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弹丸高速碰撞过程中靶面三维面形数据获取方法
引用本文:薛俊鹏,张启灿,王旭,隆昌宇,何徽,刘元坤,龙仁荣.弹丸高速碰撞过程中靶面三维面形数据获取方法[J].航天器环境工程,2020,37(3):258-263.
作者姓名:薛俊鹏  张启灿  王旭  隆昌宇  何徽  刘元坤  龙仁荣
作者单位:1.四川大学 空天科学与工程学院;2.四川大学 电子信息学院:成都 610065;3.中国工程物理研究院 流体物理研究所,绵阳 621900;4.北京卫星环境工程研究所,北京 100094;5.北京理工大学 爆炸科学与技术国家重点实验室,北京 100081
基金项目:人工智能四川省重点实验室开放基金;国家自然科学基金;国家科技重大专项;创新基金
摘    要:文章利用二级轻气炮作为高速碰撞弹丸的加载设备,结合基于傅里叶变换轮廓术的结构光三维测量方案实现高速碰撞过程三维面形数据的获取。系统由柯拉照明条纹投影部分和记录形变相位调制信息的百万帧频光电相机组成,根据所标定的相位高度映射参数和高速采集图像的相位分析数据计算出不同时刻穿甲靶面的三维坐标值。实验结果表明,该方法可实现2.976 km/s高速碰撞实验靶面几何变形的三维数据测量,能够为航天器防护结构设计及爆轰穿甲特性分析提供真实三维几何尺寸数据。

关 键 词:三维面形测量    二级轻气炮    超高速撞击    傅里叶变换    相机标定
收稿时间:2019-11-04
修稿时间:2020-05-20

Method for acquiring 3D shape data of target face in simulated hypervelocity impact
XUE Junpeng,ZHANG Qican,WANG Xu,LONG Changyu,HE Hui,LIU Yuankun,LONG Renrong.Method for acquiring 3D shape data of target face in simulated hypervelocity impact[J].Spacecraft Environment Engineering,2020,37(3):258-263.
Authors:XUE Junpeng  ZHANG Qican  WANG Xu  LONG Changyu  HE Hui  LIU Yuankun  LONG Renrong
Institution:1. School of Aeronautics and Astronautics, Sichuan University;2. College of Electronics and Information Engineering, Sichuan University: Chengdu 610065, China;3. Institute of Fluid Physics, China Academy of Engineering Physics, Mianyang 621900, China;4. Beijing Institute of Spacecraft Environment Engineering, Beijing 100094, China;5. State Key Laboratory of Explosion Science and Technology, Beijing Institute of Technology, Beijing 100081, China
Abstract:In this paper, the 3D shape data of high-speed impact process are acquired with the proposed 3D measurement system, which takes the two-stage light gas gun as the loading equipment for high-speed impact projectile, and adopts the structural light projection approach of Fourier transform profilometry. The system consists of a fringe projection part of the designed Kola illumination system, and a high-speed photoelectric camera with a million-level frame rate for recording the modulated phase information reflecting the shape deformation. The 3D coordinates of the armor pierced target surface are calculated from the calibrated phase height mapping parameters and the analyzed phase data of the high-speed captured images for different times. The experimental results show that with this method, the 3D geometric deformation in the hypervelocity impact experiment with a bullet speed up to 2.976 km/s can be measured, to provide real 3D geometric data for the design of spacecraft protective structures and the analysis of detonation & armor piercing characteristics.
Keywords:3D shape measurement  two-stage light gas gun  hypervelocity impact  Fourier transformation  camera calibration
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