Design of air data system of an aircraft integrated electronic standby instrument

Chen Kai; Yan Jie; Huang Panfeng

doi:10.1109/ICMA.2006.257787

Design of air data system of an aircraft integrated electronic standby instrument

Chen Kai, Yan Jie, Huang Panfeng

航天学院

Northwestern Polytechnical University Xian

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

2 引用（Scopus）

摘要

The authors discussed the design of Air Data System (ADS) in this paper, which is an important part of Integrated Electronic Standby Instrument (IESI) of aircrafts. The architecture, modelling and development of the ADS are introduced firstly. The selection of an accurate and reliable pressure transducer is one of the challenges in designing the overall air data instrument. Two Precision Pressure Transducers (PPT) are selected as sensors and a tiny single board computer (686CORE) is selected as the CPU of the ADS. The flight altitude, airspeed and Mach number can be displayed in the Active Matrix Liquid Crystal Display (AMLCD).

源语言	英语
主期刊名	2006 IEEE International Conference on Mechatronics and Automation, ICMA 2006
页	1147-1151
页数	5
DOI	https://doi.org/10.1109/ICMA.2006.257787
出版状态	已出版 - 2006
活动	2006 IEEE International Conference on Mechatronics and Automation, ICMA 2006 - Luoyang, 中国期限: 25 6月 2006 → 28 6月 2006

出版系列

姓名	2006 IEEE International Conference on Mechatronics and Automation, ICMA 2006
卷	2006

会议

会议	2006 IEEE International Conference on Mechatronics and Automation, ICMA 2006
国家/地区	中国
市	Luoyang
时期	25/06/06 → 28/06/06

访问文件

10.1109/ICMA.2006.257787

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链接到 Scopus 的出版物

引用此

@inproceedings{c5fd0ed883b1422393eb5f91af6c4e17,

title = "Design of air data system of an aircraft integrated electronic standby instrument",

abstract = "The authors discussed the design of Air Data System (ADS) in this paper, which is an important part of Integrated Electronic Standby Instrument (IESI) of aircrafts. The architecture, modelling and development of the ADS are introduced firstly. The selection of an accurate and reliable pressure transducer is one of the challenges in designing the overall air data instrument. Two Precision Pressure Transducers (PPT) are selected as sensors and a tiny single board computer (686CORE) is selected as the CPU of the ADS. The flight altitude, airspeed and Mach number can be displayed in the Active Matrix Liquid Crystal Display (AMLCD).",

keywords = "Air data system, Aircraft instrument system, Precision pressure transducer",

author = "Chen Kai and Yan Jie and Huang Panfeng",

year = "2006",

doi = "10.1109/ICMA.2006.257787",

language = "英语",

isbn = "1424404665",

series = "2006 IEEE International Conference on Mechatronics and Automation, ICMA 2006",

pages = "1147--1151",

booktitle = "2006 IEEE International Conference on Mechatronics and Automation, ICMA 2006",

note = "2006 IEEE International Conference on Mechatronics and Automation, ICMA 2006 ; Conference date: 25-06-2006 Through 28-06-2006",

}

Kai, C, Jie, Y & Panfeng, H 2006, Design of air data system of an aircraft integrated electronic standby instrument. 在 2006 IEEE International Conference on Mechatronics and Automation, ICMA 2006., 4026247, 2006 IEEE International Conference on Mechatronics and Automation, ICMA 2006, 卷 2006, 页码 1147-1151, 2006 IEEE International Conference on Mechatronics and Automation, ICMA 2006, Luoyang, 中国, 25/06/06. https://doi.org/10.1109/ICMA.2006.257787

Design of air data system of an aircraft integrated electronic standby instrument. / Kai, Chen; Jie, Yan ; Panfeng, Huang.
2006 IEEE International Conference on Mechatronics and Automation, ICMA 2006. 2006. 页码 1147-1151 4026247 (2006 IEEE International Conference on Mechatronics and Automation, ICMA 2006; 卷 2006).

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

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AU - Jie, Yan

AU - Panfeng, Huang

PY - 2006

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N2 - The authors discussed the design of Air Data System (ADS) in this paper, which is an important part of Integrated Electronic Standby Instrument (IESI) of aircrafts. The architecture, modelling and development of the ADS are introduced firstly. The selection of an accurate and reliable pressure transducer is one of the challenges in designing the overall air data instrument. Two Precision Pressure Transducers (PPT) are selected as sensors and a tiny single board computer (686CORE) is selected as the CPU of the ADS. The flight altitude, airspeed and Mach number can be displayed in the Active Matrix Liquid Crystal Display (AMLCD).

AB - The authors discussed the design of Air Data System (ADS) in this paper, which is an important part of Integrated Electronic Standby Instrument (IESI) of aircrafts. The architecture, modelling and development of the ADS are introduced firstly. The selection of an accurate and reliable pressure transducer is one of the challenges in designing the overall air data instrument. Two Precision Pressure Transducers (PPT) are selected as sensors and a tiny single board computer (686CORE) is selected as the CPU of the ADS. The flight altitude, airspeed and Mach number can be displayed in the Active Matrix Liquid Crystal Display (AMLCD).

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KW - Aircraft instrument system

KW - Precision pressure transducer

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DO - 10.1109/ICMA.2006.257787

M3 - 会议稿件

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BT - 2006 IEEE International Conference on Mechatronics and Automation, ICMA 2006

T2 - 2006 IEEE International Conference on Mechatronics and Automation, ICMA 2006

Y2 - 25 June 2006 through 28 June 2006

ER -

Design of air data system of an aircraft integrated electronic standby instrument

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