A method for transmitting flight parameters from a leading aircraft (L) to at least one intruding aircraft (I), wherein, the transmission is effected by a collision avoidance system of TCAS type. The transponder of the leading aircraft (L) is configured to measure the spectrum of an interrogation signal received from the intruding aircraft (I) and to compare the power of the spectrum to a threshold power. If the power of the interrogation signal is greater than or equal to the threshold power, then the intruding aircraft (I) is eligible to receive flight parameters from the leading aircraft to be able to compute the position of the centres or the force of circulation of wake vortexes (14L, 15L) generated by the leading aircraft (L). The exchange of flight parameters from the leading aircraft only to eligible intruding aircraft makes it possible to not exceed the maximum automated communication bandwidth capacity.
METHOD FOR TRANSMITTING FLIGHT PARAMETERS FROM A LEADING AIRCRAFT TO AN INTRUDING AIRCRAFT
2018-10-25
Patent
Electronic Resource
English
IPC: | G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS |
Method for transmitting flight parameters from a leading aircraft to an intruding aircraft
European Patent Office | 2019
|Method for transmitting flight parameters of a lead aircraft to an intruder aircraft
European Patent Office | 2019
|METHOD FOR TRANSMITTING FLIGHT PARAMETERS OF A LEAD AIRCRAFT TO AN INTRUDER AIRCRAFT
European Patent Office | 2018
|