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Possible optimization of integrated avionics systems with regard to errors of air data unit sensors

Szelmanowski A., Michalak S.

Prace Naukowe Instytutu Technicznego Wojsk Lotniczych

2009

nr 25

69-87

This paper presents errors of electronic static and dynamic pressure sensors (used in air data units in military aviation) and their impact on errors of calculated piloting-navigation parameters such as the flight air speed and altitude. Selected problems and possible optimization of these errors in avionics systems integrated on the basis of a digital data bus (e.g. ARINC-429 and MIL-1553B) are presented. The paper presents also accredited research base of the AFIT Pressure Measurement Laboratory and ways of possible correcions of errors of pressure sensors used at air data units.