| 某型直升机飞行控制系统仿真研究 |
| |
| 引用本文： | 戴宁,司云玲,雷亚平.某型直升机飞行控制系统仿真研究[J].飞行力学,2006,24(1):77-80,84. |
| |
| 作者姓名： | 戴宁 司云玲 雷亚平 |
| |
| 作者单位： | 西北工业大学,自动化学院,陕西,西安,710072 |
| |
| 摘 要： | 介绍了基于M ATLAB开发的某型直升机飞行控制系统仿真软件包及快速原型的开发,说明了系统各单元的模型及系统仿真的实现。并对飞控系统的所有功能进行了仿真验证,仿真结果表明,控制系统的设计合理可行。在某型直升机飞行控制系统的设计过程中,本软件取得了较好的效果,对控制律的设计及验证发挥了较好的作用。
|
| 关 键 词： | 直升机 飞行控制 快速原型 |
| 文章编号： | 1002-0853（2006）01-0077-04 |
| 收稿时间： | 2004-11-08 |
| 修稿时间： | 2004-11-082005-12-02 |
Helicopter Flight Control System Simulation Research |
| |
| DAI Ning,SI Yun-ling,LEI Ya-ping.Helicopter Flight Control System Simulation Research[J].Flight Dynamics,2006,24(1):77-80,84. |
| |
| Authors: | DAI Ning SI Yun-ling LEI Ya-ping |
| |
| Abstract: | In this paper,a helicopter flight control system simulation software package and rapid prototype was introduced,which was developed on MATLAB.Several unit math models and system simulation were described.All functions of the flight control system had been tested.The feasibility of the control system was validated by simulation.The software had made a good effect on designing the helicopter flight control system.It is helpful for designing and validating the control law of the helicopter. |
| |
| Keywords: | helicopter flight control rapid prototype |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
|
