FIELD: instrument engineering.
SUBSTANCE: invention relates to the field of navigational instrument making and can find application in the systems for displaying aircraft attitude. Method comprises receiving a roll angle, a pitch angle and a yaw angle of aircraft (20); generating display image (14) indicating the roll angle, the pitch angle and the yaw angle; and displaying display image (14) on display device (12). Display image (14) comprises spherical shell (30) with track angle scale (44), projected onto spherical shell (30) along latitude line (42) of spherical shell (30), and with pitch angle scale (46) projected onto spherical shell (30) along longitude line (36) of spherical shell. Furthermore, display image (14) comprises graphical aircraft attitude indicator (48) inside the spherical shell (30) rotated with respect to spherical shell (30), such that graphical aircraft attitude indicator (48) indicates the roll angle, the pitch angle and the yaw angle of aircraft (20) with respect to spherical shell (30).
EFFECT: technical result is expansion of functional capabilities.
12 cl, 7 dwg
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