Simulation of RC Helicopter based on dynamics of quaternion by using OpenGL and simulink

W. Ham, Jaebyung Park, E. Tumenjargal, L. Badarch, Hyeokjae Kwon
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Abstract

In this paper, we present a sliding mode control for the radio controlled helicopter based on quaternion dynamics. We also introduce the kinematics of the rotating object based on quaternion and then propose a robust sliding mode control algorithm which can guarantee the over all stability of the whole system. We will show the simulation results by using the matlab simulink software tool and then implement the computer animation by using OpenGL based on the data of the simulation results. In this paper, we introduce implementation of virtual training environments based on Embedded System. Our virtual environment consists of S3C6410 ARM11 based embedded board, 3D Auto-Stereoscopic LCD Module, and RC Helicopter's remote controller. We use the simple dynamics of the helicopter which we derived in previous research work under the assumption that it can be modeled as rigid body composed of three main parts, such as main body, main rotor, and tail rotor. From the computer simulation, we can check the validness of proposed control law.
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基于四元数动力学的遥控直升机仿真
本文提出了一种基于四元数动力学的直升机滑模控制方法。在此基础上引入了基于四元数的旋转对象运动学,并提出了一种鲁棒滑模控制算法,保证了整个系统的整体稳定性。我们将使用matlab simulink软件工具显示仿真结果,然后根据仿真结果的数据使用OpenGL实现计算机动画。本文介绍了基于嵌入式系统的虚拟训练环境的实现。我们的虚拟环境由基于S3C6410 ARM11的嵌入式板、3D自动立体显示模块和遥控直升机遥控器组成。在假定直升机可以被建模为由主体、主旋翼和尾桨三个主要部分组成的刚体的前提下,我们使用了之前研究工作中推导出的直升机简单动力学模型。通过计算机仿真,验证了所提控制律的有效性。
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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