Air defense missile space killing area model construction and shooting data element calculation method based on small amount of actual data

An anti-aircraft missile, actual data technology, applied in CAD numerical modeling, design optimization/simulation, etc., can solve problems such as weak real-time performance, large data space, and insufficient actual data.

Active Publication Date: 2020-05-22
NAVAL UNIV OF ENG PLA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The method is cumbersome, the change of feature points is more complicated, and it is difficult to generate a smooth spatial kill zone by fitting a cluster of vertical kill zones, it takes up a lot of data space, and the real-time performance i

Method used

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  • Air defense missile space killing area model construction and shooting data element calculation method based on small amount of actual data
  • Air defense missile space killing area model construction and shooting data element calculation method based on small amount of actual data
  • Air defense missile space killing area model construction and shooting data element calculation method based on small amount of actual data

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Experimental program
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Effect test

Embodiment 1

[0128] see Figure 1 to Figure 7 , a method based on a small amount of actual data for the construction of the air defense missile space kill zone model and the calculation of the shooting elements, which mainly includes the following steps:

[0129] 1) Obtain anti-aircraft missile data.

[0130] The air defense missile data includes the kill zone height boundary H max , the lower limit of the kill zone H min , Kill Zone Far Boundary S sy , near border S of kill zone sj , the maximum elevation angle ε of the kill zone max , the maximum route angle q in the kill zone max , the maximum route shortcut P max , The time t when the anti-aircraft missile meets the target D实际 and the encounter point slope distance D s实际 .

[0131] 2) Establish a space kill zone model based on the air defense missile data.

[0132] The main steps to establish a space kill zone model are as follows:

[0133] 2.1) Based on the boundary parameters of the kill zone, an analytical geometric mathe...

Embodiment 2

[0265] A method for constructing an air defense missile space kill zone model and shooting elements based on a small amount of actual data. The main steps are as follows:

[0266] 1) Construction of the Matlab model of the space killing area: According to the analytical geometry mathematical model of the killing area, a small amount of public actual data is input, and polynomial fitting, linear fitting methods and curved polygon, plane polygon, and space polygon mapping matrix algorithms are used. The sequence of low near interface, high near interface, far interface, high low interface, positive and negative side interface, front positive and negative to bottom front positive and negative constructs a closed kill zone engineering model.

[0267] 2) Apply the lethal zone model to solve the shooting elements: apply the lethal zone model to solve the shooting elements, according to the actual data of time and slant distance, the space launch area is calculated from the space leth...

Embodiment 3

[0269] An experiment to verify the construction of the air defense missile space kill zone model based on a small amount of actual data and the calculation method of shooting elements, the main steps are as follows:

[0270] 1) Obtaining actual data: the actual data of the parameters of a certain type of anti-aircraft missile kill zone are shown in Table 1, and the actual data of time and slant distance are shown in Table 1. Figure 12 shown.

[0271] Table 1 The actual data table of the parameters of the kill zone of a certain type of air defense missile

[0272]

[0273] 2) Construction of kill zone and launch zone models for typical targets

[0274] A certain type of missile weapon system intercepts a horizontally flying anti-ship missile target with V≤300m / s, and the calculation results of the kill zone and launch zone are as follows: Figure 13 shown.

[0275] 2.1) Kill zone

[0276] a) Low near interface

[0277] The DGG′D′ equation of the low and near boundary o...

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Abstract

The invention discloses an air defense missile space killing area model construction and shooting data element calculation method based on a small amount of actual data. The method mainly comprises the steps of (1) acquiring air-defense missile data 2) based on the air defense missile data, establishing a space killing area model; and 3) resolving the space killing area model to obtain shooting data. According to the method, a killing area model is constructed by adopting a polynomial fitting method, a linear fitting method, a curved-edge polygon mapping matrix algorithm, a planar polygon mapping matrix algorithm and a spatial polygon mapping matrix algorithm according to the analytic geometry mathematical model of the killing area and a small amount of public actual data, and the defect of blindness and low efficiency of traditional spatial killing area construction is overcome.

Description

technical field [0001] The invention relates to the field of application of missile weapon systems, in particular to a method for building a space kill zone model of an air defense missile based on a small amount of actual data and solving the shooting elements. Background technique [0002] The killing zone (killing zone) refers to the space area where the air defense missile weapon system kills the specified air target at a given probability (the space range that kills a typical target with a given probability), and is an important aspect of the air defense missile weapon system. Combat comprehensive performance indicators. The spatial shape of the air defense missile weapon system kill zone is relatively complex, including indicators such as far boundary, near boundary, high boundary, low boundary, maximum route shortcut, maximum route angle, and maximum elevation angle. The general outline of the lethal area is mostly represented by data tables and graphs, most of which...

Claims

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Application Information

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IPC IPC(8): G06F30/20G06F111/10
Inventor 黄隽刘方彭英武邹强李晓宝肖金石薛冰
Owner NAVAL UNIV OF ENG PLA
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