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Air Combat Maneuvering Decision-Making Method and Device

A decision-making method and maneuvering technology, applied in computer-aided design, complex mathematical operations, geometric CAD, etc., to achieve fast and efficient air combat maneuver decision-making, reducing real-time and accuracy effects

Active Publication Date: 2022-04-08
INST OF AUTOMATION CHINESE ACAD OF SCI
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The present invention provides a method and device for air combat maneuver decision-making, which is used to solve the defect that air combat maneuver decision-making cannot be made quickly and efficiently in the prior art, and realize fast and efficient air combat maneuver decision-making

Method used

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Embodiment Construction

[0046] In order to make the purpose, technical solutions and advantages of the present invention clearer, the technical solutions in the present invention will be clearly and completely described below in conjunction with the accompanying drawings in the present invention. Obviously, the described embodiments are part of the embodiments of the present invention , but not all examples. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0047] figure 1 It is a schematic flow chart of the air combat maneuver decision-making method provided by the present invention. refer to figure 1 , the air combat maneuver decision-making method provided by the present invention may include:

[0048] Step 110, constructing an air combat model of the aircraft according to the actual performance constraints of the aircraft;

[0049] Step ...

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Abstract

The present invention provides an air combat maneuver decision-making method and device. The method includes: constructing an aircraft air combat model according to the actual performance limiting factors of the aircraft; The state sets different decision-making cycles; according to the state of the aircraft after the decision-making cycle is set, the target air combat maneuver instructions corresponding to different aircraft states are respectively determined; according to the target air combat maneuver instructions and the aircraft air combat model, the air combat maneuver decision is made for the aircraft; among them, the aircraft Status includes: altitude, heading angle and speed. The air combat maneuver decision-making method and device provided by the present invention set different decision-making periods for the maneuver decision-making of different aircraft states through the dynamic response characteristics of different aircraft states under the control system, which can effectively reduce the real-time and accuracy of air combat maneuver decision-making. The contradiction between characteristics, to achieve fast and efficient air combat maneuver decision-making.

Description

technical field [0001] The invention relates to the technical field of aircraft air combat maneuver decision-making, in particular to a method and device for air combat maneuver decision-making. Background technique [0002] In modern air combat, based on the advantages and limitations brought by air-to-air missile technology, pilots often take a large number of maneuvers to find the best air combat position and launch air-to-air missiles to attack enemy aircraft on the premise of ensuring that our aircraft is not shot down. Therefore, the scramble for a favorable position in air combat has become one of the key issues in air combat confrontation. On the other hand, with the complexity and diversification of aircraft air combat missions and environments, the complexity of aircraft air combat maneuver decision-making is also increasing. [0003] At present, the aircraft air combat maneuver decision-making algorithms are all based on fixed-period design, and the maneuver deci...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F30/15G06F30/20G06F17/16G06F119/12
CPCG06F30/15G06F30/20G06F17/16G06F2119/12
Inventor 刘振周志明付清旭蒲志强丘腾海易建强
Owner INST OF AUTOMATION CHINESE ACAD OF SCI
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