| 基于MEMS加速度传感器的飞行器倾角测量系统设计 |
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| 引用本文： | 蒋海涛,郭战营.基于MEMS加速度传感器的飞行器倾角测量系统设计[J].计算机测量与控制,2010,18(1). |
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| 作者姓名： | 蒋海涛 郭战营 |
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| 作者单位： | 1. 西北工业大学,电子信息学院,陕西,西安,710072;焦作师范高等专科学校,河南,焦作,454001
2. 焦作师范高等专科学校,河南,焦作,454001 |
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| 摘 要： | 根据MEMS加速度传感器的工作原理和特点,研究了一种基于MEMS三轴加速度传感器和C8051F352单片机的飞行器倾角测量系统的实现方法;介绍了倾角的测量原理及整体框架,重点阐述了系统的硬件电路设计和软件设计;该系统体积小、功耗低且可靠性高,可用于各类飞行器的倾角指示和测量。
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| 关 键 词： | MEMS加速度传感器 飞行器 倾角指示系统 |
Design of Aircraft Tilt Measurement System Based on MESM Accelerometer Sensor |
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| Jiang Haitao,Guo Zhanying.Design of Aircraft Tilt Measurement System Based on MESM Accelerometer Sensor[J].Computer Measurement & Control,2010,18(1). |
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| Authors: | Jiang Haitao Guo Zhanying |
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| Affiliation: | 1.College of Electronics and Information/a>;Northwestern Polytechnical University/a>;Xi'an 710072/a>;China/a>;2.Jiaozuo Teachers college/a>;Jiaozuo 454001 |
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| Abstract: | According to the principle and characteristics of the MEMS accelerometer sensor,a realization methodment of aircraft tilt measure system based on MEMS accelerometer sensor and C8051F352 is studied.The principle and whole frame of the system are given,the design of the hardware circuit and software are mainly presented.Compared with tradition attitude indication system,this system has low power consumption and small size.The results of tests indicate that the system has high reliability and this method can b... |
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| Keywords: | MEMS accelerometer aircraft tilt angle indication system |
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