| 一种次优空射巡航导弹中制导律的推导与仿真 |
| |
| 引用本文： | 冯星,李锋,邹杰.一种次优空射巡航导弹中制导律的推导与仿真[J].电光与控制,2003,10(3):28-30,34. |
| |
| 作者姓名： | 冯星 李锋 邹杰 |
| |
| 作者单位： | 1. 南京航空航天大学自动化学院,江苏,南京,210016
2. 洛阳电光设备研究所,河南,洛阳,471009 |
| |
| 基金项目： | 火力控制技术国防科技重点实验室资助项目 |
| |
| 摘 要： | 介绍了空射巡航导弹的攻击过程，建立了空射巡航导弹中制导律的数学模型，提出了最优性能指标，利用最优控制的基本理论，提出了一种新的次优中制导律，数字仿真结果表明该制导律对导弹的性能有很大的提高。
|
| 关 键 词： | 巡航导弹 最优控制 中制导律 |
| 文章编号： | 1671-637X(2003)03-0028-03 |
Derivation and simulation of a suboptimal midcourse guidance law for air-launched cruise missile |
| |
| FENG Xing ,LI Feng ,ZOU Jie.Derivation and simulation of a suboptimal midcourse guidance law for air-launched cruise missile[J].Electronics Optics & Control,2003,10(3):28-30,34. |
| |
| Authors: | FENG Xing LI Feng ZOU Jie |
| |
| Institution: | FENG Xing 1,LI Feng 2,ZOU Jie 2 |
| |
| Abstract: | The attacking procedure of air launched cruise missile is introduced at first, then a mathematical model of midcourse guidance law is established and the optimal performance index is given. A new suboptimal midcourse guidance law is put forward based on primary theory of optimal control, and the result of simulation shows that the performance of missile is improved greatly. |
| |
| Keywords: | cruise missile optimal control midcourse guidance law |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
