FIELD: automatic flight control systems for stabilization of lateral movement of light aircraft. SUBSTANCE: system includes first and second roll-rate pick-ups, four adders, three amplifiers, aileron drive, aileron position sensor, first and second yaw-rate pick-ups, rudder position sensor, programmer, bank angle computer, accelerometer, flight velocity transducer, flight altitude transducer, setter, four scalers, two inverters and two non-linear units. EFFECT: reduced error in determination of bank angle. 6 dwg
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Authors
Dates
2001-12-10—Published
2000-07-26—Filed