The multi-point pressure and temperature measurement system based on MEMS sensors

• Autorzy: Zbieć M , Obrębski D.
• Języki publikacji: EN

Abstrakty

EN

This paper deals with 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]. The system comprises three main components: the hardware part, the embedded software for microcontroller and the measurement program (for LabVIEW environment).

Słowa kluczowe

EN

bare die MEMS pressure sensor; embedded system; LabVIEW

PL

czujnik ciśnienia MEMS; system wbudowany; LabVIEW

• Wydawca: Lodz University of Technology. Department of Microelectronics and Computer Science
• Czasopismo: International Journal of Microelectronics and Computer Science
• Rocznik: 2014
• Tom: Vol. 5, nr 4
• Strony: 160--165
• Opis fizyczny: Bibliogr. 5 poz.

Twórcy

autor

Zbieć M

• ICs and Systems Design Department, Institute of Electron Technology, Warsaw, Poland

autor

Obrębski D.

• ICs and Systems Design Department, Institute of Electron Technology, Warsaw, Poland

Bibliografia

• [1] G. Janczyk, T. Bieniek, P. Grabiec, A. Wymysłowski, R. Swierczyński, “Optimization of MEMS-IC SiP Development Reliable Design Methods” Third IEEE International Workshop on Testing Three-Dimensional Stacked Integrated Circuits 3D-TEST in conjunction with ITC / Test Week 2012 November 8-9, 2012 - Anaheim, California, USA
• [2] The EPCOS C41 Pressure Sensor Datasheet, http://www.epcos.com/inf/57/ds/c41_gauge.pdf
• [3] The EPCOS C27 Pressure Sensor Datasheet, http://www.epcos.com/inf/57/ds/c27_gauge.pdf
• [4] The Texas Instruments 8-Channel, 24-Bits Analog-to-Digital Converter ADS1216 Datasheet, http://www.ti.com/lit/ds/symlink/ads1216.pdf
• [5] The National Instruments VISA Help, http://digital.ni.com/manuals.nsf/websearch/F18AFBCF54BF133A862574CE004B9B97