Task and risk oriented health degree evaluation method for typical functional structure level of satellite

A technology for functional structure and health

Active Publication Date: 2020-08-18
BEIHANG UNIV
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

When calculating the satellite multi-level system health, this method sets the reconfigurability artificially to 0 and 1, which weakens the physical meaning of various system structures, and only studies the system with one reconfigurability. The method itself has certain limitations

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  • Task and risk oriented health degree evaluation method for typical functional structure level of satellite
  • Task and risk oriented health degree evaluation method for typical functional structure level of satellite
  • Task and risk oriented health degree evaluation method for typical functional structure level of satellite

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Embodiment Construction

[0062] The embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings. It should be understood that the embodiments described below are only used to illustrate and explain the present invention, and are not intended to limit the present invention.

[0063] figure 1 is a schematic diagram of the first flow chart of a task- and risk-oriented satellite typical functional structure level health evaluation method provided by an embodiment of the present invention, as shown in figure 1 As shown, the steps include:

[0064] Step S101: Determine each task that the satellite needs to perform.

[0065] Step S102: Determine a satellite-level functional structural block diagram when the satellite performs each task, and the satellite-level functional structural block diagram includes a plurality of subsystems.

[0066] Step S103: Using the satellite-level functional structure diagram when the satellite performs each task, evaluat...

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Abstract

The invention discloses a task and risk oriented health degree evaluation method for a typical functional structure level of a satellite. The method comprises the following steps: determining each task needing to be executed by the satellite; determining a functional structure block diagram of a satellite level when the satellite executes each task, wherein the functional structure block diagram of the satellite level comprises a plurality of subsystems; evaluating the task health degree and the risk health degree of the satellite level of each task by utilizing the functional structure blockdiagram of the satellite level when the satellite executes each task; weighting and accumulating the task health degree of the satellite level of each task to obtain a satellite task health degree, and weighting and accumulating the risk health degree of the satellite level of each task to obtain a satellite risk health degree; and comprehensively evaluating the health state of the satellite according to the satellite task health degree and the satellite risk health degree.

Description

technical field [0001] The invention relates to the field of satellites, in particular to a task- and risk-oriented health degree evaluation method for typical functional structures of satellites. Background technique [0002] Satellites have the characteristics of long in-orbit running time, arduous tasks, and unknown working environment. At the same time, with the increase in the number of satellites and the upgrading of satellite systems in recent years, the structure and functions of stars have become increasingly complex and diverse, and the integration is high, resulting in complex failure modes. Changeable, the failure rate of single machine, system and other components will also increase. Therefore, the existing satellite monitoring system can no longer meet the high reliability mission realization requirements of current satellites. At the same time, traditional satellite status monitoring and health calculations focus on the task completion capabilities of a singl...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F30/20G06F119/02
CPCG06F30/20G06F2119/02
Inventor 吕琛许庶陶来发王自力
Owner BEIHANG UNIV
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