Aircraft noise monitoring method and device thereof
A technology of aircraft noise and aircraft, which is applied in the field of aircraft noise monitoring methods and devices, and can solve the problems of inability to objectively and accurately evaluate the impact of aircraft noise and noise
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no. 1 example
[0026] Please refer to figure 2 , figure 2 It is a flowchart of an aircraft noise monitoring method provided by the first embodiment of the present invention. The following will be figure 2 The process shown is described in detail, and the method includes:
[0027] Step S110: Obtain flight parameters and actual meteorological data of the aircraft in the monitoring environment. The flight parameters include aircraft type, engine power, and airport runway information. The actual meteorological data include air pressure, air temperature, relative humidity, and wind speed.
[0028] According to the regulations of ICAO (International Civil Aviation Organization), the meteorological conditions for airport noise measurement are: pressure value 1013.25 hPa, temperature 25 degrees Celsius, relative humidity 70% and no wind. However, the meteorological conditions of the airport are usually difficult to meet this standard. In actual measurement, the temperature value is 2 degrees Cel...
no. 2 example
[0051] Please refer to Figure 4 , Figure 4 It is a flowchart of an aircraft noise monitoring method provided by the second embodiment of the present invention. The following will be Figure 4 The process shown is described in detail, and the method includes:
[0052] Step S210: Obtain flight parameters and actual meteorological data of the aircraft in the monitoring environment. The flight parameters include aircraft type, engine power, and airport runway information. The actual meteorological data include air pressure, air temperature, relative humidity, and wind speed.
[0053] Step S220: Correct the flight track of the aircraft type on the airport runway based on the pre-saved broadcast and climb rules, the flight parameters and actual weather data.
[0054] Step S230: Obtain a random prediction point, and calculate the slant distance between the aircraft of the type and the random prediction point on the airport runway based on the corrected flight track.
[0055] St...
no. 3 example
[0061] Please refer to Figure 5 , Figure 5 It is a structural block diagram of an aircraft noise monitoring device provided by the third embodiment of the present invention. The following will be Figure 5 The illustrated structural block diagram is for illustration, and the illustrated apparatus 400 includes: an acquisition module 410 , a correction module 420 , a first calculation module 430 , a second calculation module 440 , a third calculation module 450 and a fourth calculation module 460 .
[0062] The obtaining module 410 is used to obtain flight parameters and actual meteorological data of the aircraft in the monitoring environment. The flight parameters include aircraft type, engine power, airport runway information, and the actual meteorological data include air pressure, air temperature, relative humidity and wind speed.
[0063] The correction module 420 is configured to correct the flight track of the aircraft type on the airport runway based on the pre-saved...
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