AIRCRAFT TURN ANGLE CONTROL SYSTEM

摘要

FIELD: aircraft engineering.SUBSTANCE: proposed system generates control instruction signal for controlled nose wheel corresponding to turn angle. Said control instruction causes aircraft fuselage taxiing in preset direction. Proposed system comprises controller of the turn nominal angle, slip detector and switch. Said controller computes turn nominal angle under the assumption of slip absence. Slip detector proceeds from turn nominal angle to reveal said slip. Said switch selects control instruction signal and outputs it. In the case of slip signal corresponding to nominal turn angle is sent to output as a control signal for nose wheel without using control signal corresponding to turn angle.EFFECT: minimised slip in taxiing on iced taxiway, higher stability and safety.2 cl, 6 dwg