Air defense missile weapon hit probability correction method based on combat simulation system

A combat simulation system and air defense missile technology are applied in the field of hit probability correction of air defense missile weapons, which can solve problems such as intractable and difficult to handle, and achieve the effect of improving efficiency and enhancing engineering operability.

Active Publication Date: 2021-03-09
NAVAL UNIV OF ENG PLA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

But for multi-dimensional problems, it is very difficult to deal with segmentation, because a surface or a curve will appear in the segmentation of multi-dimensional problems or even a higher-dimensional situation
For the emergence of high-dimensional situations, fitting segmentation is very difficult to deal with
[0010] The Bayes method requires pre-test data and field test data, and is mainly used for parameter estimation and identification of air defense missile hit probability, and is not suitable for combat simulation deduction

Method used

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  • Air defense missile weapon hit probability correction method based on combat simulation system
  • Air defense missile weapon hit probability correction method based on combat simulation system
  • Air defense missile weapon hit probability correction method based on combat simulation system

Examples

Experimental program
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Effect test

Embodiment

[0083] Embodiment: When fighting against an aircraft target, the hit probability P after the correction of the combating distance of the combating aircraft is calculated respectively by the step 1 of the above-mentioned technical solution 抗击距离修正 , The hit probability P after the corrected speed of the combat aircraft target 目标速度修正 , Calculate the hit probability P after the maneuverability correction of the combat aircraft target 机动系数修正 , calculate the corrected hit probability P of the air defense missile weapon against the aircraft target by step 2 of the above technical scheme 抗击飞机目标突防海拔高度修正 , multiplied to obtain the corrected hit probability against aircraft targets.

[0084] When fighting against the guided target, the corrected hit probability P of the anti-aircraft missile weapon against the guided target is calculated by step 2 of the above technical scheme 抗击制导目标突防海拔高度修正 , the hit probability P of the counter-guided target corrected by the azimuth angle correction ...

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Abstract

The invention relates to an air defense missile weapon hit probability correction method based on a combat simulation system. The method comprises the following steps: calculating the hit probabilityof an anti-hit airplane after the anti-hit distance is corrected; calculating the hit probability of the corrected target speed of the strike-resistant aircraft; calculating the hit probability afterthe maneuverability of the anti-impact aircraft target is corrected; calculating the corrected hit probability of the air defense missile weapon anti-impact airplane target or anti-impact guidance target; and 3, calculating the hit probability of the anti-impact guidance target with the corrected azimuth angle of the anti-impact guidance target. The method is based on a combat simulation system, the hit probability of the air defense missile weapon is corrected online in real time by adopting a method of combining a mathematical analysis model and numerical fitting, the efficiency is improved,and the engineering operability is enhanced.

Description

technical field [0001] The invention relates to the technical field of application of missile weapon systems, in particular to a method for correcting the hit probability of air defense missile weapons based on a combat simulation system. [0002] technical background [0003] Anti-aircraft missile hit probability (hit probability) belongs to the evaluation index of missile combat effectiveness. The hit of the missile includes the correct positioning of the missile, the fragments and detonation products covering the target, the three sequential events of the fragments and detonation products hitting the target, the characteristics of the target's motion and geometric characteristics, and the power ring and power circle formed by different warheads. The two basic elements of the geometric characteristics. The estimation of hit probability belongs to the problem of missile test qualification and effectiveness evaluation. [0004] The key technologies of air defense missile hi...

Claims

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Application Information

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IPC IPC(8): G06F30/20G06F111/10G06F111/08
CPCG06F30/20G06F2111/08G06F2111/10
Inventor 黄隽刘方李晓宝刘玥
Owner NAVAL UNIV OF ENG PLA
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