The multi-point pressure and temperature measurement system for aerodynamic tunnel

Author

Zbiec, Michal ; Obrebski, Dariusz

Author_Institution

ICs & Syst. Design Dept., Inst. of Electron Technol., Warsaw, Poland

fYear

2014

fDate

19-21 June 2014

Firstpage

482

Lastpage

485

Abstract

This paper presents design and testing process of the pressure and temperature measurement system for aerodynamic tunnel, named SIESTA (System of Intelligent Sensors for Experimental Avionic Applications), announced in [1]. This system consists of three main parts: the hardware, the embedded software for microcontroller and the measurement program built in LabVIEW environment.

Keywords

aerodynamics; aerospace computing; aircraft instrumentation; avionics; mechanical engineering computing; pressure measurement; temperature measurement; tunnels; vehicle dynamics; virtual instrumentation; LabVIEW environment; SIESTA; aerodynamic tunnel; embedded software; hardware; measurement program; microcontroller; multipoint pressure measurement system; pressure testing process; system of intelligent sensors for experimental avionic applications; temperature measurement system; Calibration; Hardware; Pressure measurement; Temperature measurement; Temperature sensors; Thermistors; LabVIEW; MEMS pressure sensors;

fLanguage

English

Publisher

ieee

Conference_Titel

Mixed Design of Integrated Circuits & Systems (MIXDES), 2014 Proceedings of the 21st International Conference

Conference_Location

Lublin

Print_ISBN

978-83-63578-03-9

Type

conf

DOI

10.1109/MIXDES.2014.6872246

Filename

6872246