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Allocation Method of Combat Aircraft System Vulnerability Index

A combat aircraft and indicator distribution technology, applied in special data processing applications, instruments, electrical digital data processing, etc., can solve the problems of not considering the intermediate state of the aircraft, affecting the performance of the aircraft and the efficiency of completing tasks, etc.

Active Publication Date: 2017-10-13
NORTHWESTERN POLYTECHNICAL UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Northwestern Polytechnical University proposed a method for sorting the vulnerability of aircraft components in the invention with the application number 201410352457.9. This method provides five kinds of vulnerability ranking methods, which are respectively structural probability importance, key importance ( Criticality), FV importance, RAW importance and RRW importance, but these five methods are only suitable for two-state systems, that is, when the aircraft is hit, the aircraft has a killing state and a non-killing state, without considering the intermediate state of the aircraft. intermediate states do not result in aircraft kills, but affect aircraft performance and mission efficiency

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  • Allocation Method of Combat Aircraft System Vulnerability Index
  • Allocation Method of Combat Aircraft System Vulnerability Index
  • Allocation Method of Combat Aircraft System Vulnerability Index

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Embodiment Construction

[0055] This embodiment takes a certain type of fighter jet as an example to illustrate the method of quantitative calculation of vulnerability and index distribution of components of a complex multi-state system based on comprehensive importance and Griffith importance proposed by the present invention.

[0056] Step 1: Establish aircraft vulnerability model.

[0057] For an existing fighter model, determine those parts that will cause the aircraft to be killed after damage or loss, that is, lethal parts. The simplified aircraft model in this embodiment is as attached image 3 As shown, the fatal components of the model determined by the definition of fatal components are pilot B, tail fuel tank C, left engine D, right engine F, left hydraulic oil tank G, right hydraulic oil tank H, left generator I and right power generator Machine J. Pilot B, tail fuel tank C, left engine D and right engine F are non-redundant components. The aircraft vulnerability model has two redundanc...

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Abstract

A method for assigning vulnerability indicators of a combat aircraft system. By establishing a vulnerability model of a certain type of fighter, under certain threat strikes, determine the initial parameters of vulnerability, and then determine the number of times the aircraft has been hit and the number of times each component has been hit. Then determine the independent state of the aircraft and the probability of each state being hit, and substitute the above data into the calculation formula of the comprehensive importance and Griffith importance to obtain the comprehensive importance and Griffith importance of each component. Finally, the fragility of the whole machine is allocated by using the fragility index allocation method, and the fragility of each component can be obtained. After obtaining the fragility assigned to each component, the fragility reduction is performed on the components with high fragility to reduce its fragility, thereby improving the survivability of the aircraft.

Description

technical field [0001] The invention relates to the field of vulnerability reduction design of aviation combat aircraft, and specifically allocates vulnerability indexes of aircraft systems based on comprehensive importance and Griffith importance theory. Background technique [0002] Vulnerability is defined as the ability of a combat aircraft to withstand the threat of man-made hostile environments in a combat state. Given the vulnerability of aircraft components is an important task in survivability assessment, it should be considered in the early stage of aircraft design. It provides guidelines for effectively improving aircraft survivability, and puts the main design tasks on highly vulnerable components in a targeted manner, so as to achieve efficient and optimal design of aircraft survivability. [0003] The higher the vulnerability of the aircraft, the easier it is to be killed when it is hit, and the more it will reduce the ability of the aircraft to complete the t...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F19/00
Inventor 裴扬赵倩田晨谢芳敏宋笔锋
Owner NORTHWESTERN POLYTECHNICAL UNIV
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