摘要
以某型飞行器的惯性制导系统为应用背景,介绍了一种基于ARM的陀螺仪特性仿真系统的设计与实现。根据嵌入式系统的体积小、性能强、功耗低等突出特点,采用结构化的程序设计、模块同步通讯、电磁兼容、抗干扰与容错等技术,构建了以ARM为核心的陀螺仪仿真系统,解决了陀螺仪控制回路复杂、信号敏感度高等难题。
Design and realization of the simulation system of the character of gyroscope based on ARM are presented,according to the practical application of inertial navigation system of missile.According to the embedded system＇s outstanding characteristics of small size,high performance,low cost,the system was used solving the problem such as complex control circuit,high signal accuracy,which adopts the key technology of the structured design,the modular synchronous communication,the compatible of electricity and magnetic,the reliability design and fault-tolerant technique.
出处
《战术导弹技术》
2012年第2期95-97,101,共4页
Tactical Missile Technology
关键词
ARM
陀螺仪特性
测试
仿真
ARM
the character of gyroscope
test
simulation
