SIMULATION METHOD ON FLIGHT TEST BENCH OF AIRCRAFT PENETRATION INTO VORTEX TRACE Russian patent published in 2019 - IPC G09B9/08 G06F17/00 

FIELD: aviation.

SUBSTANCE: invention relates to a simulation method at a flight test bench of aircraft penetration into a vortex trail. For this purpose, the pilot's working conditions are simulated in the cockpit of the aircraft cabin, the dynamics of the aircraft and the operation of its systems in real time are modeled, simulating the evolution of the vortex trace behind the vortex generator aircraft, determining additional forces and moments occurring when the aircraft hits the vortex trail, performing disturbance hazard assessment, displaying on the display hazardous zones simultaneously in horizontal and vertical planes, aircraft position, predicted flight path, determining and displaying on the display a range of flight control parameters leading to the ingress of the aircraft into the hazardous zone of the vortex trace, determining the increment of overloads along the flight trajectory, degree of discomfort to effects on crew and passengers is assessed.

EFFECT: broader capabilities in training piloting techniques in vortex hazard conditions.

1 cl, 3 dwg