Aircraft route planning method

A route planning and planning technology, applied in the direction of navigation calculation tools, etc., can solve problems such as large solution space, inability to effectively avoid dynamic threat sources, and difficulty in meeting the timeliness requirements of aircraft route planning.

Pending Publication Date: 2020-03-17
SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
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AI Technical Summary

Problems solved by technology

[0004] 1) Using the full connection method, the solution space is huge in the three-dimensional situation environment, and the number of pre-generated auxiliary waypoints is large, which is difficult to meet the timeliness requirements of aircraft route planning;
[0005] 2) The route planned based on it can only avoid static threat sources, but cannot effectively avoid dynamic threat sources

Method used

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Embodiment Construction

[0047] The application will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the related application, not to limit the application. In addition, it should be noted that, for ease of description, only parts relevant to the present application are shown in the drawings.

[0048] It should be noted that, in the case of no conflict, the embodiments in the present application and the features in the embodiments can be combined with each other. The present application will be described in detail below with reference to the accompanying drawings and embodiments.

[0049] It should be noted that in the description of this application, the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. The terms of the indicated direction or positional relationship are based on the direction or positional ...

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Abstract

The invention belongs to the technical field of aircraft route planning, and particularly relates to an aircraft route planning method which comprises the following steps: step 1, discretizing a situation space to obtain a plurality of discrete points; step 2, generating a heuristic factor matrix of each discrete point; step 3, taking the discrete point at a planning starting point as a current planning point; step 4, selecting discrete points meeting the safe flight condition of the aircraft in the current planning point range to form a set of next planning points of the discrete points; step5, judging whether the set is empty or not; step 6, if the set is not empty, selecting a next planning point from the set based on the heuristic factor matrix and the pheromone matrix thereof to update the current planning point; judging whether the current planning point is a discrete point at the planning end point or not, and if not, returning to the step 4; if so, searching to obtain and store a planned route; and step 7, if the set is empty, searching to obtain and store the planned route.

Description

technical field [0001] The application belongs to the technical field of aircraft route planning, and in particular relates to an aircraft route planning method. Background technique [0002] In order to avoid being threatened by threat sources, the aircraft needs to plan its flight route in advance in order to avoid various scattered threat sources effectively. [0003] At present, the flight route of the aircraft is mostly planned based on the A* algorithm. This technical solution has the following defects: [0004] 1) Using the full connection method, the solution space is huge in the three-dimensional situation environment, and the number of pre-generated auxiliary waypoints is large, which is difficult to meet the timeliness requirements of aircraft route planning; [0005] 2) The route planned based on it can only avoid static threat sources, but cannot effectively avoid dynamic threat sources. [0006] The present application is proposed in view of the above-mention...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01C21/20
CPCG01C21/20
Inventor 吕明伟张少卿王言伟刘伟
Owner SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
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