Results 21 to 30 of about 3,121 (160)
Modeling and Analysis of Micro-Spacecraft Attitude Sensing with Gyrowheel
This paper proposes two kinds of approaches of angular rate sensing for micro-spacecraft with a gyrowheel (GW), which can combine attitude sensing with attitude control into one single device to achieve a compact micro-spacecraft design.
Xiaokun Liu +3 more
doaj +1 more source
Stability of a tilt-controlling axial gap self-bearing motor with single-stator
This paper discusses the stability of a tilt-controlling axial gap self-bearing motor with a single stator. The motor consists of a stator and a disc rotor and is capable of controlling motor torque, axial position, and tilt angles.
Satoshi UENO, Ryo ISEKI, Changan JIANG
doaj +1 more source
Conversion control of a tilt tri-rotor unmanned aerial vehicle with modeling uncertainty
The tilt-rotor unmanned aerial vehicle (TRUAV) has vertical take-off and landing and high-speed flight capabilities through conversion and reconversion modes, thereby presenting wide application prospects.
Chao Chen +4 more
doaj +1 more source
Flight Mechanics Modeling of the New Configuration Tilt-rotor
The flight mechanical model of tilt-rotor UAV is the basis of designing flight control rate and analyzing flight characteristics.Based on the engineering reality, the nonlinear flight mechanics model of a new configuration tilt-rotor UAV is set up ...
Zhang Lian +3 more
doaj +1 more source
A conical passive magnetic bearing with constant stiffness
A nested conical passive magnetic bearing is presented. The bearing consists of a nested conical rotor inside a conical stator, i.e. two coaxial tilted rings of permanent magnets, both with a rectangular cross section.
R. Bjørk, C. R. H. Bahl
doaj +1 more source
Influence of tilt angle and the number of guide vane blades towards the Savonius rotor performance
Additional guide vane (GV) to the Savonius rotor is used to overcome the low rotor efficiency. This study is experimentally carried out to know the influence of guide vane in improving two blades Savonius rotor performance.
Waled Yahya +5 more
doaj +1 more source
The numerical calculation model for the aero-acoustic analysis of a tilt rotor was established by combining the free wake method and the FW-H (Ffowcs Williams-Hawkings) equation.
YUAN Mingchuan +4 more
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Giant Diffusion of Nanomechanical Rotors in a Tilted Washboard Potential
We present an experimental realization of a biased optical periodic potential in the low friction limit. The noise-induced bistability between locked (torsional) and running (spinning) states in the rotational motion of a nanodumbbell is driven by an elliptically polarized light beam tilting the angular potential. By varying the gas pressure around the
L. Bellando +4 more
openaire +3 more sources
The distributed electric tilt-rotor Unmanned Aerial Vehicle (UAV) combines the vertical take-off and landing (VTOL) capability of helicopters with the high-speed cruise performance of fixed-wing aircraft, offering a transformative solution for Urban Air ...
He Zhu +4 more
doaj +1 more source
Four-Dimensional Gait Surfaces for a Tilt-Rotor—Two Color Map Theorem
This article presents the four-dimensional surfaces that guide the gait plan for a tilt-rotor. The previous gaits analyzed in the tilt-rotor research are inspired by animals; no theoretical base backs the robustness of these gaits.
Zhe Shen, Yudong Ma, Takeshi Tsuchiya
doaj +1 more source

