FIELD: aircraft engineering.
SUBSTANCE: proposed system comprises set of transducers (2) collect data on flight parametre, central electronic unit (3) to process aforesaid data and make them representative. System comprises also electronic graphics data (4) controlled by above mentioned central electronic unit to display aforesaid data on display or transparent plate (5) with the help of protector. During take-off and landing, symbols displaying spatial position of aircraft are displayed on aforesaid display. The symbols above comprises aircraft wings undercarriage positions in terms of pitch angle, the positions being superimposed on pitch vertical scale made up of indicators pairs projected on aforesaid plate-screen.
EFFECT: improved control over aircraft parametres in take-off and landing.
4 cl, 2 dwg
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