| 火箭炮射表编拟及发射诸元快速装定研究 |
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| 引用本文： | 徐劲祥,祁载康,林德福,宋锦武.火箭炮射表编拟及发射诸元快速装定研究[J].南京理工大学学报(自然科学版),2004,28(3):333-336. |
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| 作者姓名： | 徐劲祥 祁载康 林德福 宋锦武 |
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| 作者单位： | 北京理工大学,机电工程学院,北京,100081 |
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| 摘 要： | 研究火箭炮射表编拟方法，分析了射表试验数据处理中的阻力系数辨识、出炮口初速确定、主动段终点诸元数据处理、动态推力数据提取等，建立火箭炮射表刚体六自由度弹道模型，利用编写的火箭弹六自由度弹道仿真程序，对某远程火箭弹进行仿真计算；针对传统方法进行火箭弹发射诸元装定中容易出现的问题，提出在火控计算机实现火箭弹发射诸元快速装定的方法，并给出程序流程图。
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| 关 键 词： | 火箭炮 射表 编拟 符合计算 发射诸元 装定 阻力系数辨识 |
| 文章编号： | 1005-9830(2004)03-0333-04 |
| 修稿时间： | 2002年5月12日 |
Study on the Compilation of Firing Tables and Rapid Firing Elements Binding of Rocket Gun System |
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| XU Jin xiang,QI Zai kang,LIN De fu,SONG Jin wu.Study on the Compilation of Firing Tables and Rapid Firing Elements Binding of Rocket Gun System[J].Journal of Nanjing University of Science and Technology(Nature Science),2004,28(3):333-336. |
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| Authors: | XU Jin xiang QI Zai kang LIN De fu SONG Jin wu |
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| Abstract: | This paper researches the compilation of firing tables of rocket gun system and analyzes data processing of firing tables test,such as drag coefficient identification,rocket muzzle velocity calculation,data processing of terminal elements of ascent trajectory and dynamic thrust data acquisition.A 6-DOF rigid body trajectory model of firing tables is established for rocket gun system by using a developed 6-DOF trajectory simulation program.The simulation of a long distance rocket was implemented.Aiming at the problems in firing elements caused by traditional methods,this paper brings out a method of rapid firing elements binding on fire control computers,and the rapid binding flowchart also has been put forward. |
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| Keywords: | rocket gun system firing tables complilation fit calculation firing elements bind drag coefficient identification |
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