科技广场Issue(5)：100-102,3.
3-自由度直升机模型的分析与控制器设计
The Controller Design and Analysis of 3-DOC Helicopter Model
胡睿 1鲍俊卿 1饶祺1
作者信息
- 1. 中航工业洪都集团650所,江西南昌330024
- 折叠
摘要
Abstract
In this paper, 3-DOC helicopter system is applied as a simulator platform. According to its charac- teristic of linear model, a method of LQR is adopted to design the helicopter controller to improve the performance of the system. In order to improve the tracking and anti-jamming capabilities of the system, an internal mode/is used to this method.关键词
3-自由度直升飞机/线性化模型/LQRKey words
3-DOC Helicopter Model/Linear Model/LQR分类
航空航天引用本文复制引用
胡睿,鲍俊卿,饶祺..3-自由度直升机模型的分析与控制器设计[J].科技广场,2012,(5):100-102,3.
