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Flight trajectory optimization method and system based on dynamic sampling

A technology of flight trajectory and dynamic sampling, applied in registration/indication of vehicle operation, structured data retrieval, instruments, etc., can solve the problems of large adoption rate setting, display distortion, large data volume, etc., to improve the level of safety capability, The effect of shielding jumps and saving storage space

Pending Publication Date: 2022-05-13
SHANDONG AIRLINES CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] (1) if figure 1 As shown, the amount of presented data is large and takes up a lot of resources;
[0008] (2) if figure 2 As shown, a single data error will seriously affect the rendering effect
[0011] Disadvantage one: if image 3 As shown, for the turn information, the data loss is serious, the display is distorted, and the presentation pattern is not smooth enough;
[0012] Disadvantage 2: The adoption rate setting is large, the data volume increases, the adoption rate is small, and the information details cannot be reflected

Method used

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  • Flight trajectory optimization method and system based on dynamic sampling
  • Flight trajectory optimization method and system based on dynamic sampling
  • Flight trajectory optimization method and system based on dynamic sampling

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0057] This embodiment provides a flight trajectory optimization method based on dynamic sampling;

[0058] Such as Figure 7 As shown, the flight trajectory optimization method based on dynamic sampling includes:

[0059] S101: Obtain the data of the airborne quick access recorder QAR; create an empty array L, and sample and record data idx=0;

[0060] S102: Load the data of the quick access recorder QAR one by one in chronological order;

[0061] S103: Determine whether the ground speed at the current time point is greater than the first set threshold; if yes, enter S104, if not, return to S102;

[0062] S104: Determine whether the difference between the heading in the previous second and the heading at the current time point is greater than the second set threshold; if yes, go to S105; if not, go back to S102; add one to the sampling record data idx;

[0063] S105: judge whether the sampling record data idx is a multiple of the third set threshold, if yes, record the lat...

Embodiment 2

[0081] This embodiment provides a flight trajectory optimization system based on dynamic sampling;

[0082] Flight trajectory optimization system based on dynamic sampling, including:

[0083] The acquisition module is configured to: acquire the data of the airborne quick access recorder QAR; establish an empty array L, and sample and record data idx=0;

[0084] The loading module is configured to: load the data of the quick access recorder QAR one by one in chronological order;

[0085] The first judging module is configured to: judge whether the ground speed at the current time point is greater than the first set threshold; if yes, enter the second judging module and the third judging module, if not, return to the loading module;

[0086] The second judging module is configured to: judge whether the difference between the heading in the previous second and the heading at the current time point is greater than the second set threshold; if yes, enter the third judging module,...

Embodiment 3

[0093] This embodiment also provides an electronic device, including: one or more processors, one or more memories, and one or more computer programs; wherein, the processor is connected to the memory, and the one or more computer programs are programmed Stored in the memory, when the electronic device is running, the processor executes one or more computer programs stored in the memory, so that the electronic device executes the method described in Embodiment 1 above.

[0094] It should be understood that in this embodiment, the processor can be a central processing unit CPU, and the processor can also be other general-purpose processors, digital signal processors DSP, application specific integrated circuits ASIC, off-the-shelf programmable gate array FPGA or other programmable logic devices , discrete gate or transistor logic devices, discrete hardware components, etc. A general-purpose processor may be a microprocessor, or the processor may be any conventional processor, o...

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PUM

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Abstract

The invention discloses a flight path optimization method and system based on dynamic sampling. The method comprises the following steps: acquiring data of an airborne quick access recorder QAR; establishing a null array L, and sampling and recording data idx = 0; loading data of the quick access recorder QAR item by item according to a time sequence; judging whether the ground speed at the current time point is greater than a first set threshold; if yes, whether the difference value between the course of the previous second and the course of the current time point is larger than a second set threshold value or not is judged; if yes, whether the sampling record data idx is a multiple of a third set threshold value or not is judged, and if yes, longitude and latitude information of the current aircraft position point is recorded; putting longitude and latitude information of a current aircraft position point into an array L; and judging whether QAR data circulation is completed or not, and if yes, outputting the current array L as a result. Longitude and latitude information is sampled according to course change conditions, and smooth track display is realized.

Description

technical field [0001] The invention relates to the technical field of trajectory optimization, in particular to a dynamic sampling-based flight trajectory optimization method and system. Background technique [0002] The statements in this section merely mention the background technology related to the present invention and do not necessarily constitute the prior art. [0003] A flight trajectory is the linear trajectory of a flight's itinerary. By analyzing the trajectory of the flight, you can find out the points that can be optimized for the flight operation. For example, analyze whether there is a detour or a direct flight during the flight operation. We should minimize the detour and increase the direct flight, which can save fuel and save flight time. , to increase user experience. In addition, by comparing the flight trajectory with the standard arrival and departure procedures, the flight operation SOP can be optimized, the pilot's ability to enter and leave the a...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F16/2457G06F16/248G06F16/29G07C5/08
CPCG06F16/24575G06F16/248G06F16/29G07C5/085
Inventor 侯研崔昊张申利许洪澎任海军庄德全
Owner SHANDONG AIRLINES CO LTD