Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

Method for simulating magnetism of space ship

A simulation method and spacecraft technology, applied in the direction of instruments, special data processing applications, electrical digital data processing, etc., can solve the problems that the estimation cannot meet the accuracy requirements and cannot be measured.

Active Publication Date: 2012-05-09
BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
View PDF2 Cites 4 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, sometimes, due to some reasons, the actual measurement cannot be carried out, especially at the beginning of the design, and the estimation cannot meet the accuracy requirements. Give a more accurate calculation or simulation of the magnetic properties of the spacecraft
In view of the fact that there is currently no feasible magnetic simulation method for spacecraft, the inventor finally developed a method that can simulate the magnetic properties of spacecraft with high precision and fast speed after many efforts

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Method for simulating magnetism of space ship
  • Method for simulating magnetism of space ship
  • Method for simulating magnetism of space ship

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0028] Hereinafter, the present invention will be further described through specific embodiments in conjunction with the accompanying drawings. The accompanying drawings are only for the purpose of illustration, and are not intended to limit the scope of protection of the present invention. The magnetic simulation method of spacecraft of the present invention comprises the following concrete steps:

[0029] 1) Obtain the initial magnetic test data of the spacecraft components

[0030] Set the components of the spacecraft part on the center of the magnetic test platform. There are three three-component fluxgate magnetometer probes arranged in a straight line at equal intervals outside the magnetic test platform. The magnetic test platform is rotated from 0-360° every 10° by Three three-component fluxgate magnetometer probes respectively acquire 36 sets of test data, each set includes 9 values, and the magnetic test data are recorded by the magnetic field data acquisition system...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention discloses a method for simulating magnetism. The method comprises the following steps of: acquiring initial magnetic test data of parts and components of a space ship; building a multi-dipole model of the parts and components of the space ship; establishing a magnetic test simulation system background database of the parts and components of the space ship; establishing a three-dimensional interactive system; and carrying out magnetism simulation of the space ship and other steps. In the method disclosed by the invention, the error introduced in the multi-dipole model is less than 5%, the time for establishing a model by using each group of data is 0-I minute, the operating rate of an improved algorithm is improved greatly, and thus, time requirement of modeling is met.

Description

technical field [0001] The invention belongs to the field of spacecraft magnetic simulation, and in particular relates to a simulation method of spacecraft magnetism, which can be directly applied to spacecraft magnetic simulation and magnetic test. Background technique [0002] For spacecraft in low and medium orbits, there is generally a requirement for magnetic control to eliminate the influence of magnetic interference torque during its service. For individual spacecraft that undertake magnetic measurement tasks or carry magnetically sensitive instruments, the requirements for magnetic control are often more stringent. At present, the commonly used method is to measure the magnetism of the units or parts that may have potential effects one by one, so as to evaluate the magnetic influence on the entire spacecraft or estimate the magnetic properties of the spacecraft based on the magnetic properties of the units or parts, and sometimes use the method of measuring the magne...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
Patent Type & Authority Applications(China)
IPC IPC(8): G06F17/50
Inventor 肖琦易忠马青永孟立飞史尧宜
Owner BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com