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Go-around risk detecting and evaluating method for aircraft

An evaluation method and aircraft technology, applied in the field of risk evaluation, can solve the problems that the characteristics of go-around risk changes cannot be expressed quantitatively, the evaluation results are qualitative and single, and the flight process of the aircraft is less considered.

Active Publication Date: 2015-02-25
哈尔滨哈船智控科技有限责任公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

After the go-around point is determined, if the go-around decision is made after flying over this point, the pilot does not have enough time to correct the deviation or the visual height is high, which will cause the aircraft to collide with the ground, resulting in the risk of go-around and accidents
[0005] The traditional go-around risk assessment method only qualitatively classifies the go-around risk based on a single go-around point, and cannot quantitatively express the changing characteristics of the go-around risk. The evaluation results are qualitative and single; the traditional go-around risk assessment method does not analyze the transition from normal flight status to The change of the state quantity of the aircraft itself in the go-around state, the analysis of the influencing factors of the evaluation is relatively limited; the traditional go-around risk evaluation method only uses the go-around point (a certain point in the flight space) as the basis for judging the go-around risk, and takes less consideration of the overall flight process of the aircraft , the real-time performance is poor; in summary, the traditional go-around risk assessment method cannot fully express the risks existing in the process of the aircraft's go-around maneuver in real time

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  • Go-around risk detecting and evaluating method for aircraft

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Embodiment Construction

[0036] Below in conjunction with accompanying drawing, the present invention will be further described:

[0037] What this embodiment described is a kind of aircraft go-around risk dynamic evaluation method based on BP neural network, and its specific implementation steps are as follows:

[0038] 1 Establish flight status data set

[0039] For a specific model, by performing multiple programmed go-arounds on the simulator, record the real-time status data of the aircraft during the go-around maneuver of the model, including flight position information (gx, gy, gz), flight speed information (vx , vy, vz), flight acceleration information (ax, ay, az) and flight attitude information (α, β), where gx is the longitudinal flight position of the aircraft, gy is the lateral flight position of the aircraft, gz is the vertical flight position of the aircraft, vx is the longitudinal flight speed of the aircraft, vy is the lateral flight speed of the aircraft, vz is the vertical flight s...

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Abstract

The invention relates to a risk detecting and evaluating method, in particular to a go-around risk detecting and evaluating technique based on an error back propagation neural network. The risk detecting and evaluating method comprises the following steps of (1) building a flying status data set; (2) building a go-around surplus distance data set; (3) conducting risk assessment; and (4) determining a relation between go-around surplus distances and land collision risks. The go-around risk detecting and evaluating method is wide in application, can conduct risk measurement on any flying state of the aircraft, provides reasonable references for go-around maneuvering safety under emergency circumstances and improves go-around safety.

Description

technical field [0001] The present invention relates to a risk assessment method, in particular to a dynamic assessment technology for aircraft go-around risk based on error back propagation (Back Propagation, BP) neural network. Background technique [0002] When the aircraft is about to land, if the pilot thinks it is unsafe to continue landing due to obstacles suddenly appearing on the runway or the observation is affected by the low visibility of the weather, or the aircraft body temporarily malfunctions, the pilot should increase the thrust to interrupt the landing of the aircraft and restart the aircraft. The process of turning into a normal ascent state is called a go-around. Go-around is a backup for normal landing, and it is not used in general, but it is an important measure to ensure flight safety. [0003] Go-around is one of the standing flight maneuvers, and there are certain risks in its maneuvering process. When the pilot decides to perform a go-around oper...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06N3/02
Inventor 朱齐丹李晖夏桂华张智张雯蔡成涛刘志林闻子侠喻勇涛于梦竹
Owner 哈尔滨哈船智控科技有限责任公司
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