| 基于典型弹道的反导导弹制导方式分析 |
| |
| 引用本文： | 王亮,闫杰.基于典型弹道的反导导弹制导方式分析[J].火力与指挥控制,2012,37(8):94-97. |
| |
| 作者姓名： | 王亮 闫杰 |
| |
| 作者单位： | 西北工业大学航天学院,西安,710072 |
| |
| 摘 要： | 针对典型的导弹弹道仿真,通过对反导导弹的几种备选制导律进行了参数调试和数字仿真,设计了初、中制导方案,通过数字仿真给出了弹道规划,明确了允许的发射条件。同时,分析了各方案主要的制导信息误差及其影响,针对高斯噪声误差模型提出了制导信息误差指标。最终确定了较优制导方案。该方案经数字仿真验证具有较优的攻击区性能,攻击区较大、发射条件约束较为宽松,以当前的技术水平有望实现。
|
| 关 键 词： | 反导导弹 仿真 制导律 |
Analysis of Guidance Mode of Anti-ballistic Missile Type Based on Typical Trajectory |
| |
| WANG Liang
,
YAN Jie.Analysis of Guidance Mode of Anti-ballistic Missile Type Based on Typical Trajectory[J].Fire Control & Command Control,2012,37(8):94-97. |
| |
| Authors: | WANG Liang YAN Jie |
| |
| Institution: | (College of Astronautics,Northwestern Polytechnical University,Xi’an 710072,China) |
| |
| Abstract: | For the typical missile trajectory,several guidance laws of anti ballistic missile is simulated and debuged,the project of original control and midst control are designed,and the trajectory programming by figure simulation is given.At the same time,the allowable condition of launch is definituded,and the control’s information error is analyzed.It is influence of every project,advances the control’s information error basic the gauss yawp error simulation.The excellent control project is confirmed and error analysis of assault section and control information is proposed.This project has bigger assault section and easier assault condition,and it’s easy to be realize nowadays |
| |
| Keywords: | anti ballistic missile simulation guidance law |
| 本文献已被 CNKI 万方数据 等数据库收录！ |
|
