[1]徐星辰,付尧明,安斯奇.无人机电动燃油泵流量控制系统设计[J].控制与信息技术(原大功率变流技术),2019,(01):23-26.[doi:10.13889/j.issn.2096-5427.2019.01.005]
 XU Xingchen,FU Yaoming,AN Siqi.Flow Control of the Electric Fuel Pump for Unmanned Aerial Vehicle[J].High Power Converter Technology,2019,(01):23-26.[doi:10.13889/j.issn.2096-5427.2019.01.005]
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无人机电动燃油泵流量控制系统设计()
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《控制与信息技术》(原《大功率变流技术》)[ISSN:2095-3631/CN:43-1486/U]

卷:
期数:
2019年01期
页码:
23-26
栏目:
控制理论与应用
出版日期:
2019-02-05

文章信息/Info

Title:
Flow Control of the Electric Fuel Pump for Unmanned Aerial Vehicle
文章编号:
2096-5427(2019)01-0023-04
作者:
徐星辰付尧明安斯奇
(中国民用航空飞行学院 航空工程学院,四川 广汉 618300)
Author(s):
XU XingchenFU YaomingAN Siqi
( Aviation Engineering Institute,Civil Aviation Flight University of China,Guanghan, Sichuan 618300, China )
关键词:
电动燃油泵流量测量控制系统PID控制无人机
Keywords:
electric fuel pump flow measurement control system PID control UAV(unmanned aerial vehicle)
分类号:
V233.7
DOI:
10.13889/j.issn.2096-5427.2019.01.005
文献标志码:
A
摘要:
电动燃油泵具备可靠性高、功率密度大和响应快等传统燃油泵不具备的优势,其流量的精确、迅速供给将有效提升无人机的飞行性能;但是其存在大范围流量测量精度低且控制性能不达标的缺点。对此,文章提出使用多传感器对流量测量方式进行改良,并融合数据测试、反馈数据处理和PID控制技术共同完成对电动燃油泵的流量控制软硬件环境的实物验证。结果表明电动燃油泵在该控制方法作用下能得到满足要求的稳态和动态输出流量。
Abstract:
Compared with the traditional fuel pump, electric fuel pump has the advantages of high reliability, high power density and fast response. Its accurate and rapid flow supply will effectively improve the flight performance of UAV, but its large-scale flow measurement accuracy is low and its control performance is not up to the standard. In this regard, this paper proposed a method to improve the flow measurement by using multiple sensors, and to integrate data testing, feedback data processing and PID control technology to complete the physical verification of the flow control software and hardware environment of the electric fuel pump. The results show that the steady and dynamic output flow of the electric fuel pump can meet the requirements under the control method.

参考文献/References:

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备注/Memo

备注/Memo:
收稿日期:2018-08-14
作者简介:徐星辰(1995—),男,硕士研究生,研究方向为自动控制。
更新日期/Last Update: 2019-02-28