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Airplane take-off and landing early warning method based on flight simulation platform and wind measurement laser radar

A wind-measuring lidar and flight simulation technology, applied in the field of flight simulation technology and wind-measuring lidar, can solve the problems of lack of wind speed data fusion research, to overcome the difficulty of airport wind shear forecast, ensure take-off and landing safety, and intuitively dangerous effect of forecast

Pending Publication Date: 2019-08-23
山东国耀量子雷达科技有限公司
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  • Summary
  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, most of the wind speed data used for low-altitude wind shear and flight simulation fusion research at home and abroad are based on simulated data and databases, and there is a lack of fusion research based on measured wind speed data.

Method used

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  • Airplane take-off and landing early warning method based on flight simulation platform and wind measurement laser radar
  • Airplane take-off and landing early warning method based on flight simulation platform and wind measurement laser radar
  • Airplane take-off and landing early warning method based on flight simulation platform and wind measurement laser radar

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Embodiment

[0058] figure 1 The flowchart of the aircraft take-off and landing warning method based on the flight simulation platform and wind-measuring laser radar provided by the embodiment of the present invention; figure 1 Shown, a kind of aircraft take-off and landing warning method based on flight simulation platform and wind-measuring lidar, based on wind-measuring lidar, described lidar system is arranged at the target airport, and described method comprises:

[0059] Step S1, acquiring the runway information of the target airport.

[0060] The runway information includes runway code, longitude, latitude, altitude, runway length, runway width, takeoff point number and landing point number; the runway information of the aircraft is mainly used for the calibration of the takeoff and landing paths of the aircraft.

[0061] Step S2, obtaining real-time flight information, and setting an aircraft control panel for the target aircraft according to the flight information;

[0062] Spec...

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Abstract

The invention discloses an airplane take-off and landing early warning method based on a flight simulation platform and a wind measurement laser radar. According to the method, a built-in flight dynamics solver JSBSim of a FlightGear platform is compiled into a dynamic link library; a wind profile of a take-off area and a wind profile of a descending area are measured in real time through a wind measurement laser radar, a flight path is predicted by calling a JSBSim dynamic link library and related flight scripts, a flight data result is displayed on a user interface through a UDP interface, and danger early warning of airplane take-off and landing is achieved. Early warning is carried out according to the flight parameters and the aircraft trajectory, so that a user can more intuitively judge the influence of wind shear and turbulence on the aircraft, and the efficiency and accuracy of early warning of danger are improved. The method is used for guaranteeing the safety of takeoff andlanding of the civil aircraft, and has the advantages of high flexibility, high response speed and high accuracy.

Description

technical field [0001] The invention relates to the fields of flight simulation technology and wind-measuring laser radar, in particular to an aircraft take-off and landing warning method based on a flight simulation platform and wind-measuring laser radar. Background technique [0002] In recent years, aviation flight safety has attracted much attention. Wind shear is one of the main culprits in the downfall of large airliners. Low-altitude wind shear is the change of wind vector from one point to another point in the space below the height of 600m, which is the vector difference of wind speed between two points. Encountering low-altitude wind shear will cause an instantaneous change in the speed of the aircraft, which in turn will cause a change in the lift of the aircraft, causing the flight track to deviate from the course and cause an accident. The international aviation community believes that the consequences of wind shear during the entire flight mainly seriously a...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F17/50G06Q10/04G06Q10/06G06Q50/30G01S17/58G01S17/95
CPCG06Q10/04G06Q10/0635G01S17/95G01S17/58G06F30/15G06F2119/06G06F30/20G06Q50/40Y02A90/10
Inventor 袁金龙岳斌夏海云
Owner 山东国耀量子雷达科技有限公司