| 导弹中末段制导导引律转换研究 |
| |
| 引用本文： | 赵东,蔡海超,赵海涛.导弹中末段制导导引律转换研究[J].舰船电子工程,2010,30(5):47-50. |
| |
| 作者姓名： | 赵东 蔡海超 赵海涛 |
| |
| 作者单位： | 1. 海军装备部驻上海地区军事代表局,上海,201206
2. 92721部队,舟山,316000 |
| |
| 摘 要： | 文章研究了导弹由中间段制导律向末段制导律转换的问题,提出了一种可变导引系数的组合制导律,即可变系数组合比例导引律（ACNG）。仿真结果表明,该导引律总体优于纯比例导引和固定系数组合比例导引律,中末段弹道过渡平滑,衔接良好,有利于中末段的交班,同时降低了导弹的需用过载。
|
| 关 键 词： | 比例导引律 可变系数组合制导律 数字仿真 |
Research of Missile Navigation Guidance Law Transfering from Midcourse to Terminal |
| |
| Zhao Dong,Cai Haichao,Zhao Haitao.Research of Missile Navigation Guidance Law Transfering from Midcourse to Terminal[J].Ship Electronic Engineering,2010,30(5):47-50. |
| |
| Authors: | Zhao Dong Cai Haichao Zhao Haitao |
| |
| Institution: | Zhao Dong) Cai Haichao) Zhao Haitao)(Navy Military Delegate Bureau in Shanghai1),Shanghai 201206)(No.92721 Troops of PLA2),Zhoushan 316000) |
| |
| Abstract: | Based on the research on the problem about missile guidence law transfering from midcourse to terminal,a new simple combined alterable coefficient navigation guidance（ACNG） law is proposed.Simulation results show that the midcourse and terminalcourse trajectory can be linked up smoothly and the change of over-load is in the permitted range,which is better than proportional navigation guidance（PNG）. |
| |
| Keywords: | proportional navigation guidance alterable combined navigation guidance law digital simulation |
| 本文献已被 维普 万方数据 等数据库收录！ |
|
