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

School of Astronautics

Northwestern Polytechnical University Xian

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

2 Scopus citations

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).

Original language	English
Title of host publication	2006 IEEE International Conference on Mechatronics and Automation, ICMA 2006
Pages	1147-1151
Number of pages	5
DOIs	https://doi.org/10.1109/ICMA.2006.257787
State	Published - 2006
Event	2006 IEEE International Conference on Mechatronics and Automation, ICMA 2006 - Luoyang, China Duration: 25 Jun 2006 → 28 Jun 2006

Publication series

Name	2006 IEEE International Conference on Mechatronics and Automation, ICMA 2006
Volume	2006

Conference

Conference	2006 IEEE International Conference on Mechatronics and Automation, ICMA 2006
Country/Territory	China
City	Luoyang
Period	25/06/06 → 28/06/06

Keywords

Air data system
Aircraft instrument system
Precision pressure transducer

Access to Document

10.1109/ICMA.2006.257787

Cite this

@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. in 2006 IEEE International Conference on Mechatronics and Automation, ICMA 2006., 4026247, 2006 IEEE International Conference on Mechatronics and Automation, ICMA 2006, vol. 2006, pp. 1147-1151, 2006 IEEE International Conference on Mechatronics and Automation, ICMA 2006, Luoyang, China, 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. p. 1147-1151 4026247 (2006 IEEE International Conference on Mechatronics and Automation, ICMA 2006; Vol. 2006).

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

TY - GEN

T1 - Design of air data system of an aircraft integrated electronic standby instrument

AU - Kai, Chen

AU - Jie, Yan

AU - Panfeng, Huang

PY - 2006

Y1 - 2006

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).

KW - Air data system

KW - Aircraft instrument system

KW - Precision pressure transducer

UR - http://www.scopus.com/inward/record.url?scp=34247243188&partnerID=8YFLogxK

U2 - 10.1109/ICMA.2006.257787

DO - 10.1109/ICMA.2006.257787

M3 - 会议稿件

AN - SCOPUS:34247243188

SN - 1424404665

SN - 9781424404667

T3 - 2006 IEEE International Conference on Mechatronics and Automation, ICMA 2006

SP - 1147

EP - 1151

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

Abstract

Publication series

Conference

Keywords

Access to Document

Other files and links

Fingerprint

Cite this