FIELD: aviation.
SUBSTANCE: method consists in receiving information on configuration, location, orientation of aircraft, information on position, geometrical and mass characteristics and parameters of movement of the vortex generator at the current moment in time, information on environmental parameters, determining geometric dimensions of the hazardous zone of the vortex trace, presenting visual information to the crew in a certain manner.
EFFECT: invention relates to a method of preventing penetration of an aircraft into a hazardous zone of a vortex trace of a vortex generator.
1 cl, 2 dwg
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|
RU2469411C1 |
| METHOD FOR PROVISION OF AIRCRAFT FLIGHT VORTEX SAFETY | 2012 |
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RU2496121C1 |
