| 对抗仿真系统中的防空导弹比例导引法仿真弹道设计 |
| |
| 引用本文： | 朱永文,娄寿春,周林,丁尔启.对抗仿真系统中的防空导弹比例导引法仿真弹道设计[J].系统仿真学报,2005,17(12):3095-3097. |
| |
| 作者姓名： | 朱永文 娄寿春 周林 丁尔启 |
| |
| 作者单位： | 空军工程大学导弹学院,陕西,三原,713800 |
| |
| 基金项目： | 国防预研基金资助专项项目（41306020202） |
| |
| 摘 要： | 针对某型防空导弹，利用一系列假设，设计满足对抗仿真系统需求的比例导引法仿真弹道；运用瞬时平衡法对导弹气动力参数进行处理，形成平衡升力系数和平衡侧力系数；在导弹控制系统理想工作情况下，运用弹体法向、侧向受力与控制系统产生的需求力相等的假设，建立弹道方程；通过仿真可以看出，利用的假设和建立的弹道方程是正确的，能够描述某型防空导弹的弹道特性。
|
| 关 键 词： | 防空导弹 仿真弹道 比例导引法 气动力参数 |
| 文章编号： | 1004-731X（2005）12-3095-03 |
| 收稿时间： | 2004-11-09 |
| 修稿时间： | 2005-08-20 |
Proportional Navigation Trajectory Simulation In Air Defence System |
| |
| ZHU Yong-wen,LOU Shou-chun,ZHOU Lin,DING Er-qi.Proportional Navigation Trajectory Simulation In Air Defence System[J].Journal of System Simulation,2005,17(12):3095-3097. |
| |
| Authors: | ZHU Yong-wen LOU Shou-chun ZHOU Lin DING Er-qi |
| |
| Institution: | Airforce Missile College of Technology University, Sanyuan 713800, China |
| |
| Abstract: | Some SAM was discussed. Using a series of hypothesis to design proportional navigation simulation trajectory that satisfied the counterwork simulation; Using the method of instantaneous balance to handle the some SAM aerodynamic parameter. In result, It formed the balance pitch coefficient and side coefficient after the aerodynamic parameter being handled. Under the perfect work condition of the missile control system, the body of normal force and side force equaled to the requirement force could be educed. Through this conclusion, the trajectory equation was constituted. From the simulation, It can educe that the equation of ballistic trajectory by the hypothesis is true. The equation of ballistic trajectory can describe some SAM trajectory characteristic. |
| |
| Keywords: | SAM Simulation of Trajectory Proportional Navigation Trajectory Aerodynamic Parameter |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
