FIELD: transport.
SUBSTANCE: proposed system comprises pressure pickup; first, second and third pickups of undecarriage, unit to process signals from all aforesaid pickups. Proposed method comprises measuring hydraulic system working fluid pressure in undercarriage main leg, determining output electric signal, generating message about undercarriage extension, determining position of landing gear in flight, recording first and second operating conditions, measuring working fluid pressure in said first and second operating conditions, and generating output signal on measurement results. Aircraft landing gear comprises load control system. Aircraft incorporates load control system.
EFFECT: higher accuracy of load control.
20 cl, 11 dwg
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