计算机工程2012,Vol.38Issue(4):212-214,217,4.
MUH姿态增稳控制系统设计与实现
Design and Realization of Attitude Stability Augmentation Control System for Mini Unmanned Helicopter
摘要
Abstract
This paper designs and realizes an attitude stability augmentation control system for Mini Unmanned Helicopter(MUH), which is low-cost, independent, safe and reliable. It is applied to maintain the stability of MUH. The precision attitude values which are obtained by the estimate algorithm of gravitational complementary filter based on filtering switching are used as the feedback of this system. Multi-loop fuzzy PI cascade control is introduced because it does not require high accurate model. Experimental results show that the system has satisfactory performance on stability augmentation effect, and it is cheap for application.关键词
姿态解算/角速率反馈/模糊PI控制/姿态增稳/微小型无入直升机/地面站Key words
attitude calculation/ angular rate feedback/ fuzzy PI control/ attitude stability augmentation/ Mini Unmanned Helicopter(MUH)/ ground station分类
自科综合引用本文复制引用
罗平波,韩波,禹科,李平..MUH姿态增稳控制系统设计与实现[J].计算机工程,2012,38(4):212-214,217,4.基金项目
国家“863”计划基金资助项目“基于自主无人飞行器的田问作物遥感信息采集系统的研制与应用”(2006AA1OZ204) (2006AA1OZ204)