FIELD: aircraft engineering.
SUBSTANCE: device has indicators for speeds of bank, pitch, hunt, attack angle, height, speed, M number and angles of deviation of aerodynamic surfaces of plane. In block for determining pitch moment calculation of current moment of pith acting on plane is calculated. Concurrently angular acceleration of pitch is calculated. Weight of plane load is determined on basis of known functional connection to inertial moment along transverse axis of linked coordinates system. Weight control is realized in comparison device.
EFFECT: higher precision, higher reliability.
6 cl, 6 dwg
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