Two DOF Parallel Robot Design and Dynamics Simulation for Quick Picking

2012 ◽  
Vol 236-237 ◽  
pp. 448-453
Author(s):  
De Xue Bi ◽  
Chao Zhuo Guo ◽  
Xu Man Zhang
Keyword(s):  
Three Dimensional ◽  
Parallel Robot ◽  
Experimental Results ◽  
Dynamics Simulation ◽  
Solid Model ◽  
Robot Design ◽  
Dynamics Model ◽  
Simulation And Control ◽  
Design Mechanism ◽  
And Control

This paper presents a new design approach of parallel robot for quick grasp based on parallelogram mechanism，and derives the dynamics model. Using SimMechanics toolbox and simlink toolbox in Matlab Software, and guiding the three dimensional solid model into it, the dynamics simulation and control on two DOF parallel robot is designed and studied. The experimental results show that the design mechanism obtains the anticipated requirement.

Fast Tracking Spherical Parallel Robot Design and Hybrid Simulation Base on Solidwork and Simmechanics

2014 ◽  
Vol 556-562 ◽  
pp. 2549-2552 ◽  
Author(s):  
Ying Jun Hu ◽  
Guang Yan
Keyword(s):  
Three Dimensional ◽  
Parallel Robot ◽  
Dynamics Simulation ◽  
Robot Design ◽  
Simulation Approach ◽  
Fast Tracking ◽  
Simulation And Control ◽  
Design Mechanism ◽  
And Control ◽  
Tracking Objects

This paper presents a new design and dynamics simulation approach of spherical parallel robot for fast tracking objects based on parallelogram mechanism. Using SimMechanics toolbox and simlink toolbox in Matlab Software, and guiding the three dimensional Solidwork model into it, the dynamics simulation and control on three DOF fast tracking spherical parallel robot is designed and studied. The experimental results show that the design mechanism obtains the anticipated requirement.

Dynamics Simulation and Control Design of Gun Adjustment for Nonlinear Multibody System of Multiple Launch Rocket System

2019 ◽  
Author(s):  
Yunfei Miao ◽  
Guoping Wang ◽  
Xiaoting Rui ◽  
Tianxiong Tu ◽  
Lilin Gu
Keyword(s):  
Monte Carlo ◽  
Multibody System ◽  
Control Method ◽  
Control Design ◽  
Dynamics Simulation ◽  
System Dynamics Model ◽  
Dynamics Model ◽  
Simulation And Control ◽  
And Control ◽  
Rocket System

Abstract The dynamics simulation of the processing of the gun adjustment for multiple launch rocket system (MLRS) as a complex nonlinear multibody system is studied. Based on the new version of transfer matrix method for multibody system (MSTMM), the nonlinear multibody system dynamics model of MLRS is established, and the overall transfer equation of the nonlinear multibody system is deduced. The launch dynamics simulation of MLRS is carried out by combining the general kinematics equations of rocket and Monte Carlo method, and the simulated results are verified by experiments. On this basis, the control design and dynamics simulation of the gun adjustment of MLRS has been preliminary studied by combing MSTMM with PD control method. The results show that the proposed control method has a good stability and can realize the automatic control of gun adjustment of MLRS quickly and accurately.

scholarly journals Simulation and control of three-dimensional wakes

2004 ◽  
Vol 33 (5-6) ◽  
pp. 697-713 ◽  
Author(s):  
Georges-Henri Cottet ◽  
Philippe Poncet
Keyword(s):  
Three Dimensional ◽  
Simulation And Control ◽  
And Control

The Research on the Embedded Vehicle Dynamics Simulation Method

2013 ◽  
Vol 380-384 ◽  
pp. 1746-1749
Author(s):  
Jun Zhan ◽  
Jiang Li Lu ◽  
Liang Xu ◽  
Wei Zhang
Keyword(s):  
Real Time ◽  
Vehicle Dynamics ◽  
Subjective Evaluation ◽  
Simulation Method ◽  
Dynamics Simulation ◽  
Dynamics Model ◽  
The Real ◽  
Online Simulation ◽  
Preliminary Study ◽  
And Control

At present, the performance of the vehicle dynamics model is mainly evaluated objectively through offline simulation. In this paper, a vehicle dynamics model was implemented in dSPACE, which was applied to the Automotive Performance Simulator and the preliminary study was made for the realization of the subjective evaluation of the performance of vehicle dynamics model through the real-time closed-loop online simulation. The dSPACE interface library was used to write a Clib program to operate and control the Carsim RT model running on the dSPACE platform, which realized the communication between the external hardware and the real-time hardware of dSPACE.

scholarly journals Dynamics, simulation and control of a wheeled robotic glider

2012 ◽  
pp. 679-687 ◽  
Author(s):  
L. V. Glazkova ◽  
◽  
A. V. Panchenko ◽  
V. E. Pavlovsky ◽  
Keyword(s):  
Dynamics Simulation ◽  
Simulation And Control ◽  
And Control

Simulation and Control of Porosity in a Three-Dimensional Thin-Film Solar Cell

2013 ◽  
Vol 52 (33) ◽  
pp. 11246-11252 ◽  
Author(s):  
Jianqiao Huang ◽  
Gerassimos Orkoulas ◽  
Panagiotis D. Christofides
Keyword(s):  
Thin Film ◽  
Solar Cell ◽  
Thin Film Solar Cell ◽  
Three Dimensional ◽  
Simulation And Control ◽  
And Control

Analysis of a Missile's Initial Disturbance

2014 ◽  
Vol 889-890 ◽  
pp. 152-155 ◽  
Author(s):  
Xin Lin Wei ◽  
Yi Jiang
Keyword(s):  
Working Conditions ◽  
Complex Structure ◽  
Three Dimensional ◽  
Coupling Model ◽  
Dynamics Simulation ◽  
Dynamics Model ◽  
Three Dimensional Model ◽  
Flexible Coupling ◽  
Coupling System ◽  
Systems Simulation

In this paper, a certain type of vehicle missile launching system is the research object, which uses CAE technology to make a flexible coupling system dynamics simulation and analysis to provide a reference for similar tests. Since the complex structure of the vehicle missile system, reasonable assumptions and simplifications are made in establishing the dynamics model. Pro/E is used to build the three-dimensional model, and then it is imported to the ABAQUS to establish its dynamics model. Finally, in a complete virtual prototyping system model, we make a simulation of working conditions, and draw conclusions and analysis. The results show that the use of independent dynamics rigid-flexible coupling model dynamics simulation based on ABAQUS can be more realistic simulation of the process of vehicle missile launch, and it verifies the results of different working conditions, which provides a reference for the vehicle missile launching systems simulation .

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