Air combat maneuver decision-making method and device

A decision-making method and maneuvering technology, applied in computer-aided design, complex mathematical operations, special data processing applications, etc., to achieve fast and efficient air combat maneuver decision-making, reduce real-time and accuracy effects

Active Publication Date: 2022-01-21
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 com...

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  • Air combat maneuver decision-making method and device
  • Air combat maneuver decision-making method and device

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Embodiment Construction

[0046] In order to make the objects, technical solutions, and advantages of the present invention, the technical solutions in the present invention will be apparent from the drawings of the present invention, and it will be described in connection with the drawings of the present invention. , Not all of the embodiments. Based on the embodiments in the present invention, all other embodiments obtained without creative labor are not made in the premise of creative labor.

[0047] figure 1 It is a flow chart of the air-war motor decision method provided by the present invention. Refer figure 1 The air combat machine decision method provided by the present invention can include:

[0048] Step 110, according to the actual performance limit factor of the aircraft, construct aircraft air combat model;

[0049] Step 120, according to the time of the dynamic response of the aircraft state under the flight control system, different decision cycles are set differently;

[0050] Step 130, ba...

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Abstract

The invention provides an air combat maneuver decision-making method and device, and the method comprises the steps: constructing an aircraft air combat model according to the actual performance limiting factors of an aircraft; respectively setting different decision periods for different aircraft states according to the dynamic response time of the aircraft states under the control of a flight control system; according to the aircraft states after the decision period is set, determining target air combat maneuvering instructions corresponding to different aircraft states; and according to the target air combat maneuvering instruction and the aircraft air combat model, performing an air combat maneuvering decision on the aircraft, wherein the aircraft states comprise the height, the course angle and the speed. According to the air combat maneuver decision-making method and device, different decision-making periods are set for maneuver decisions of different aircraft states through the dynamic response characteristics of different aircraft states under the control system, the contradiction between the real-time performance and the accuracy of air combat maneuver decision-making can be effectively relieved, and rapid and efficient air combat maneuver decision making is realized.

Description

Technical field [0001] The present invention relates to the field of aerobic air operations, in particular, involving an air-war mobile decision making method and apparatus. Background technique [0002] In modern air combat, based on the advantages and limitations of air missile technology, pilots often take a lot of motorized actions. Under the premise of ensuring that our machine is not hit, look for the optimal air combat position, the opportunity to launch an empty missile attack enemy machine, Therefore, it is one of the key issues of favorable positions in air warfare. On the other hand, with the complexity and diversification of the aircraft airfare tasks and the environment, the complexity of the aircraft air combat mobile decision is also increasing. [0003] At present, the aircraft air-war motor decision algorithm is based on fixed cycle design, and mobile decisions in different aircraft status are in accordance with unified time cycle decisions. However, the dynamic ...

Claims

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Application Information

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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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