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The Measurement for Moving Pos of High-speed Missile

  • HUANG Shasha ,
  • LIU Qi ,
  • QIAO Jia
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  • Testing Institute, Chinese Flight Test Establishment, Xi'an 710089, China

Received date: 2018-06-01

  Online published: 2025-05-30

Abstract

In the flight test, the rapid movement and rolling motion of the missile may threaten the aircraft flight safety. A method for the measurement of the missile's movement attitude is given Photographs the missile witn the calibrated measurement system. Then test the marked points with intersection measurement. Through the calculation, the outbound attitude parameters of the missile are obtained. This method has the characteristics of high accuracy and simple calculation process, and is of great significance to the missile-drop mission in flight tests.

Cite this article

HUANG Shasha , LIU Qi , QIAO Jia . The Measurement for Moving Pos of High-speed Missile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2018 , 38(4) : 73 -76 . DOI: 10.15892/j.cnki.djzdxb.2018.04.018

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References

[1]
吴立峰. 无驱动结构的硅微机械陀螺若干关键技术研究[D]. 北京: 北京邮电大学, 2010,
[2]
PADGAONKAR A J, KRIEGER K W, KING A I. Measurement of angular acceleration of a rigid using linear accelerometers[J]. Journal of Applied Meehanies, 1975, 42(3): 552-556.
[3]
MERHAV S J. A nongyroscopic inertial measurement uint[J]. Journal of Guidance and eontrol, 1982, 5(3): 227-235.
[4]
王继方. 高速投掷物体跟踪与姿态测量方法的研究[D]. 天津: 天津大学, 2007,
[5]
张文娇. 弹道跟踪镜技术研究[D]. 西安: 西安工业大学, 2010,
[6]
柯鹏, 杨春信. 货台空投系统的三维动画仿真[J]. 系统仿真学报, 2006, 18(5): 1253-4256.
[7]
杨廷梧. 一种新的光电跟踪测量交会模型[J]. 测控技术, 2012, 31(8): 20-22.
[8]
项树林, 徐宁. 基于多台光学经纬仪实时交会的弹道初段解算方案探讨[J]. 弹箭与制导学报, 2009, 29(1): 205-208.
Outlines

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