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Different-orbit-altitude background radiation dynamic simulation method and device

A technology of background radiation and orbit height, which is applied in the field of radiation simulation, can solve the problems of not considering the distance and angle relationship between the target and the radiation block, and the background radiation simulator does not consider the influence of flight height, so as to achieve the effect of improving the simulation accuracy

Active Publication Date: 2019-04-02
BEIJING AEROSPACE INST OF THE LONG MARCH VEHICLE
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  • Application Information

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Problems solved by technology

[0002] In the existing space environment simulation experiments, the background radiation simulator does not consider the influence of the flight height on the radiation heat flow, that is, the distance and angle relationship between the target and the radiation block are not considered in the radiation heat flow simulation process

Method used

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  • Different-orbit-altitude background radiation dynamic simulation method and device
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  • Different-orbit-altitude background radiation dynamic simulation method and device

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Embodiment Construction

[0056] The characteristics and exemplary embodiments of various aspects of the present invention will be described in detail below. In order to make the purpose, technical solutions and advantages of the present invention more clear, 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 configured to explain the present invention, not to limit the present invention. It will be apparent to one skilled in the art that the present invention may be practiced without some of these specific details. The following description of the embodiments is only to provide a better understanding of the present invention by showing examples of the present invention.

[0057] It should be noted that in this article, relational terms such as first and second are only used to distinguish one entity or operation from another entity or operation, and ...

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Abstract

The invention relates to a different-orbit-altitude background radiation dynamic simulation method and device, a computer storage medium and a background radiation simulator. The method includes the steps that according to the orbit altitude of a to-be-simulated spacecraft and the distance between a spacecraft model and the radiating surface of the background radiation simulator in a simulation system, the effective radiation radius of the radiating surface of the background radiation simulator is calculated; the background radiation simulator comprises multiple arc-shaped radiation blocks, circular areas with different radii are formed by the radiation blocks firstly, all the circular areas with the different radii are concentrically arranged to form the whole radiating surface of the background radiation simulator; and according to the calculated effective radiation radius, the temperatures of the radiation blocks with the radii not larger than the effective radiation radius in the background radiation simulator are controlled to be increased to a first target range value, and the temperatures of the radiation blocks with the radii larger than the effective radiation radius in the background radiation simulator are controlled to be reduced to a second target range value. Through control over temperature increase or reduction of the radiation blocks in the different radius positions of the background radiation simulator, radiation heat flows at different orbit altitudes can be simulated.

Description

technical field [0001] The invention relates to a radiation simulation method, in particular to a background radiation dynamic simulation method, device, computer storage medium and background radiation simulator at different orbit heights. Background technique [0002] In the existing space environment simulation experiments, the background radiation simulator does not consider the influence of flight height on the radiation heat flow, that is, the distance and angle relationship between the target and the radiation block are not considered in the radiation heat flow simulation process. [0003] Therefore, how to effectively simulate the radiation heat flow at different orbit heights in the space environment simulation test system is an urgent problem to be solved. Contents of the invention [0004] The purpose of the present invention is to solve at least part of the technical problems in the prior art. It provides a dynamic simulation method, device, computer storage me...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G7/00
Inventor 孟刚南华李亚男薛莲周岩邓蓉范小礼水涌涛刘鑫陈福泰
Owner BEIJING AEROSPACE INST OF THE LONG MARCH VEHICLE
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