[an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]Study on Gravity Moment Algorithm of Pitch System in Any Loading Mode
Received date: 2015-11-16
Online published: 2025-05-30
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
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.
| [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. |
/
| 〈 |
|
〉 |