Power unit test system for small unmanned aerial vehicle

Deng Zhao; Luo Ji'An; Xu Yang; Lin Hui; Wu Liaoni

doi:10.1109/IAEAC.2015.7428587

Power unit test system for small unmanned aerial vehicle

Deng Zhao, Luo Ji'An, Xu Yang, Lin Hui, Wu Liaoni

Xiamen University

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

A test system is proposed, which can be applied to processes of designing, commissioning and other tests for the power unit of unmanned aerial vehicles (UAV). The working principle, software/hardware design and key technologies of this system are specifically introduced. Reliability of various functions of the system is examined and assessed through repeated engine tests, which indicates that, the system can control the engine stably and the data measured can reflect changes in parameters authentically. This system, meeting all requirements for performance testing, commissioning and maintenance of the engine, is suitable for the process of designing, commissioning and other tests for power units of small aircrafts.

Original language	English
Title of host publication	Proceedings of 2015 IEEE Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2015
Editors	Bing Xu
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	419-422
Number of pages	4
ISBN (Electronic)	9781479919796
DOIs	https://doi.org/10.1109/IAEAC.2015.7428587
State	Published - 7 Mar 2016
Externally published	Yes
Event	IEEE Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2015 - Chongqing, China Duration: 19 Dec 2015 → 20 Dec 2015

Publication series

Name	Proceedings of 2015 IEEE Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2015

Conference

Conference	IEEE Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2015
Country/Territory	China
City	Chongqing
Period	19/12/15 → 20/12/15

Keywords

engine test-bed
power unit
test system
UAV

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10.1109/IAEAC.2015.7428587

Cite this

Zhao, D., Ji'An, L., Yang, X., Hui, L., & Liaoni, W. (2016). Power unit test system for small unmanned aerial vehicle. In B. Xu (Ed.), Proceedings of 2015 IEEE Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2015 (pp. 419-422). Article 7428587 (Proceedings of 2015 IEEE Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2015). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/IAEAC.2015.7428587

Zhao, Deng ; Ji'An, Luo ; Yang, Xu et al. / Power unit test system for small unmanned aerial vehicle. Proceedings of 2015 IEEE Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2015. editor / Bing Xu. Institute of Electrical and Electronics Engineers Inc., 2016. pp. 419-422 (Proceedings of 2015 IEEE Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2015).

@inproceedings{12fa4e1d078a40d3bed7ee508fb036f6,

title = "Power unit test system for small unmanned aerial vehicle",

abstract = "A test system is proposed, which can be applied to processes of designing, commissioning and other tests for the power unit of unmanned aerial vehicles (UAV). The working principle, software/hardware design and key technologies of this system are specifically introduced. Reliability of various functions of the system is examined and assessed through repeated engine tests, which indicates that, the system can control the engine stably and the data measured can reflect changes in parameters authentically. This system, meeting all requirements for performance testing, commissioning and maintenance of the engine, is suitable for the process of designing, commissioning and other tests for power units of small aircrafts.",

keywords = "engine test-bed, power unit, test system, UAV",

author = "Deng Zhao and Luo Ji'An and Xu Yang and Lin Hui and Wu Liaoni",

note = "Publisher Copyright: {\textcopyright} 2015 IEEE.; IEEE Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2015 ; Conference date: 19-12-2015 Through 20-12-2015",

year = "2016",

month = mar,

day = "7",

doi = "10.1109/IAEAC.2015.7428587",

language = "英语",

series = "Proceedings of 2015 IEEE Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2015",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

pages = "419--422",

editor = "Bing Xu",

booktitle = "Proceedings of 2015 IEEE Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2015",

}

Zhao, D, Ji'An, L, Yang, X, Hui, L & Liaoni, W 2016, Power unit test system for small unmanned aerial vehicle. in B Xu (ed.), Proceedings of 2015 IEEE Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2015., 7428587, Proceedings of 2015 IEEE Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2015, Institute of Electrical and Electronics Engineers Inc., pp. 419-422, IEEE Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2015, Chongqing, China, 19/12/15. https://doi.org/10.1109/IAEAC.2015.7428587

Power unit test system for small unmanned aerial vehicle. / Zhao, Deng; Ji'An, Luo; Yang, Xu et al.
Proceedings of 2015 IEEE Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2015. ed. / Bing Xu. Institute of Electrical and Electronics Engineers Inc., 2016. p. 419-422 7428587 (Proceedings of 2015 IEEE Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2015).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Power unit test system for small unmanned aerial vehicle

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AU - Ji'An, Luo

AU - Yang, Xu

AU - Hui, Lin

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N2 - A test system is proposed, which can be applied to processes of designing, commissioning and other tests for the power unit of unmanned aerial vehicles (UAV). The working principle, software/hardware design and key technologies of this system are specifically introduced. Reliability of various functions of the system is examined and assessed through repeated engine tests, which indicates that, the system can control the engine stably and the data measured can reflect changes in parameters authentically. This system, meeting all requirements for performance testing, commissioning and maintenance of the engine, is suitable for the process of designing, commissioning and other tests for power units of small aircrafts.

AB - A test system is proposed, which can be applied to processes of designing, commissioning and other tests for the power unit of unmanned aerial vehicles (UAV). The working principle, software/hardware design and key technologies of this system are specifically introduced. Reliability of various functions of the system is examined and assessed through repeated engine tests, which indicates that, the system can control the engine stably and the data measured can reflect changes in parameters authentically. This system, meeting all requirements for performance testing, commissioning and maintenance of the engine, is suitable for the process of designing, commissioning and other tests for power units of small aircrafts.

KW - engine test-bed

KW - power unit

KW - test system

KW - UAV

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Zhao D, Ji'An L, Yang X, Hui L, Liaoni W. Power unit test system for small unmanned aerial vehicle. In Xu B, editor, Proceedings of 2015 IEEE Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2015. Institute of Electrical and Electronics Engineers Inc. 2016. p. 419-422. 7428587. (Proceedings of 2015 IEEE Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2015). doi: 10.1109/IAEAC.2015.7428587

Power unit test system for small unmanned aerial vehicle

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