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相关技术

任意载弹模式俯仰系统重力矩算法研究

  • 方航 ,
  • 黄朝学 ,
  • 王敏毅
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  • 中国船舶重工集团公司第710研究所,湖北宜昌 443003

方航(1991-),男,湖北黄冈人,硕士研究生,主要研究:动力学与控制、嵌入式系统软硬件设计。

收稿日期: 2015-11-16

  网络出版日期: 2025-05-30

Study on Gravity Moment Algorithm of Pitch System in Any Loading Mode

  • FANG Hang ,
  • HUANG Chaoxue ,
  • WANG Minyi
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  • No. 710 Research Institute, CSIC, Hubei Yichang 443003, China

Received date: 2015-11-16

  Online published: 2025-05-30

摘要

为实时解算某型火箭发射装置俯仰系统重力矩,基于质点系等效质心原理推导出任意载弹模式下重力矩算法模型,采用Matlab编程实现算法并同Pro/E测量计算实际值对比分析。仿真结果表明,该算法满足任意载弹模式下重力矩实时解算要求并达到较高精度,有效解决当前采用Pro/E软件测量并计算重力矩方法工作量大且通用性差等缺点,极大的提高研究效率。

本文引用格式

方航 , 黄朝学 , 王敏毅 . 任意载弹模式俯仰系统重力矩算法研究[J]. 弹箭与制导学报, 2016 , 36(4) : 161 -164 . DOI: 10.15892/j.cnki.djzdxb.2016.04.042

Abstract

In order to calculate load of gravity moment of a certain type of rocket launcher in real time, based on the principle of equivalent mass center of mass of a particle system, the model function of gravity moment in any load mode was deduced and programmed with Matlab, and compared with actual results measured and calculated by Pro/E software. Simulation results show that this kind of algorithm can satisfy real-time solution of gravity moment in any load mode, settles effectively current use of Pro/E software to measure and calculate gravity moment method which has series of shortcomings like a large amount of work and poor generality, which can greatly improve research efficiency.

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参考文献

[1]
原星武 某自行导弹防空系统炮塔重力矩平衡技术[C] // 第九届全国雷达学术年会论文集, 2003: 976-978.
[2]
张鹏, 范树迁, 石明全. 某扭杆式双向平衡机设计及试验分析[J]. 机械设计与制造, 2011(2):11-13.
[3]
黄朝学. 某扭杆式双向平衡机的设计及疲劳寿命分析[J].机械设计,2010,27(9):7275.
[4]
哈尔滨工业大学理论力学教研室. 理论力学[M].7版.北京:高等教育出版社,2009: 28-58.
[5]
同济大学数学系. 高等数学[M].6版.北京:高等教育出版社,2007: 272-282.
[6]
郑文纬, 吴克坚. 机械原理[M].7版.北京:高等教育出版社,1997: 69-76.
[7]
程永强, 韩勇. 某型导弹发射装置平衡机的改装设计[J].军事装备测控技术, 2014, 22(5):1469-4471.
[8]
方航, 王敏毅, 黄朝学. 某火箭弹发射装置自适应平衡机原理方案研究[J].舰船电子工程,2015,35(9):51-55.
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