Method and system for preventing alerting of an aircraft's onboard collision avoidance system during altitude change maneuvers
An altitude change and anti-collision technology, applied in aircraft traffic control, traffic control system, radio wave measurement system, etc., can solve problems such as increasing time spent, reducing vertical speed, and prolonging execution time
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[0041] exist figure 1 In , a device 1 according to the invention onboard an aircraft AC is shown in block diagram. Such a device 1 is used to prevent some TA and / or RA alarms from the on-board collision avoidance system TCAS2 of the aircraft AC while the aircraft AC is performing an altitude change maneuver for intercepting the set level Zc.
[0042]The aircraft AC is also provided with an autopilot system 3 that controls more specifically its vertical velocity Vz. The automatic navigation system 3 may include at least some of the devices 5 to 8 of the apparatus 1 described later.
[0043] In this figure, the anti-collision system 2 and the autopilot system 3 are shown outside the aircraft AC, while they are actually installed on the aircraft.
[0044] As known, the anti-collision system 2 is capable of detecting an intruding aircraft AI in the air environment of the aircraft AC, to calculate a theoretical collision time between the aircraft AC and said intruding aircraft AI...
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