METHOD FOR TRANSMITTING FLIGHT PARAMETERS FROM AN AIRCRAFT TO AN INTRUSTED AIRCRAFT

摘要

The invention relates to a method for transmitting flight parameters from a leading aircraft (L) to at least one intruder aircraft (I). According to the invention, the transmission is effected by means of a TC AS type collision avoidance system to which is connected a flight parameter emission authorization system having a database comprising coordinates defining a volume. , said confidence volume (C), lower than the TCAS monitoring volume. The authorizing aircraft's flight parameter emission authorizing authorization system authorizes, for an intruder aircraft identified as flying in the confidence volume, the transmission of at least one flight parameter of the leading aircraft so that the intruder aircraft can calculate the position of wake vortex centers (14L, 15L) generated by the leading aircraft (L) or the driving force of said wake vortices (14L, 15L). The exchange of flight parameters from the leading aircraft only to intruding aircraft flying within the restricted-size confidence volume makes it possible to not exceed the maximum capacity of the bandwidth of the automated communication.