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Airborne anti-collision system failure recording method

An airborne collision avoidance system and fault recording technology, applied in traffic control system, registration/indication, time register, etc., to achieve the effect of shortening maintenance time

Active Publication Date: 2017-01-25
四川九洲空管科技有限责任公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At the same time, the complete recording information of occasional failures or intermittent failures during the flight is helpful to help analyze the potential problems of the equipment, and the differences of the equipment under different environmental conditions can help the equipment to be improved and upgraded.

Method used

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  • Airborne anti-collision system failure recording method
  • Airborne anti-collision system failure recording method

Examples

Experimental program
Comparison scheme
Effect test

specific Embodiment 1

[0047] Such as figure 1 with figure 2 The specific method steps for the fault recording method of the airborne collision avoidance system are as follows:

[0048] 1. When the airborne collision avoidance system is started, read the number of starts of the airborne collision avoidance system in the fault maintenance configuration file of the airborne collision avoidance system and add 1, and save the number of starts after adding 1 in the global variable, At the same time, update the system's airborne collision avoidance system fault record configuration file with the updated number of starts;

[0049] 2. When the airborne collision avoidance system fails and changes, code the changed fault, and the fault coding information includes fault change time, fault type and fault state information;

[0050] 3. Find the fault record file corresponding to this startup according to the current startup times. If the corresponding fault record file exists, open it directly; if the corres...

specific Embodiment 2

[0054] On the basis of the specific embodiment 1, the method also includes, in step 3, in the opened fault record file, check whether the fault coding information has been recorded in this startup, if yes, in the current startup times Record the fault code information directly in the directory; if not, record the number of startups this time, mark that the fault information has been recorded in this startup, and then record the fault code information this time.

specific Embodiment 3

[0056] On the basis of the specific embodiment 1 or 2, the fault code information further includes the number of fault occurrences, which refers to the number of occurrences of the fault type in the fault code information.

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Abstract

The invention provides an airborne anti-collision system failure recording method; in the case that an airborne anti-collision system experiences a failure change, encoding the failure change; recording the information such as a failure code to a corresponding failure recording file; compared with the prior art, the method may determine the information such as failure occurring time, failure content, failure state, failure times and failure types according to the failure recording information of the failure file, enables a failure to be quickly located, and accurately and specifically describes the failure change process during a flight, and the maintenance time of TCASII airborne anti-collision system is greatly shortened; great assistance is provided for clearing the failure of the TCASII airborne anti-collision system and analyzing possible potential issues; the problems are solved that the conventional recording approach with failure redundant recordings has no 'failure recovery' recording and fails to provide elaborate accurate locating.

Description

technical field [0001] The invention relates to a fault recording method of an airborne anti-collision system, in particular to a fault recording method applicable to a TCASII airborne anti-collision system. Background technique [0002] TCASII is an integrated 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 a complex structure. The entire system consists of an S-mode transponder, a transceiver host, an antenna switch, a directional antenna, an omnidirectional antenna, a traffic decision display or an inte...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G07C5/08G08G5/04
CPCG07C5/0808G08G5/04
Inventor 马少阳刘永刚李涛付红
Owner 四川九洲空管科技有限责任公司
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