| 基于MEMS器件的倾角指示系统研究 |
| |
| 引用本文： | 蒋海涛,冯文光,刘诗斌.基于MEMS器件的倾角指示系统研究[J].测控技术,2010,29(6):5-7. |
| |
| 作者姓名： | 蒋海涛 冯文光 刘诗斌 |
| |
| 作者单位： | 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;西北工业大学,电子信息学院,陕西,西安,710072 |
| |
| 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。
|
| 关 键 词： | MEMS 加速度传感器 倾角指示系统 |
Inclination Indication System Based on MEMS Units |
| |
| JIANG Hai-tao,FENG Wen-guang,LIU Shi-bin.Inclination Indication System Based on MEMS Units[J].Measurement & Control Technology,2010,29(6):5-7. |
| |
| Authors: | JIANG Hai-tao FENG Wen-guang LIU Shi-bin |
| |
| Abstract: | 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. |
| |
| Keywords: | MEMS |
| 本文献已被 CNKI 万方数据 等数据库收录！ |
| 点击此处可从《测控技术》浏览原始摘要信息 |
|
点击此处可从《测控技术》下载全文 |
|
