Unlock instant, AI-driven research and patent intelligence for your innovation.

Non-cooperative spacecraft relative pose measurement method based on multi-source information fusion

A multi-source information fusion, relative pose technology, applied in measuring devices, radio wave measuring systems, instruments, etc., can solve the problems of insufficient precision, inaccurate sensors, and fast acquisition of relative pose information of non-cooperative spacecraft, to achieve The effect of overcoming the lack of measurement accuracy

Pending Publication Date: 2022-03-01
BEIHANG UNIV
View PDF2 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] In order to solve the problem that a single sensor cannot accurately and quickly obtain the relative pose information of non-cooperative spacecraft due to the influence of the environment and the characteristics of the sensor itself, the present invention is based on the two most commonly used sensors for space navigation: binocular camera and laser radar , to provide a non-cooperative spacecraft relative pose measurement method based on multi-source information fusion, to overcome the shortcomings of relying on a single sensor to measure the relative pose of non-cooperative spacecraft, and to establish a binocular camera and lidar data fusion structure to measure non-cooperative The relative pose of the cooperative spacecraft ensures the measurement accuracy of the relative pose of the non-cooperative spacecraft

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
  • Non-cooperative spacecraft relative pose measurement method based on multi-source information fusion
  • Non-cooperative spacecraft relative pose measurement method based on multi-source information fusion
  • Non-cooperative spacecraft relative pose measurement method based on multi-source information fusion

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0046] The present invention will be further described below in conjunction with the accompanying drawings.

[0047] Such as figure 1 As shown, the sensor data fusion structure design of the present invention is aimed at the structural characteristics of non-cooperative spacecraft, and comprehensively considers the data characteristics of binocular cameras and lidar sensors, and extracts the line features of non-cooperative spacecraft in binocular images for low-precision The relative attitude of the target is calculated, and then the point features of the non-cooperative spacecraft in the binocular image are extracted, and its depth information is restored. Combined with the radar point cloud data, the low-precision relative position of the target is obtained, and finally the non-cooperative space vehicle will be obtained The relative pose of the spacecraft is used as the initial value, and the radar point cloud data is used for iterative calculation to further improve the me...

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 relates to a non-cooperative spacecraft relative pose measurement method based on multi-source information fusion, and the method comprises the steps: firstly, designing a non-cooperative spacecraft model, and constructing a simulation model of a binocular camera and a laser radar; then, considering that the binocular camera can acquire all information of the non-cooperative spacecraft but the accuracy of the recovered depth information is influenced by configuration calibration of the binocular camera, and the laser radar imaging can directly acquire the accurate depth information of the non-cooperative spacecraft but the laser radar imaging point clouds are sparse, and combining the advantages of the two types of sensors; designing a sensor data fusion structure to measure the relative pose of the non-cooperative spacecraft; and finally, based on the measured target relative pose, performing iterative operation by using laser radar data to improve the measurement precision of the relative pose of the non-cooperative spacecraft. According to the invention, the high-precision identification of the relative pose information of the non-cooperative spacecraft is realized through the measurement of the relative pose of the non-cooperative spacecraft based on the binocular camera and the laser radar data fusion.

Description

technical field [0001] The invention belongs to the field of navigation design of non-cooperative spacecraft, and relates to a method for measuring the relative pose of non-cooperative spacecraft based on multi-source information fusion. Background technique [0002] At present, the mission requirements of spacecraft tend to be diverse and complex, including various space operations, such as close-range operations such as on-orbit refueling, on-orbit maintenance and assembly, and on-orbit module replacement; there are a lot of space junk in space , there is a risk of collision between spacecraft running in space, and the cleaning of space junk can ensure the safety of the spacecraft; spacecraft rendezvous and docking requires accurate knowledge of the relative position and orientation information of the main and auxiliary spacecraft; and so on. With the rapid development of space technology and the increasing strategic position of space, the research on the space mission of ...

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
IPC IPC(8): G01S17/86G01S7/48G01C11/04
CPCG01S17/86G01S7/4802G01C11/04
Inventor 胡庆雷郭鹏宇邵小东郑建英郭雷
Owner BEIHANG UNIV