FIELD: physics.
SUBSTANCE: device includes a micromechanical gimballess inertial navigation system, a satellite receiver, a magnetometer, a barometric altimeter, a display and the following computation-logic units: a unit for generating flight routes, a 2D map synthesis unit, a 3D map synthesis unit based on the object composition and a unit for generating a low-altitude flight path.
EFFECT: high flight safety of aircraft owing to backup of the main piloting-navigation loop, as well as information support during flight of aircraft in difficult weather conditions by forming 3D and 2D images of the cartographic environment with application of piloting-navigation information.
2 dwg
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