Fuzzy Logic Controller Optimization Design for Tiltrotor Aircraft Landing Conversion

被引：0

作者：

Chen Heng ^{[1
]}

Wang Xu ^{[1
]}

Lei Tengfei ^{[1
]}

机构：

[1] Xijing Univ, Grad Dept, Xian 710123, Peoples R China

来源：

2013 32ND CHINESE CONTROL CONFERENCE (CCC) | 2013年

关键词：

Tiltrotor Aircraft; Fuzzy Logic; Genetic Algorithm; Flight Control System;

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

The tiltrotor aircraft can flight in the helicopter mode or in airplane mode during the procedure of its landing conversion. Its control system is very complicated and it is very difficult to obtain the model. After studying the mathematic model of the tiltrotor aircraft, we introduce the fuzzy logic control and design the flight controller based on fuzzy logic. The fuzzy logic controller is optimized in Genetic Algorithm. The simulation shows that the whole control system of the tiltrotor aircraft poses the good performances. The controller meets the requirement about its landing character. it is very useful to design the flight control system in the Fuzzy logic control via GA.

引用

页码：3482 / 3486

页数：5

共 7 条

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