scholarly journals Experimental Study on a Test Stand for Magnetically Levitated Vehicle Dynamics Evaluation

2013 ◽  
Vol 79 (799) ◽  
pp. 507-518 ◽  
Author(s):  
Shuichiro OTA ◽  
Toshiaki MURAI ◽  
Hiroshi YOSHIOKA ◽  
Yoshiaki TERUMICHI
1996 ◽  
Vol 116 (3) ◽  
pp. 124-131
Author(s):  
Takashi Hikihara ◽  
Yoshihisa Hirane ◽  
Takeshi Uejyou

2009 ◽  
Vol 75 (751) ◽  
pp. 616-622
Author(s):  
Haruo IWANO ◽  
Satoshi NISHIOKA ◽  
Takahisa KAMIKURA ◽  
Nobuo MASAKI ◽  
Shougo KANAGAWA ◽  
...  

2019 ◽  
Vol 9 (6) ◽  
pp. 1151 ◽  
Author(s):  
Pongsathorn Raksincharoensak ◽  
Sato Daisuke ◽  
Mathias Lidberg

In this paper a vehicle dynamics control system is designed to compensate the change in vehicle handling dynamics of lightweight vehicles due to variation in loading conditions and the effectiveness of the proposed design is verified by simulations and an experimental study using a fixed-base driving simulator. Considering the electrification of future mobility, the target vehicle of this research is a lightweight vehicle equipped with in-wheel motors that can generate an additional direct yaw moment by transverse distribution of traction forces to control vehicle yawing as well as side slip motions. Previously, the change in vehicle handling dynamics for various loading conditions have been analyzed by using a linear two-wheel vehicle model in planar motion and a control law of the DYC system based on feed-forward of front steering angular velocity and feedback of vehicle yaw rate. The feed-forward controller is derived based on the model following control with approximation of the vehicle dynamics to 1st-order transfer function. To make the determination of the yaw rate feedback gain model-based and adaptable to various vehicle velocity conditions, this paper selects a method where the yaw rate feedback gain in the DYC system is determined in a way that the steady-state yaw rate gain of the controlled loaded vehicle matches the gain of the unloaded vehicle. The DYC system is simulated in a single lane change maneuver to confirm the improved responsiveness of the vehicle while simulations of a double-lane change maneuver with a driver steering model confirms the effectiveness of the DYC system to support tracking control. Finally, the effectiveness of the proposed DYC system is also verified in an experimental study with ten human drivers using a fix-based driving simulator.


1993 ◽  
Vol 59 (567) ◽  
pp. 3291-3298
Author(s):  
Hideyuki Tamura ◽  
Zhi-Xiang Xu ◽  
Nobuyuki Souwa ◽  
Jun-ichi Matsunaga ◽  
Emil Gad Halim

2015 ◽  
Vol 81 (832) ◽  
pp. 15-00384-15-00384 ◽  
Author(s):  
Masashi KABUTOMORI ◽  
Toshiaki MURAI ◽  
Hiroshi YOSHIOKA ◽  
Yoshiaki TERUMICHI

2017 ◽  
Vol 83 (845) ◽  
pp. 16-00304-16-00304
Author(s):  
Masashi KABUTOMORI ◽  
Toshiaki MURAI ◽  
Hiroshi YOSHIOKA ◽  
Yoshiaki TERUMICHI

2005 ◽  
Vol 13 (4) ◽  
pp. 654-662
Author(s):  
P.K.C. Wang ◽  
J. Yee ◽  
C.Y. Xia ◽  
M. Mokuno ◽  
F.Y. Hadaegh

2018 ◽  
Vol 234 ◽  
pp. 01002 ◽  
Author(s):  
Filip Panayotov ◽  
Ivan Dobrev ◽  
Fawaz Massouh ◽  
Michael Todorov

This paper presents the results from an experimental study of the aerodynamic performance and efficiency of a model helicopter rotor in steady hover at Reynolds numbers below 70000. Results are shown for a two-, three- and four-bladed rotor configuration for various pitch angles and speeds of rotation. The influence of the rotor solidity on the aerodynamic efficiency in terms of the Figure of Merit is highlighted. The profile drag component is evaluated as a function of the Reynolds number. The internal friction losses of the test stand are estimated and taken into account in all measurements. A brief description of the designed test stand is provided. The experimental setup allows for the measurement of thrust and torque of helicopter rotors with diameters of up to 1 meter, for pitch angles varying from -12° to +24° and for rotational speeds of up to 3000 RPM. Conclusions are drawn about the aerodynamic performance and efficiency of the studied rotor configurations. This experimental study provided a significant database, which will serve for validation purposes.


Author(s):  
P.M. Heerwan ◽  
S.M. Asyraf ◽  
A.N. Efistein ◽  
C.H. Seah ◽  
J.M. Zikri ◽  
...  

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