Moving target atmospheric disturbance characteristic simulation method

A technology of atmospheric disturbance and simulation method, applied in design optimization/simulation, image data processing, 3D modeling, etc., to improve the accuracy of simulation analysis

Active Publication Date: 2020-05-08
BEIJING RES INST OF SPATIAL MECHANICAL & ELECTRICAL TECH
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Problems solved by technology

Therefore, the use of wind tunnel tests to study the characteristics of atmospheric disturbances of high-speed moving targets in the atmosphere has many limitations.

Method used

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  • Moving target atmospheric disturbance characteristic simulation method
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  • Moving target atmospheric disturbance characteristic simulation method

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Embodiment Construction

[0047] The working principle of a moving target atmospheric disturbance characteristic simulation method of the present invention is as follows: figure 1 As shown, including obtaining the target geometric parameters, establishing the target 3D model, meshing the target and flow field solution area, setting the flow field calculation conditions, selecting the flow field calculation model, obtaining the target atmospheric disturbance flow field parameters, and calculating the flow field refraction Calculate the refractive index gradient according to the Barron operator, use Runge-Kutta ray tracing to calculate the deflection transmission path of the disturbed atmosphere, and obtain the deflection angle of the light passing through the disturbance field. The present invention can provide a new method other than the wind tunnel for acquiring the atmospheric disturbance characteristics of the high-speed moving target, can be applied to the optimization of the aerodynamic shape of th...

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Abstract

The invention discloses a moving target atmospheric disturbance characteristic simulation method. The method includes obtaining target geometry parameters, establishing target three-dimensional model,dividing grids of a target and flow field solving area; setting flow field calculation conditions, selecting a flow field calculation model, obtaining target atmospheric disturbance flow field parameters, calculating flow field refractive index distribution, calculating a refractive index gradient according to a Barron operator, calculating a disturbance atmospheric deflection transmission path through Runge-Kutta light tracing, and obtaining a deflection angle of light passing through a disturbance field. According to the method, simulation analysis is carried out on light deflection generated when ground object light passes through an atmospheric disturbance area formed by a high-speed target for the first time. The method can be used for atmospheric disturbance simulation analysis of any target flying in the atmospheric layer, can analyze the deflection condition of the ground object light of any spectral band passing through the target atmospheric disturbance area, and can also analyze the deflection condition formed by the ground object light of different spectral bands passing through the atmospheric disturbance area of the target at different incident angles. A new means isprovided for target atmospheric disturbance simulation analysis, and the method can be applied to atmospheric disturbance field characteristic research.

Description

technical field [0001] The invention relates to a method for simulating the atmospheric disturbance characteristics of a moving target, which is a new method for simulating the atmospheric disturbance characteristics caused by the high-speed movement of the target in the atmosphere. The deflection of light can provide design input for the visual observation of atmospheric disturbances by optical means, and provide a new technical means for the study of atmospheric disturbance characteristics, which can be applied to the optimization of aerodynamic shape of high-speed moving targets, low resolution and wide Detection, etc., can be applied to the background of ground objects, breaking through the limitation that the aerodynamic characteristics must be obtained in the wind tunnel, and greatly reducing the difficulty and cost of obtaining aerodynamic characteristics. Background technique [0002] The high-speed flight of a high-speed moving target in the atmosphere will inevitab...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F30/20G06T17/00
CPCG06T17/00Y02T90/00
Inventor 张月董士奎高鹏张学敏邓红艳赵号张琢苏云郑国宪
Owner BEIJING RES INST OF SPATIAL MECHANICAL & ELECTRICAL TECH
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