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Aircraft cargo loading method, device and equipment and storage medium

A technology for aircraft and aircraft take-off, applied in the Internet field, can solve the problem of low transportation timeliness, and achieve the effect of improving transportation timeliness

Inactive Publication Date: 2019-03-08
顺丰航空有限公司 +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, in the field of cargo transportation, foreign countries have realized automatic aircraft cargo loading through operations research, but all of them only consider the requirements of the center of gravity, and the transportation timeliness is low

Method used

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  • Aircraft cargo loading method, device and equipment and storage medium
  • Aircraft cargo loading method, device and equipment and storage medium
  • Aircraft cargo loading method, device and equipment and storage medium

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0028] figure 2 It is a schematic flow chart of the aircraft cargo loading method provided in Embodiment 1 of the present invention. The executive body of this embodiment may be the aircraft cargo loading device provided in the embodiment of the present invention. This device can be integrated into a mobile terminal device (for example, a smart phone, Tablet PC, etc.), can also be integrated in a fixed terminal (desktop computer) or server, and the aircraft cargo loading device can be realized by hardware or software. Below will be described in conjunction with embodiment, as figure 2 shown, including:

[0029] S201. Determine the cargo priority value according to the attributes of the cargo;

[0030] Among them, the attributes of the loaded goods include but are not limited to time-limitation requirements or transit requirements.

[0031] Specifically, the timeliness requirements for goods are divided into same-day delivery, next-day delivery, and next-day delivery, etc....

Embodiment 2

[0039] image 3 It is a schematic flow chart of the aircraft cargo loading method provided by Embodiment 2 of the present invention. On the basis of the above embodiments, this embodiment determines the corresponding loading of cargo and space according to the center of gravity requirements that the aircraft needs to meet for take-off and the cargo priority value of the cargo Relationships include:

[0040] S301, counting the quantity of goods and the quantity of shipping spaces;

[0041] S302. Calculate the corresponding loading relationship between the cargo and the shipping space according to the statistical results.

[0042] Furthermore, the calculation of the corresponding loading relationship between cargo and shipping space based on statistical results can be achieved in the following ways:

[0043] According to the formula Establishing an objective function, and determining the corresponding loading relationship between the cargo and the berth by solving the maximu...

Embodiment 3

[0051] In this embodiment, on the basis of the above-mentioned embodiments, the calculation of the corresponding loading relationship between the cargo and the space according to the statistical results further includes: when establishing the objective function, in the objective function, further adding the first item of the cargo that is guaranteed to be loaded the most, which is And the second term that minimizes the moment difference between the aircraft's front, rear and left and right cargo relative to the aircraft's optimal center of gravity, namely Specifically include:

[0052] According to the formula or formula Establish an objective function, and determine the loading sequence of high-priority cargo by solving the objective function under the constraints of the center of gravity requirements that the aircraft needs to meet for takeoff; where, N ULD is the total number of ULDs that can be loaded; N POS is the total number of cabins where ULD can be installed ...

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PUM

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Abstract

The present invention discloses an aircraft cargo loading method, device and equipment and a storage medium, wherein the method comprises determining a cargo priority value according to an attribute of the cargo; determining a class priority value according to the class attribute; determining the corresponding loading relationship between cargo and cargo space according to the center of gravity requirement and cargo priority value that the aircraft needs to meet when taking off. According to the technical proposal of the embodiment of the invention, the transportation process of the goods is more intelligent, and the transportation efficiency of the goods can be improved.

Description

technical field [0001] The present disclosure relates to the technical field of the Internet, and in particular to an aircraft cargo loading method, device, equipment and storage medium. Background technique [0002] With the rapid development of the logistics field, leading logistics companies are using aviation resources to transport express shipments, and each aircraft uses multiple aviation container units (Unit Load Device, ULD) that meet international standards to load express shipments. Aircraft manufacturers have strict requirements for the center of gravity of each aircraft. The center of gravity of the aircraft must meet the corresponding take-off conditions under the three conditions of take-off weight, fuel-free weight, and landing weight after the aircraft is loaded. [0003] specific reference figure 1 As shown, the ordinate is the gross weight of the aircraft, in KG; the abscissa is the aircraft index value (INDEX), which refers to the moment value that is re...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06Q10/04G06Q10/08
CPCG06Q10/04G06Q10/083
Inventor 李娜黄林赵雪松李增恺禹楚航
Owner 顺丰航空有限公司
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