FIELD: physics.
SUBSTANCE: invention relates to a method for integral display of flight situation parameters. To implement the method, data from an information and measurement system consisting of a set of systems for measuring motion and state of an aircraft, on-board aircraft, ground and satellite navigation systems, an on-board computer system and means of displaying information of aircraft, which enables displaying on the screen of a multifunctional digital indicator a set of flight situation parameters. Set of parameters of flight situation is displayed in a certain way, taking into account their mutual conditioning and interaction, which is manifested in various aspects - in location, connection, sizes of scales and indicators.
EFFECT: higher flight safety due to continuous formation and presentation of an integral volume of information on the flight situation and reduced load on the pilot.
1 cl, 16 dwg
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