Method for batch calculation of multi-model performance chart data based on SCAP protocol

一种数据、性能的技术，应用在计算、数据处理应用、文件/文件夹操作等方向，能够解决无法批量计算性能图表数据等问题，达到提高制作效率、降低人为差错隐患、减轻工作负荷的效果

Inactive Publication Date: 2022-08-02
CHINA AVIATION NAVIGATION DATA (BEIJING) CO LTD
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  • Description
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AI Technical Summary

Problems solved by technology

[0006] In order to solve the problem that the current multi-model, multi-vendor and multi-performance computing software cannot batch calculate the performance chart data, the present invention provides a method for batch calculation of multi-model performance chart data based on the SCAP protocol
Especially for airlines with multiple aircraft types, the problem of calculating performance chart data in large quantities when updating the airport data cycle every 28 days

Method used

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Embodiment Construction

[0066] In order to make the objectives, technical solutions and advantages of the present invention clearer, further detailed description will be given below with reference to specific embodiments and accompanying drawings. It should be understood that the specific embodiments described herein are only used to explain the present invention, but not to limit the present invention.

[0067] At present, the reality of the coexistence of multi-model, multi-manufacturer and multi-performance computing software generally exists in various airlines, and the performance parameter standards of different aircraft performance computing software provided by various aircraft manufacturers are also quite different, which makes it impossible to perform batch calculation. Multi-model performance chart data, manual calculation workload is large and there is a risk of human calculation errors, which endangers the safety of aviation operations.

[0068] Based on this, the present invention propo...

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Abstract

The invention discloses a method for batch calculation of multi-model performance chart data based on an SCAP protocol. The method comprises the following steps: configuring model parameter data based on the SCAP protocol; generating a calculation input file according to the configured model parameter data based on an SCAP protocol; calling a kernel file of the manufacturer performance calculation software in combination with the calculation input file to obtain output result data; verifying the consistency of the output result data and the result data of the manufacturer performance calculation software; configuring a performance chart calculation template according to the model; generating a calculation input file according to the configured performance chart calculation template based on the SCAP protocol; calling a kernel file of the manufacturer performance calculation software to obtain output result data; analyzing the output result data and generating performance chart data; the method is applied to the production work of the takeoff and landing performance chart data of the airline company, the workload can be reduced, the human error rate is reduced, and the aviation operation safety is improved.

Description

technical field [0001] The invention relates to the technical field of aircraft performance calculation, in particular to a method for batch calculation of multi-model performance chart data based on the SCAP protocol. Background technique [0002] With the gradual expansion of civil aviation flight volume, flight safety has become particularly important. Civil aviation flight safety is not only related to the safety of passengers' lives and property, but also to the future development of the entire civil aviation industry, and also reflects my country's national image. [0003] The performance calculation software refers to the aircraft manufacturer's performance data in different stages of take-off, climb, cruise, descent, waiting and landing, through a specific and approved mathematical model, to calculate and determine the weight and speed of the aircraft in the above-mentioned stages. Calculation software for key parameters such as altitude, fuel consumption and distanc...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06Q10/10G06Q50/30G06F16/16
CPCG06Q10/10G06F16/16G06Q50/40Y02T90/00
Inventor 宋江文邢维论曹忠赞李宗奎任振杰宋柯
Owner CHINA AVIATION NAVIGATION DATA (BEIJING) CO LTD
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