摘要
研究了一种基于MEMS加速度传感器的倾角指示系统,包括倾角指示系统的工作原理、硬件设计以及软件算法流程。与传统倾角仪相比较,该系统体积小、功耗低。试验结果表明该系统具有较高的可靠性,可用于指示需要进行姿态控制的各类飞行器的姿态。
A realization method of aircraft attitude indication system based on MEMS accelerometer sensor is studied.The work principle,hardware design and software flow chart of this inclination indication system are introduced in detail separately.Compared with traditional attitude indication system,this system has lower power consumption and smaller size.The results of tests indicate that the system has higher reliability and this method can be used to determine the attitude of aircraft which needs to be controlled.
出处
《测控技术》
CSCD
北大核心
2010年第6期5-7,11,共4页
Measurement & Control Technology
