PILOT IN-FLIGHT BIOMECHANICAL CONTROL SYSTEM Russian patent published in 2014 - IPC B64D10/00 A61B5/103 A61B5/11 

FIELD: aircraft engineering.

SUBSTANCE: proposed system comprises sensitive transducers arranged at pilot outfit and connected with built-in computer. Flying gear incorporates inertial transducers (accelerometers and gyros) and mechanical goniometric sensors for definition of the pilot upper and lower extremities. Gloves house inertial sensors for definition of motion and orientation (angular position) of hands, strain gage transducers for determination of hands flexion, palm compression, hands turn, and piezoelectric crystal transducers at finger tips for determination of pressure on the surface. Socks house strain gages and piezoelectric crystal transducers for determination of foot motion and depression at pedals. Belt accommodates accelerometers and gyros for determination of pilot body motion jointly with aircraft at manoeuvring. Pilot outfit accommodates the built-in computer for compensation for errors in integration of accelerometers and errors in measurements of rough mechanical sensors.

EFFECT: higher precision of evaluation of pilot working condition.

1 dwg