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Operational capability estimation method for air-defense anti-missile system

A combat capability and system technology, applied in the direction of instruments, data processing applications, resources, etc., to achieve reliable evaluation, reasonable expert experience, and overcome the effects of subjective defects

Inactive Publication Date: 2018-10-02
BEIHANG UNIV
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Problems solved by technology

The entropy weight method only determines the weight based on the index data, which often contradicts the actual situation

Method used

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  • Operational capability estimation method for air-defense anti-missile system
  • Operational capability estimation method for air-defense anti-missile system
  • Operational capability estimation method for air-defense anti-missile system

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specific example

[0117] A specific example of the above-mentioned preferred processing flow is as follows:

[0118] First of all, according to the combat tasks and related combat activities of the air defense and anti-missile system, 16 relevant evaluation indicators are selected from four aspects: reconnaissance and early warning, command and control, interception and strike, and comprehensive support, including target detection probability, target recognition probability, target tracking probability, early warning Time, information transmission delay, information transmission speed, information fusion capability, threat assessment capability, command decision-making time, total target penetration, total target interception, total target damage, maneuver speed, battle damage probability, repair speed, support speed.

[0119] Secondly, establish the combat capability evaluation model of the air defense and anti-missile system, obtain three groups of index data of the air defense and anti-missil...

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Abstract

The invention provides an operational capability estimation method for an air-defense anti-missile system, and the method comprises the steps: decomposing an operational activity based on an operational mission, and extracting corresponding evaluation indexes; establishing an operational capability evaluation model based on the evaluation indexes, obtaining quantitative index data of the to-be-evaluated anti-aircraft anti-missile system based on the operational capability evaluation model, and constructing a corresponding capability requirement satisfaction degree evaluation matrix; estimatingthe comprehensive operational capability of the to-be-evaluated anti-aircraft anti-missile system through employing weighted aggregation operation based on the comprehensive weight of each of the evaluation indexes and the capability requirement satisfaction degree evaluation matrix corresponding to the quantitative index data. The method can effectively reduce the subjectivity of an evaluation process through building the complete, reliable and feasible air-defense anti-missile system while making the better use of the experience of an expert group, and improves the effectiveness and the reliability of an evaluation result.

Description

technical field [0001] The invention relates to the technical field of weapon equipment system construction, and more specifically, to a method for evaluating the combat capability of an air defense and anti-missile system. Background technique [0002] With the continuous development of military technology in various countries, the equipment for air strike operations tends to be diversified, and the combat environment also tends to be complicated. In order to cope with the complex combat environment, it is necessary to speed up the construction of the air defense and anti-missile system and improve the comprehensive combat capability of the system. The assessment of the combat capability of the system can promptly and effectively discover the weak links in the system and equipment, thereby providing scientific decision-making for the development and planning of the system and equipment. Therefore, the air defense and anti-missile system needs a complete and feasible combat...

Claims

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Application Information

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IPC IPC(8): G06Q10/06
CPCG06Q10/06393
Inventor 师鹏刘泽宇王逍赵育善
Owner BEIHANG UNIV
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