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1. 中国空空导弹研究院
2. 仪器科学与动态测试教育部重点实验室中北大学
纸质出版:2008
移动端阅览
王武杰, 侯文, 郑宾. 火箭弹滚转角测量方法研究[J]. 中北大学学报(自然科学版), 2008,(2):170-175.
王武杰, 侯文, 郑宾. Study on the Measurement of Rocket Rotation Angle[J]. 2008, (2): 170-175.
为了对火箭弹实施某种控制以达到减小火箭弹射弹散布和增加射程的目的
需要实时测量火箭弹滚转角度.本文比较了二加速度计法、四加速度计法和感应线圈法等三种火箭弹滚转角测量方法
并详细地分析了该方法的测试原理误差.这些方法的共同特点是数据处理过程简单
适合实时测试的要求
测试系统结构简单
容易实现低的成本和高的工作可靠性.
To lower the shell distribution and to extend the range of rocket
a nozzle-like rocket-bounded actuator is deliberately designed to alter the outer trajectory.Real-time measurement of rocket rotation angle is needed to help the actuator act at the precise time.Three test methods
including two-accelerometers method
four-accelerometers method and geomagnetic induction coil method
for measuring rocket rotation angle are put forward in this paper.With its comparatively simple combination
the method tends to meet the requirement of real-time measurement
high reliability
low cost
and high feasibility.
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赵捍东,张亚,陈宏伟.用地磁感应转数传感器实现引信定距方法的研究[J].探测与控制学报,2002(1):57-60.Zhao Handong,Zhang Ya,Chen Hongwei.The research of using geomagnetic revolution sensor to realize Fuse-ranging[J].Journal of Detection&Control,2002(5):57-60.(in Chinese).
沈波,陈荷娟,王志兴.基于地磁传感器的计转数引信可行性研究[J].探测与控制学报,2001(4):45-48.Shen Bo,Chen Hejuan,Wang Zhixing.The study of the feasibiliby of fuze based on the geomagnetism turns-counting sensor[J].Journal of Detection&Control,2001(4):45-48.(in Chinese).
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