METHOD OF AUTOMATIC CONTROL OF HIGHLY-MANEUVERABLE AIRCRAFT

摘要

FIELD: aircraft engineering. ^ SUBSTANCE: invention relates to methods of controlling highly-maneuverable aircraft. Aerodynamic control surface drive control signal component that of integrated transducer unit corresponding to current normal overload are dynamically limited. Drive control signal component is passed through nonlinear element with restriction and zone of insensitivity. Signal generated at nonlinear element output is sent to integrating device of prefilter. Aircraft control stick "free travel" compensation signal is generated. Signal of difference between current magnitude of control stick position pickup signal and control stick "free travel" compensation signal is computed to be sent to prefilter. ^ EFFECT: higher stability, controllability and safety. ^ 1 dwg