[1]杨成顺,杨忠,马俊,等.基于MS5540C的无人机高度传感器设计[J].应用科技,2010,37(08):26-30.[doi:10.3969/j.issn.1009-671X.2010.08.007]
 YANG Cheng-shun,YANG Zhong,MA Jun,et al.Design of UAV altimeter based on MS5540C[J].Applied science and technology,2010,37(08):26-30.[doi:10.3969/j.issn.1009-671X.2010.08.007]
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基于MS5540C的无人机高度传感器设计(/HTML)
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《应用科技》[ISSN:1009-671X/CN:23-1191/U]

卷:
第37卷
期数:
2010年08期
页码:
26-30
栏目:
自动化技术
出版日期:
2010-08-05

文章信息/Info

Title:
Design of UAV altimeter based on MS5540C
文章编号:
1009-671X (2010) 08-0026-05
作者:
杨成顺1杨忠1马俊1郭晓鸿1张会影2
1.南京航空航天大学 自动化学院,江苏 南京 210016; 2.蚌埠学院 计算机科学与技术系,安徽, 蚌埠 233000
Author(s):
YANG Cheng-shun1YANG Zhong1MA Jun1GUO Xiao-hong1ZHANG Hui-ying2
1.College of Automation Control, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;2.Department of Computer Science and Technology,Bengbu College,Bengbu,233000
关键词:
MS5540C无人机温度补偿高度传感器
Keywords:
MS5540C UAV temperature compensation altitude sensor
分类号:
TP212.9
DOI:
10.3969/j.issn.1009-671X.2010.08.007
文献标志码:
A
摘要:
飞行高度是无人机飞行控制中重要的控制参数.针对传统高度测量系统的缺陷,设计并实现了具有温度补偿功能的高度传感器.该高度传感器具有体积小、质量轻、数据稳定、响应速度快等优点,特别适合微小型无人机的使用.经过某小型无人机飞行试验,该传感器完全可以达到精确测量飞行高度的要求.
Abstract:
Flight altitude is an important control parameter in the control of MicroUAV. An altitude sensor with temperature compensation function was designed and implemented to overcome the shortcomings of the traditional altitude measurement system. With advantages of small volume, light weight, data stability and rapid response, the sensor is particularly suitable for the use of MicroUAV. According to experimentation of a certain MicroUAV, it can fully meet the requirement of accurately measuring the altitude.

参考文献/References:

[1]吴森堂,费玉华.飞行控制系统[M]. 北京:北京航空航天大学出版社,2005.
[2]Intersema. MS5540C (RoHS*) Miniature Barometer Module[EB/OL].[2009-08-23].http://www.intersema.ch/products/documentation/datasheets/.
[3]STM32F103 datasheet [EB/OL].[2009-09-26]. http://wwww.st.com/stonline/Products/literature/ds/13587.pdf.
[4]王志刚,唐飞. 基于MS5534B的气压高度计系统的设计[J]. 微纳米电子技术,2008,45(6): 351-355.
[5]NOTH A,ENGEL W, SIEGWART R. Design of an ultralight weight autonomous solar airplane for continuous flight[J]. Proceedings of Field and Service Robotics, 2006, 25(7): 441-452.
[6]Intersema. Using MS5534 for altimeters and barometers [EB/OL]. [2009-09-30]. http://www.intersema.capplications/altimeters/.

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备注/Memo

备注/Memo:
基金项目:国家自然科学基金资助项目(60674100).
作者简介:杨成顺(1984-),男,博士研究生,主要研究方向:智能飞行控制,E-mail:yangchengshun@126.com.
更新日期/Last Update: 2010-09-02