Name
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. |
Year | DOI | Venue |
|---|---|---|
2014 | 10.1109/MIXDES.2014.6872246 | MIXDES |
Keywords | Field | DocType |
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,labview,mems pressure sensors,thermistors,calibration | Control engineering,Electronic engineering,Engineering,Temperature measurement,Aerodynamics | Conference |
Citations | PageRank | References |
0 | 0.34 | 0 |
Authors | ||
2 | ||
Name | Order | Citations | PageRank |
|---|---|---|---|
| Zbiec, M. | 1 | 1 | 2.76 |
| Dariusz Obrebski | 2 | 7 | 4.13 |