Eureka AIR delivers breakthrough ideas for toughest innovation challenges, trusted by R&D personnel around the world.

Method for acquiring aeronautic superconducting full tensor magnetic compensation coefficient, terminal and storage medium

An aeronautical superconductivity and compensation coefficient technology, which is applied in the field of aeromagnetic measurement and can solve the problem that the optimal solution of the full tensor magnetic compensation coefficient of aeronautical superconductivity cannot be obtained.

Active Publication Date: 2019-08-16
SHANGHAI INST OF MICROSYSTEM & INFORMATION TECH CHINESE ACAD OF SCI
View PDF7 Cites 11 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] In view of the shortcomings of the prior art described above, the purpose of the present invention is to provide a method for obtaining the full tensor magnetic compensation coefficient of aeronautical superconducting, a terminal and a storage medium, which are used to solve the problem that the existing method cannot obtain the full tensor of aeronautical superconducting The Problem of Optimal Solution of Magnetic Compensation Coefficient

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 acquiring aeronautic superconducting full tensor magnetic compensation coefficient, terminal and storage medium
  • Method for acquiring aeronautic superconducting full tensor magnetic compensation coefficient, terminal and storage medium
  • Method for acquiring aeronautic superconducting full tensor magnetic compensation coefficient, terminal and storage medium

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0055] Such as figure 1 As shown, this embodiment provides a method for obtaining the full tensor magnetic compensation coefficient of the aeronautical superconductor, and the method for obtaining includes:

[0056] Obtaining the approximate value of the magnetic compensation coefficient of the planar gradiometer with respect to eddy current interference based on the dynamic measurement data, and obtaining the value constraint range of the magnetic compensation coefficient of the planar gradiometer with respect to eddy current interference;

[0057] When the aircraft carries the aeronautical superconducting full tensor magnetic gradient measurement system placed in it for high-altitude maneuvering flight, obtain the magnetic gradient measurement value and the three-axis magnetic field component output by the aeronautical superconducting full tensor magnetic gradient measurement system Measurements;

[0058] Taking the value constraint range of the magnetic compensation coeffi...

Embodiment 2

[0086] Such as figure 2 As shown, this embodiment provides a method for obtaining the full tensor magnetic compensation coefficient of the aeronautical superconductor, and the method for obtaining includes:

[0087] Obtaining the approximate value of the magnetic compensation coefficient of the planar gradiometer with respect to eddy current interference based on the dynamic measurement data, and obtaining the value constraint range of the magnetic compensation coefficient of the planar gradiometer with respect to eddy current interference;

[0088] Obtain the approximate value of the magnetic compensation coefficient of the plane gradiometer on the unbalance degree / induced magnetic field interference in the aeronautical superconducting full tensor magnetic gradient measurement system based on the static measurement data, and obtain the unbalance degree / induced magnetic field interference of the plane gradiometer based on this The value constraint range of the magnetic compen...

Embodiment 3

[0108] Such as image 3 As shown, this embodiment provides a terminal, the terminal includes: a memory 100 and a processor 200, the memory 100 is used to store computer programs, and the processor 200 is used to execute the computer programs stored in the memory 100 so that the terminal executes the method for acquiring the full tensor magnetic compensation coefficient of the aeronautical superconductor as described in the first embodiment.

[0109] The memory 100 may include but not limited to high-speed random access memory, non-volatile memory, such as one or more magnetic disk storage devices, flash memory devices or other non-volatile solid-state storage devices. The processor 200 may be a general-purpose processor, including one or more central processing units (Central Processing Unit, referred to as CPU), a network processor (Network Processor, referred to as NP), etc.; it may also be a digital signal processor (Digital Signal Processing , referred to as DSP), applica...

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 present invention provides a method for acquiring an aeronautic superconducting full tensor magnetic compensation coefficient, a terminal and a storage medium. The method comprises the following steps: an approximate value of a magnetic compensation coefficient of a plane gradiometer with respect to eddy current interference is acquired based on dynamic measured data, and a constraint range ofthe magnetic compensation coefficient of the plane gradiometer with respect to the eddy current interference is acquired based on the approximate value of the magnetic compensation coefficient; whenan aircraft carries a built-in aeronautic superconducting full tensor magnetic gradient measuring system for high altitude maneuvering flight, measured values of a magnetic gradient and a triaxial magnetic-field component output by the aeronautic superconducting full tensor magnetic gradient measuring system are acquired; the constraint range of the magnetic compensation coefficient of the plane gradiometer with respect to the eddy current interference is taken as a constraint condition, and the measured values of the magnetic gradient and the triaxial magnetic-field component are substitutedinto a magnetic compensation model with the constraint condition, thereby an optimal value of the aeronautic superconducting full tensor magnetic compensation coefficient is acquired. The invention solves the problem that an existing method cannot acquire the optimal solution of the aeronautic superconducting full tensor magnetic compensation coefficient.

Description

technical field [0001] The invention belongs to the field of aeromagnetic measurement, and in particular relates to an acquisition method, a terminal and a storage medium of an aeronautical superconducting full tensor magnetic compensation coefficient. Background technique [0002] The full tensor magnetic gradient describes the change rate information of the magnetic field vector in three-dimensional space, that is, the gradient of the three components of the magnetic field vector in three directions in space. The measurement results of the full tensor magnetic gradient have the advantages of being less affected by the magnetization direction, can reflect the vector magnetic moment information of the target body, and can better invert the field source parameters (orientation, magnetic moment, etc.), so it can be used for the field source Carry out positioning and tracking, and improve the resolution of the magnetic source body. The measurement and interpretation applicatio...

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): G01R33/025G01R33/035
CPCG01R33/025G01R33/0354
Inventor 伍俊荣亮亮邱隆清代海宾张国锋张树林裴易峰李宝清谢晓明
Owner SHANGHAI INST OF MICROSYSTEM & INFORMATION TECH CHINESE ACAD OF SCI
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
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