摘要
介绍一种新型的可以应用于微型飞行器的极化电磁驱动舵机机构。该舵机机构使用混合励磁方式的电磁驱动器 ,具有体积小、结构简单可靠、响应快和效率高等特点。本文阐述了该系统的设计思想 ,建立了电磁驱动器的电磁模型 ,详细分析了电磁舵机的吸力和反力特性的关系 ,导出它的控制特性 ,试验分析表明
A novel magnetic actuator designed for a micro-aircraft is presented, it is an actuator helm of the hybrid magnetic. It possesses many characteristics of small size, light weight, rapid response, high reliability and so on. The design consideration is described. Mathematics model of magnetic act uator is established due to the relation of the attractive force and the inverse force. A control characteristic is introduced by analysis of the model. Experim ental results verify that the output performance of the magnetic actuator is lin ear and has a dynamic response.
出处
《南京航空航天大学学报》
EI
CAS
CSCD
北大核心
2004年第1期48-51,共4页
Journal of Nanjing University of Aeronautics & Astronautics
