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Reactive wind shear false alarm suppression method fused with meteorological radar information

A weather radar and wind shear technology is applied in the field of radar to reduce the probability of false alarms and improve performance.

Pending Publication Date: 2022-04-01
LEIHUA ELECTRONICS TECH RES INST AVIATION IND OF CHINA
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  • Application Information

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Problems solved by technology

[0004] If the standard F-factor method is used for reactive windshear, there will be certain limitations. Specifically, it is easily affected by turbulence and will generate windshear false alarms. In addition, the maneuvering actions of the aircraft during flight will also generate windshear false alarms.

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  • Reactive wind shear false alarm suppression method fused with meteorological radar information
  • Reactive wind shear false alarm suppression method fused with meteorological radar information
  • Reactive wind shear false alarm suppression method fused with meteorological radar information

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Embodiment Construction

[0041] Embodiments of the present application will be described in detail below in conjunction with the accompanying drawings.

[0042] It should be noted that, in the case of no conflict, the embodiments in the present application and the features in the embodiments can be combined with each other. The present invention will be described in detail below with reference to the accompanying drawings and examples.

[0043] Such as Figure 1 to Figure 5 As shown, the embodiment of the present invention provides a reactive windshear false alarm suppression method for fusing weather radar information, comprising the following steps:

[0044] Step 1. Perform wind field inversion on the wind field information;

[0045]Step 2. Introduce wind field information to judge turbulence, correct integration time and extract predictive wind shear F factor;

[0046] Step 3: Calculate the reactive windshear F factor according to the reactive windshear method, and compare it with the warning th...

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Abstract

The invention provides a reactive wind shear false alarm suppression method fused with meteorological radar information. The reactive wind shear false alarm suppression method comprises the following steps of 1, performing wind field inversion on wind field information; 2, wind field information is introduced for turbulence judgment, integral duration is corrected, and a predictive wind shear F factor is extracted; 3, calculating a reaction formula wind shear F factor according to a reaction formula wind shear mode, and comparing the F factor with an alarm threshold to obtain a wind shear alarm result; 4, calculating and comparing the reaction type wind shear F factor and the F factor of the aircraft position point in wind field inversion, if the integral average difference value of the reaction type wind shear F factor and the prediction type wind shear F factor is greater than the tolerance, detecting the maneuvering action type, and finishing the correction of the reaction type wind shear F factor; if the integral average difference value of the reactive formula wind shear F factor and the F factor of the aircraft position point in the wind field inversion is smaller than the tolerance, generating a wind shear alarm; and step 5, obtaining a corrected F factor.

Description

technical field [0001] The invention relates to the technical field of radar, in particular to a reactive windshear false alarm suppression method for fusing meteorological radar information. Background technique [0002] According to the alarm principle, the windshear detection system is divided into two categories: predictive type (forward-looking type) and reactive type (current state type). Based on the predictive windshear function of airborne meteorological radar, windshear characteristic parameters such as echo power, Doppler wind speed, and spectral width are extracted from radar echoes to judge the existence and danger of windshear. Capable of detecting windshear information on distant routes. [0003] Reactive windshear is when the aircraft is in the wind shear wind field, the airspeed, angle of attack, sideslip angle provided by the air data computer (ADC), and the aircraft speed and attitude information provided by the inertial reference system (IRS) , to calcu...

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Application Information

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IPC IPC(8): G01S13/95G01S7/41
CPCY02A90/10
Inventor 孙慧娟臧士新吕占喆
Owner LEIHUA ELECTRONICS TECH RES INST AVIATION IND OF CHINA
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