more
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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
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DronesWhile fixed, unactuated rotor tilt is increasingly utilised in commercial multi-rotor unmanned aerial vehicles (UAV), its impact on forward flight performance remains poorly documented in the literature.
Brendan H. P. Mullen +3 more
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Aeroelastic optimization of a composite tilt rotor
39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, 1998 Composite tilt rotor aeroelastic optimization is performed by using a mixed variational formulation based on exact intrinsic equations of motion for moving beams and a finite-state dynamic inflow theory. A composite box-beam model is used to represent the principal load carrying member of the rotor blade. The blade is discretized using finite elements.
Omer Soykasap, Dewey Hodges
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