Air-ground missile hitting precision evaluation method based on error spectrum

A hit accuracy and missile technology, applied in the field of air-to-ground missile hit accuracy evaluation based on error spectrum, can solve the problem of unsteady evaluation index

Pending Publication Date: 2019-07-09
AIR FORCE UNIV PLA
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AI Technical Summary

Problems solved by technology

[0004] In order to scientifically, reasonably and comprehensively determine the key measurement index value of air-to-ground missile hit accuracy, the present invention is based on an e

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  • Air-ground missile hitting precision evaluation method based on error spectrum
  • Air-ground missile hitting precision evaluation method based on error spectrum
  • Air-ground missile hitting precision evaluation method based on error spectrum

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Embodiment Construction

[0088] In order to make the object, technical solution and advantages of the present invention clearer, the present invention 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 present invention, not to limit the present invention.

[0089] The invention discloses a method for evaluating the hit accuracy of an air-to-ground missile based on an error spectrum, which comprises the following steps:

[0090] S1. Preprocess the air-to-ground missile hit accuracy data to expand the sample size and convert it into a relative distance error;

[0091] S2. Determine the key metrics that can be used for the evaluation of the hit accuracy of the air-to-ground missile system;

[0092] S3. Constructing an air-to-ground missile hit accuracy attribute matrix;

[0093] S4. Establishing an air-to-ground missile hit accuracy attribute competiti...

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Abstract

The invention discloses an air-ground missile hit precision evaluation method based on an error spectrum, and the method comprises the following steps: S1, carrying out the preprocessing of the air-ground missile hit precision data, so as to expand the sample size, and enabling the data to be converted into a relative distance error; S2, determining a key measurement index which can be used for evaluating the hitting precision of the air-ground missile system; S3, constructing an air-ground missile hitting precision attribute matrix; s4, establishing an air-ground missile hitting precision attribute competition matrix according to the air-ground missile hitting precision attribute matrix; and S5, solving the feature vector of the air-ground missile hit precision attribute competition matrix, and giving an air-ground missile hit precision evaluation result corresponding to the element value according to the element value in the feature vector. According to the method, the evaluation index is steady, and in addition, the hitting precision of the air-ground missiles of the same type can be evaluated, and the hitting precision of the air-ground missiles of different types can also be evaluated.

Description

technical field [0001] The invention belongs to the field of system performance evaluation, in particular to an error spectrum-based air-to-ground missile hit accuracy evaluation method. Background technique [0002] The hit accuracy of the air-to-ground missile system directly reflects the statistical characteristics of the air-to-ground missile's impact point and target aiming point. Commonly used weapon accuracy indicators include Accuracy, Precision and Circular Error Probability (CEP). Accuracy refers to the degree of deviation of the center of the impact point relative to the target aiming point; density refers to the degree of dispersion of the impact point relative to the center of dispersion; CEP refers to the center of a circle with the center of the impact point as the center, and the impact point falls into the circle. When the probability is 50%, the radius of the circle is the value of CEP. [0003] In hit accuracy evaluation, traditional statistical methods ...

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Application Information

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IPC IPC(8): G06Q10/06
CPCG06Q10/06393
Inventor 彭维仕伍友利方洋旺李青
Owner AIR FORCE UNIV PLA
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