FIELD: aviation materiel, in particular, measuring instruments for determination of aircraft attutude relative to the local vertical and velocity vector.
SUBSTANCE: the device has an adder, integrator, differentiator, three amplifiers and an attitude transducer with the aid of which the dynamically similar signals of the pitch sensor or the angle-of-attack sensor are conditioned.
EFFECT: enhanced reliability of information on aircraft attitude at minimum weight and overall dimensions of the instrument complex.
1 dwg
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