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基于虚拟现实的折叠翼飞行器动态响应联合仿真

ynamic Response Simulation of Folding Wing Aircraft Based on Virtual Reality

中文摘要英文摘要

为了对折叠翼变体飞行器进行动态响应的分析,采用多体动力学方法建立了飞行器的纵向运动模型,并对非线性模型进行了小扰动线性化处理。利用CAD软件设计了折叠翼飞机的虚拟现实三维模型,与折叠翼系统模型同时导入到Simulink中,联合虚拟现实工具箱对折叠动态响应过程进行仿真,不但获得了相应的仿真结果和曲线,还能通过虚拟现实播放器实时的观察飞行器的飞行轨迹和姿态变化。

he longitudinal kinematic model is built and linearized to analyze the dynamic response of the folding wing aircraft. The 3D model of folding wing aircraft is designed with CAD software and then induced into Simulink virtual reality toolbox. The response results and curves are obtained by using integrated virtual reality simulation tool, meanwhile, the flight trajectory and posture change are displayed in the virtual reality viewer.

何真、殷明、刘玮、陆宇平

航空航天技术计算技术、计算机技术

变体飞行器折叠翼动态响应虚拟现实仿真

morphing aircraftfolding wingdynamic responsevirtual realitysimulation

何真,殷明,刘玮,陆宇平.基于虚拟现实的折叠翼飞行器动态响应联合仿真[EB/OL].(2014-05-22)[2025-07-21].http://www.paper.edu.cn/releasepaper/content/201405-363.点此复制

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