| 极坐标算法对飞机CCIP弹道解算的优化 |
| |
| 引用本文： | 陈松,祁岭,赵英杰.极坐标算法对飞机CCIP弹道解算的优化[J].海军航空工程学院学报,2007,22(1):133-136. |
| |
| 作者姓名： | 陈松 祁岭 赵英杰 |
| |
| 作者单位： | 1. 海军驻南昌地区航空军事代表室,江西南昌,330024
2. 91379部队,山东青岛,266001 |
| |
| 摘 要： | 采用极坐标算法对某型飞机CCIP攻击模式进行弹道解算优化,该算法进行坐标变换和积分变量转换后,使弹道的积分变为一个具有确定积分上限的定积分,有效地简化了计算过程,节省了计算时间,提高了计算精度,能较好满足火控系统的精度和实时性要求。
|
| 关 键 词： | 极坐标算法 火力控制 数学模型 |
| 修稿时间： | 2006年9月13日 |
Optimizing the CCIP trajectory calculation for one aeroplane by adopting the algorithm of polar coordinates |
| |
| CHEN Song,QI Ling and ZHAO Yingjie.Optimizing the CCIP trajectory calculation for one aeroplane by adopting the algorithm of polar coordinates[J].Journal of Naval Aeronautical Engineering Institute,2007,22(1):133-136. |
| |
| Authors: | CHEN Song QI Ling and ZHAO Yingjie |
| |
| Institution: | Aeronautical Military Representatives Office of Navy in Nanchang,Nanchang,Jiangxi,330024,Aeronautical Military Representatives Office of Navy in Nanchang,Nanchang,Jiangxi,330024 and The 91379th Unit of PLA,Qingdao,Shangdong,266001 |
| |
| Abstract: | The algorithm of polar coordinates is adopted to optimize the CCIP attack pattern trajectory calculation for one aeroplane. The algorithm of polar coordinates is alternated with a kind of coordinates and the conversion of integral variable. The integral becomes a problem of initial value that has definite integral upper limit. So the calculating process is predigested, the calculating time is saved, and the calculating accuracy is improved. And the fire control system accuracy and the requirement of real time are satisfied. |
| |
| Keywords: | the algorithm of polar coordinates fire control mathematic model |
| 本文献已被 CNKI 万方数据 等数据库收录！ |
| 点击此处可从《海军航空工程学院学报》浏览原始摘要信息 |
| 点击此处可从《海军航空工程学院学报》下载免费的PDF全文 |
|
