AIRCRAFT CONTROL AND INDICATION SYSTEM Russian patent published in 2011 - IPC G09G1/00 G05B15/00 

FIELD: instrument making.

SUBSTANCE: aircraft control and indication system including computing-conversion device, electron-beam device and collimator optical head, which are interconnected by means of inputs-outputs through the information exchange channel and forming collimator aircraft indicator, differs by the fact that by means of interaction of computing-conversion device via information exchange channel with indication and control devices, navigation-flight information sensors, surveillance sensors of after-cabin space at external indication and control devices, at failures of electron-beam device and collimator optical head, at test checks of equipment, at side, rear and all-round surveillance available of after-cabin space as per the data of surveillance sensors of after-cabin space at indication on indication and control devices there formed is virtual collimator aircraft indicator.

EFFECT: enlarging functional capabilities of indication and control system of aircraft owing to possible display of virtual collimator aircraft indicator.

1 dwg