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A Rapid Analysis Method for Spacecraft Mass Characteristics

A quality characteristic, rapid analysis technology, applied in instruments, special data processing applications, electrical digital data processing, etc., can solve the problems of slow calculation speed, inaccurate numerical calculation, inconvenient information change, etc., to achieve slow and fast operation speed. Calculation, Quick Check Effect

Active Publication Date: 2015-10-21
BEIJING INST OF SPACECRAFT SYST ENG
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Problems solved by technology

[0003] The technical problem of the present invention is to overcome the shortcomings of the existing methods of the quality characteristic subsystem, provide a working method and method for collaborative analysis through multiple tools, and further solve the inconvenient change of information in the quality characteristic analysis process, inaccurate numerical calculation, and calculation problems. Slow speed and other problems, realize real-time update of quality characteristic information, fast acquisition of calculation results, scientific inspection of calculation results, etc.

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  • A Rapid Analysis Method for Spacecraft Mass Characteristics
  • A Rapid Analysis Method for Spacecraft Mass Characteristics
  • A Rapid Analysis Method for Spacecraft Mass Characteristics

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Embodiment Construction

[0026] The mass characteristic is a characteristic of the spacecraft itself, mainly including mass (weight), center of mass coordinates, moment of inertia, product of inertia, etc., and is an important input for the attitude and orbit control strategies of the spacecraft; , An important work content of the overall assembly design. Quality characteristic analysis has gone through stages such as actual measurement, manual calculation, simple software calculation, three-dimensional design analysis, etc., and the degree of automation of quality analysis has been continuously improved; the current method mainly has the problems of inconvenient inspection, inconvenient review, and inconvenient modification; the method of the present invention overcomes the problems of quality characteristic Insufficiency of the existing methods of the subsystem provides a working method and method of collaborative analysis through multiple tools, and then solves the problems of inconvenient informati...

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Abstract

A rapid spacecraft quality characteristic analysis method includes the steps: firstly, forming a quality information summary table according to equipment interface data sheet records of a spacecraft; using an interface tool for importing the quality information summary table into a spacecraft equipment model; secondly, using the interface tool for exporting position information and quality information of the equipment model to form an equipment model position and quality information summary table, and computing the position information and the quality information in the equipment model position and quality information summary table by the aid of a quality characteristic computational formula to obtain quality characteristic results of the spacecraft; and thirdly, using Pro / E software for quality characteristic analysis of the spacecraft, comparing analysis results with the quality characteristic results obtained in the second step, and if comparison difference is within a preset range, completing rapid quality characteristic analysis of the aircraft. The computing method overcomes shortcomings of an existing method of a quality characteristic analysis system, and achieves real-time update of quality characteristic information, rapid acquisition and scientific inspection of computational results and the like.

Description

technical field [0001] The invention relates to a method for quickly analyzing quality characteristics of a spacecraft, which is used for assisting configuration layout design and general assembly design of the spacecraft. Background technique [0002] The mass characteristic is a characteristic of the spacecraft itself, mainly including mass, center of mass coordinates, moment of inertia, product of inertia, etc., and is an important input for spacecraft attitude and orbit control strategies. In order to reduce the limitation of ground measurement and control capabilities, domestic spacecraft usually adopt optimized attitude and orbit control strategies, and put forward counter requirements on the quality characteristics of the entire satellite, and clarify that the quality characteristics do not exceed a given range. In view of the importance of quality characteristics, quality characteristic analysis has long been an important work content in spacecraft configuration layo...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F17/50
Inventor 周孝伦武向军丛飞嵇景全
Owner BEIJING INST OF SPACECRAFT SYST ENG