FIELD: transport.
SUBSTANCE: invention relates to aircraft instrumentation and can be used in aircraft spatial position determination systems in flights under IMC and at night at the absence of natural horizon. For this, pitch and bank are defined by two separate aircraft outlines. Claimed gyrohorizon is composed of two meters integrated in one case. First meter 1 is located at the case top part whereat aircraft outline 3 in side view forms pitch angle indicator in scale 2. Meter scale is divided into nosing-up scales of 0 to 180 degrees and nosing-down scales of 5-0 to minus 180 degrees. Pitch angle is counted at said scale against aircraft outline nose. Second meter is located under first one. It shows to pilot aircraft outline 6 bank in rear view. Bank is counted on scales 7 graduated from 0 to 90 degrees. Note here that index of the angle of attack 4 can be set against the background of pitch angle scale.
EFFECT: higher reliability.
2 dwg
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