UAV Dynamics and Electric Power System Modeling and Visualization using Modelica and FMI

Meaghan Podlaski, L. Vanfretti, H. Nademi, Hao-Hsiang Chang
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引用次数: 1

Abstract

This paper presents an object-oriented, equation-based framework for multi-engineering modeling of a quadrotor UAV, which includes the rigid body dynamics, simplified aerodynamics, gyroscopic effects, electrical power system and battery losses, and DC motor dynamics. An open-source drone modeling library is introduced by explaining the mathematical models and multi-domain components used to model the drone. Animation and visualization techniques for the drone using CAD models are also introduced and explained. The proposed drone model is simulated under different flight scenarios using motor and power system models with different levels of detail, aiming to provide better means for design and understanding, of multi-engineering aspects of UAVs. This model provides a foundation for future UAV open-source model development, electrified power propulsion design, visualization and interaction, and system identification.
基于Modelica和FMI的无人机动力学与电力系统建模与可视化
本文提出了一个面向对象、基于方程的四旋翼无人机多工程建模框架,包括刚体动力学、简化空气动力学、陀螺仪效应、电力系统和电池损耗以及直流电机动力学。介绍了一个开源的无人机建模库,阐述了用于无人机建模的数学模型和多域组件。动画和可视化技术的无人机使用CAD模型也介绍和解释。采用不同细节层次的电机和动力系统模型对不同飞行场景下的无人机模型进行了仿真,旨在为无人机多工程方面的设计和理解提供更好的手段。该模型为未来无人机开源模型开发、电气化动力推进设计、可视化交互、系统识别等提供了基础。
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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