نتایج جستجو برای: freedom dynamic model

تعداد نتایج: 2439930  

ژورنال: Journal of Railway Research 2014
Betanzo-Quezada, E., Obregón-Biosca, S.A., Romero, J.A.,

In this paper a two-degree-of-freedom model representing the sprung mass and the sloshing cargo in a vehicle is proposed to study the dynamic interaction of a sloshing cargo and the carrying vehicle, to simulate the dynamic wheel forces on the rails as a result of lateral perturbations derived from turnings along the railway path and the resultant cargo sloshing. The use of the Fourth- and T...

Hemati, Sepehri,

In this paper, the 1/4 vehicle model have been simulated. The vehicle body acceleration using optimal control has been optimized. The vehicle ride comfort is achieved by using robust control, and it has been compared with optimal control. The active suspension can help the vehicle to have a good dynamic behavioral. In this paper, two degrees of freedom dynamic vibration model of a general ve...

 In practice, clearances in the joints are inevitable due to tolerances, and defects arising from design and manufacturing. In the presence of clearance at a joint, a mechanism gains some additional, uncontrollable degrees of freedom which are the source of error. Moreover, joints undergo wear and backlashes and so cannot be used in precision mechanisms. In this study, the dynamic behaviour of ...

Journal: :Research in Computing Science 2013
Carlos Alberto Yahir Hervert Cano Angel Rodríguez-Liñán Luis M. Torres-Treviño

The inverse dynamic model allows to compute the torques for each of the degrees of freedom of a robot knowing the positions, velocities and accelerations. In contrast, direct dynamic model is used to calculate the positions, velocities and accelerations knowing the torques for each of the degrees of freedom. Most of the times is difficult to obtain the direct dynamic model analytically because ...

Journal: :journal of applied and computational mechanics 2015
mostafa mohagheghi ali salehzadeh nobari alireza seyed roknizadeh

in the present paper, the aeroelastic stability of helicopter rotor blade is determined using aeroelastic frequency response function. the aeroelastic model of blade is obtained by combining dowell - hodges beam model with loewy unsteady aerodynamic theory which considers an unsteady wake beneath the rotor. equations are formed and aeroelastic frequency response functions are obtained by invert...

Journal: :نظریه های اجتماعی متفکران مسلمان 0
علی فتوتیان دانشجوی دکتری جامعه شناسی دانشگاه شیراز سید سعید زاهد زاهدانی دانشیار جامعه شناسی دانشگاه شیراز و عضو پژوهشکدۀ تحول در علوم انسانی

the first aim of this article is to present zahed’s conceptual–operational model of freedom on the basis of islamic thoughts.  the second goal is to distinguish how freedom would run in the islamic society according to this operational model. finally, we will talk about the differences between this new conceptualization of freedom and the secular one. we will introduce theoretical, social and c...

S. A. A. Moosavian and A. Mirani,

Mobile robotic systems, which include a mobile platform with one or more manipulators, mounted at specific locations on the mobile base, are of great interest in a number of applications. In this paper, after thorough kinematic studies on the platform and manipulator motions, a systematic methodology will be presented to obtain the dynamic equations for such systems without violating the base n...

S. A. A. Moosavian and A. Mirani,

Mobile robotic systems, which include a mobile platform with one or more manipulators, mounted at specific locations on the mobile base, are of great interest in a number of applications. In this paper, after thorough kinematic studies on the platform and manipulator motions, a systematic methodology will be presented to obtain the dynamic equations for such systems without violating the base n...

This paper presents an attitude control algorithm for a Reusable Launch Vehicle (RLV) with a low lift/drag ratio (L/D < 0.5), in the presence of external disturbances, model uncertainties, control output constraints and the thruster model. The main novelty of proposed control strategy is a new combination of the attitude control methods included backstepping, dynamic inversion and adaptive cont...

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