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Total dose reinforcement resistant optimization calculation method and system applied to high-orbit satellite

An anti-total dose, optimization calculation technology, applied in design optimization/simulation, special data processing applications, geometric CAD, etc., to achieve significant practical significance and engineering value, and reduce development costs

Pending Publication Date: 2022-05-17
SHANGHAI SATELLITE ENG INST
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Problems solved by technology

[0006] The utility model patent with the publication number CN202337364U discloses a communication satellite ionization total dose protection device, including tantalum foil, thermal control multi-layers and steel screws; the tantalum foil is installed on the communication satellite’s large opening through steel screws On the structural plate, the heat-controlled multi-layer is fixed on the steel screw through the pressing sheet, but this invention is only for the large-sized opening of the satellite structural plate, and it is only one aspect of the anti-radiation design of the satellite

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  • Total dose reinforcement resistant optimization calculation method and system applied to high-orbit satellite
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  • Total dose reinforcement resistant optimization calculation method and system applied to high-orbit satellite

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[0058] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several changes and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0059] An embodiment of the present invention provides an anti-total dose hardening optimization calculation method applied to high-orbit satellites, the method including: satellite total dose refinement simulation, component parameter cost modeling, and satellite anti-total dose hardening optimization calculation. The invention solves the problems of insufficient anti-total dose design margin and high component selection cost of high-orbit satellites in the harsh radiation environment at the present sta...

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Abstract

The invention provides an anti-total dose reinforcement optimization calculation method and system applied to a high-orbit satellite, relates to the technical field of satellite anti-radiation design, and aims to construct an efficiency-cost ratio optimization model for satellite anti-total dose reinforcement for a high-efficiency cost ratio. According to the model, an anti-total dose design margin (RDM) is used as an evaluation index, quality grades and anti-total dose capabilities of different types of satellite components are used as core parameters, and a parameter model of anti-total dose reinforcement cost, component grades and shielding quality is established. Then, the cost-effectiveness ratio serves as a target function, a gradient-based optimization method is adopted, optimization design is conducted on satellite total dose reinforcement resistance, and uncertainty in the optimization process is analyzed and discussed. The method is high in operability and realizability, the on-orbit reliability of a satellite system can be improved on the premise that the requirements for the service life of the satellite and the total dose reinforcement resistance are met, and the development cost is effectively reduced.

Description

technical field [0001] The invention relates to the technical field of satellite anti-radiation design, in particular to an anti-total dose reinforcement optimization calculation method and system applied to high-orbit satellites. Background technique [0002] The new generation of scientific satellites, including Jupiter detection, faint target detection satellites, and high-resolution photoelectric detection satellites, are all moving towards high-resolution, high-sensitivity, hyperspectral, all-weather, and all-time. space area. However, there are a large number of high-energy protons, electrons, cosmic rays, and auroral radiation in outer space, which can easily cause radiation damage to high-precision, high-resolution, and high-sensitivity detection payloads and components, and affect satellite detection tasks. [0003] The design of satellite anti-total dose reinforcement is one of the key directions of space protection design. The previous design work relied too much...

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Application Information

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IPC IPC(8): G06F30/15G06F30/20
CPCG06F30/15G06F30/20
Inventor 束山山李庆韦锡峰李强贾奥男廖明何海燕
Owner SHANGHAI SATELLITE ENG INST
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