[an error occurred while processing this directive] [an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]
相关技术

导弹二维加速度过载环境的离心转盘模拟方法

  • 张艳兵 ,
  • 马铁华 ,
  • 孙江涛
展开
  • 1 中北大学计算机与控制工程学院,太原 030051
    2 中北大学电子测试技术国家重点实验室,太原 030051
    3 中国空空导弹研究院,河南洛阳 471009

张艳兵(1973-),男,汉,山西临猗人,副教授,博士研究生,研究方向:动态测试与智能控制。

收稿日期: 2015-08-25

  网络出版日期: 2025-05-30

基金资助

重点实验室基金

Simulation Method of Two-dimensional Acceleration Overload Environment for Missiles Based on Turntable and Centrifuge

  • ZHANG Yanbing ,
  • MA Tiehua ,
  • SUN Jiangtao
Expand
  • 1 School of Computer Science and Control Engineering, North University of China, Taiyuan 030051, China
    2 National Key Laboratory for Electronic Measurement Technology, North University of China, Taiyuan 030051, China
    3 China Airborne Missile Academy, Henan Luoyang 471009, China

Received date: 2015-08-25

  Online published: 2025-05-30

摘要

为了在实验室条件下检测导弹关键部件的抗过载能力,提出了一种离心转盘模拟试验方法。根据合成加速度的二维矢量分配原理,利用离心机带动转臂提供持续的动态加速环境;采用位置速度时间运动控制模式,利用转盘对其合成加速度实时跟踪和矢量分配,进行二维动态加速度的同步加载,实现导弹加速度过载环境的模拟。仿真和试验结果表明了该方法的可行性和有效性。

本文引用格式

张艳兵 , 马铁华 , 孙江涛 . 导弹二维加速度过载环境的离心转盘模拟方法[J]. 弹箭与制导学报, 2016 , 36(4) : 109 -112 . DOI: 10.15892/j.cnki.djzdxb.2016.04.028

Abstract

To test anti-overload ability of missile key components under laboratory conditions, a test method based on a turntable and a centrifuge was proposed. According to the vector distribution principle of synthetic acceleration, the continuous dynamic acceleration environment was reproduced by the centrifuge. The real-time tracking and vector distribution of synthetic acceleration were achieved by the turntable based on the motion control mode of position-velocity-time. A two-dimensional dynamic acceleration was loaded synchronously, therefore, the acceleration overload environment for missiles was simulated. The results of simulation and experiment demonstrate feasibility and effectiveness of the proposed method in this paper.

[an error occurred while processing this directive]

参考文献

[1]
WU DS, GUH B. Adaptive sliding control of six-DOFflight simulator motion platform[J]. Chinese Journal ofAeronautics, 2007, 20 (5): 425- 433.
[2]
吴建国, 李海波, 张琪,等. 综合离心环境试验技术研究进展. 强度与环境, 2014, 41 (1): 1- 9.
[3]
马杰, 姚郁. 一种新型动态飞行过载模拟器及其运动学分析 系统仿真学报, 2009, 21 (z2): 112- 414.
[4]
刘力, 刘兴堂. 空中飞行模拟技术及其应用[J]. 计算机仿真, 2005, 22 (10): 51- 54.
[5]
徐周, 李建峰. 基于PCI04 的天线转台伺服系统设计[. 电子机械工程, 2014, 30 (1): 61- 64.
[6]
LEKKAS A M, FOSSEN TI. Integral LOS path followingfor curved paths based on amonotone cubi-chermite splineparametrization[J]. IEEE Transactions on Control Sys-tems Technology, 2014, 22 (6): 2287- 2301.
文章导航

/

[an error occurred while processing this directive]