HIGHLY-MANEUVERABLE AIRCRAFT CROSS-RANGE MANEUVERING AUTOMATIC CONTROL SYSTEM Russian patent published in 2010 - IPC B64C13/18 

FIELD: aircraft engineering.

SUBSTANCE: control stick displacement is used as a parametre related with pilot actions. Control signals are generated in bank and yaw channels to vary as control stick displacement. Damping isodromic signals of bank and yaw angular speeds are generated with their magnitudes, if minor, are taken to equal zero. Generated signals are summed up to be dynamically constricted by integrating links of appropriate bank and yaw channel pre-filters. Said signals are used as feedback signals sent to integrating link inputs when their absolute values exceed constriction values. Said signals are additionally summed with appropriate damping isodromic signals of bank and yaw angular speeds, earlier taken to equal zero. Shaped control signals are fed to inputs of appropriate drives to displace ailerons and rudder.

EFFECT: optimum aircraft control.

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