| 一种导弹攻击时间协同导引律 |
| |
| 引用本文： | 张友安,张友根,彭军.一种导弹攻击时间协同导引律[J].海军航空工程学院学报,2009,24(1):34-38. |
| |
| 作者姓名： | 张友安 张友根 彭军 |
| |
| 作者单位： | 1. 海军航空工程学院,控制工程系,山东,烟台,264001
2. 海军航空工程学院,新装备培训中心,山东,烟台,264001 |
| |
| 摘 要： | 研究了具有攻击时间约束的多枚导弹协同导引律。首先，根据各枚导弹的估计到达时间来指定攻击时间，并由指定攻击时间设计期望的弹目距离，使攻击时间控制问题转化为弹目距离跟踪问题；然后，引入导弹导引非线性模型，采用反馈线性化的方法将其转化为线性模型；最后，利用线性极点配置的方法设计出稳定的控制律。仿真结果证明，所有导弹都能非常精确地按照指定攻击时间到达目标。
|
| 关 键 词： | 多导弹 攻击时间控制 导引 反馈线性化 齐射攻击 |
An Impact-Time-Control Cooperative Guidance Law for Multi-Missiles |
| |
| ZHANG You-an,ZHANG You-gen and PENG Jun.An Impact-Time-Control Cooperative Guidance Law for Multi-Missiles[J].Journal of Naval Aeronautical Engineering Institute,2009,24(1):34-38. |
| |
| Authors: | ZHANG You-an ZHANG You-gen and PENG Jun |
| |
| Institution: | Naval Aeronautical and Astronautical University a.Department of Control Engineering;b.New Equipment Training Center;Yantai Shandong 264001;China |
| |
| Abstract: | An impact-time-control cooperative guidance law for multi-missiles was investigated in this paper.Firstly,the time-to-go for each missile was estimated and based on which the desired impact time was determined,so the impact time control problem was transformed into a range tracking problem.Secondly,a nonlinear model for homing guidance law design was brought forward,which was transformed into a linear system by using feedback linearization.Lastly,a stable control law was designed by using pole placement app... |
| |
| Keywords: | multi-missiles impact-time-control guidance feedback linearization salvo attack |
| 本文献已被 CNKI 维普 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 |
