摘要
微机电器件(MEMS)技术的发展为飞行器导航控制系统的设计提供了新的实现方法。基于新型微机电测量元件和大规模可编程逻辑阵列技术,设计了一种飞行器导航控制系统。详细介绍了系统硬件和接口设计,并实现了一种微机电陀螺仪的误差补偿算法,有效的修正了陀螺仪的零漂特性,提高了系统测量精度。
Development of micro electromeehanical system (MEMS) device provides new method for design of aerocraft navigation and control system. Based on micro-eleetromeehanical measuring technology and Field Programmable Gate Array(FPGA) ,a new navigation and control system was proposed. Details of the system's hardware and interface were presented. Also, a kind of compensation arithmetic was implemented. Through testing, the MEMS gyroseope's static excursion was greatly decreased.
出处
《电子测量技术》
2009年第9期42-45,共4页
Electronic Measurement Technology