Dynamic modelling of a projectile launcher with controlled double inverted pendulum

Paras Savnani, M. Chauhan, A. Mecwan, Rajesh Patel
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Abstract

The aim of this paper is to form a mathematical model to simulate the dynamics of a unique mechanism which can be used in a projectile launching machine. This mechanism is a bi-linkage mechanism with two sets of pivots having rigid and flexible links respectively and the torque to drive the mechanism is applied at the first pivot via a pneumatic cylinder. The mathematical model of this system is derived assuming the system to be a controlled double inverted pendulum and the trajectory of the ball, resulting from the combined motion of the links, is assumed to follow circular path for a small segment. The launch parameters i.e. launch velocity and launch angle are derived from the numerical analysis of the mathematical model using simulation software and these parameters are experimentally verified to a great degree of accuracy.
可控双倒立摆发射装置动力学建模
本文的目的是建立一个数学模型来模拟一种独特的可用于弹丸发射机的机构的动力学。该机构为双连杆机构,有两组分别具有刚性连杆和柔性连杆的枢轴,驱动机构的扭矩通过气缸施加在第一个枢轴上。建立了该系统的数学模型,假设该系统是一个受控的双倒立摆系统,并假设球的运动轨迹在一个小段内沿圆形轨迹运动。利用仿真软件对数学模型进行数值分析,得到了发射速度和发射角度等发射参数,并对这些参数进行了实验验证,具有较高的精度。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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