| 非线性优化方法在超音速导弹设计中的应用 |
| |
| 引用本文： | 杨蔷薇,占正勇.非线性优化方法在超音速导弹设计中的应用[J].海军航空工程学院学报,2010,25(1):41-44. |
| |
| 作者姓名： | 杨蔷薇 占正勇 |
| |
| 作者单位： | 西安飞行自动控制研究所,西安,710065 |
| |
| 摘 要： | 以某型非线性超音速导弹为例,详细介绍了在MATLAB环境下利用NCD非线性控制设计模块进行计算机辅助控制系统参数优化设计的方法。仿真结果表明,这种优化方法既避免了复杂的计算和编程,又使系统满足各项性能指标要求,具有良好的动态性能和极强的鲁棒性,易于工程实现。
|
| 关 键 词： | 超音速导弹 NCD模块 参数优化 |
Application of Nonlinear Optimization Method on Supersonic Missile Design |
| |
| YANG Qiang-wei and ZHAN Zheng-yong.Application of Nonlinear Optimization Method on Supersonic Missile Design[J].Journal of Naval Aeronautical Engineering Institute,2010,25(1):41-44. |
| |
| Authors: | YANG Qiang-wei and ZHAN Zheng-yong |
| |
| Institution: | (Xi＇an Flight Automatic Control Research Institute, Xi＇an 710065, China) |
| |
| Abstract: | An advanced method of control system parameter optimization aided by computer for supersonic missile was put forward, which adopted MATLAB＇s nonlinear optimization control toolbox. The results of simulation show that this method not only has not complex calculating and programming but also easily enable the nonlinear system meeting the needs for performance index. The system has good dynamic performance and strong robustness and it is easy to engineering realize. |
| |
| Keywords: | supersonic missile NCD blockset parameter optimization |
| 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 |
