A method for processing flight performance limitations of a tcasii airborne collision avoidance system flight platform

Abstract

The invention provides a flight performance limitation processing method and system of a flight platform of a TCASII airborne collision avoidance system. The flight performance limitation processing system comprises a parameter acquisition module, a parameter processing module, a parameter table look-up module, a parameter self-inspection module and a parameter view setting module; and according to real-time flight performance of the platform and in combination with a core algorithm of the TCASII airborne collision avoidance system, real-time processing and updating are performed on flight performance parameters so as to obtain real-time flight performance limit information and to give more accurate alarm in real time. Therefore, the TCASII airborne collision avoidance system has better user experience, the platform can obtain more refined safety prompts, and the TCASII airborne collision avoidance system is more competitive in the market.

Description

technical field [0001] The invention relates to a method and system for processing flight performance limitation of a flight platform of a TCASII airborne collision avoidance system, and relates to the field of air traffic control collision avoidance. Background technique [0002] TCASII is an airborne collision avoidance system, which is mainly used to provide air safety separation guarantee for aircraft to achieve the purpose of collision avoidance. By inquiring, receiving, and processing the response signals of other aircraft's transponders, it monitors other aircraft around, and calculates the flight trend of other aircraft within the monitoring range relative to its own aircraft, and gives traffic warning and decisive warning suggestions. [0003] The TCASII airborne collision avoidance system itself has many functions, and the system composition is extremely complex. The minimum performance standard of the TCASII airborne collision avoidance system stipulates the influ...

AI Technical Summary

Problems solved by technology

[0004] The current TCASII airborne collision avoidance system is designed according to the minimum performance standard (RTCA / DO-185A / RTCA / DO-185B) of the TCASII airborne collision avoidance system, in which the discrete line design is generally adopted for the limitation of aircraft performance, so It will cause an aircraft of a certain type. Once the discrete line is determined, the aircraft of this type will always be unable to give some warnings of the airborne collision avoidance system, which will affect the real-time interaction between the performance of the aircraft and the warnings of the airborne collision avoidance system. Coordination, because the real situation of the aircraft platform does not respond to the TCASII airborne collision avoidance system in real time, so that the TCASII airborne collision avoidance system cannot realize the real-time input based on the real performance of the aircraft to maximize the safety of the TCASII airborne collision avoidance system

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