Title :
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
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;
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
DOI :
10.1109/MIXDES.2014.6872246
