Characteristic relay method for relative position and attitude based on multi-vision

A relative position and multi-eye vision technology, applied in the direction of integrated navigator, etc., can solve the problem that the attitude calculation technology has not been reported yet, and achieve the effect of simple and effective calculation method, wide application range and wide application range

Active Publication Date: 2015-03-25
SHANGHAI XINYUE METER FACTORY
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Problems solved by technology

Only relying on the multi-eye vision system to complete the relative position and attitude calculation technology of generalized non-cooperative targets with unknown models has not been reported yet

Method used

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  • Characteristic relay method for relative position and attitude based on multi-vision
  • Characteristic relay method for relative position and attitude based on multi-vision
  • Characteristic relay method for relative position and attitude based on multi-vision

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Embodiment Construction

[0020] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several modifications and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0021] The present invention is based on the feature relay method of the relative position of multi-eye vision and attitude and comprises the following steps:

[0022] Step 1, through three-dimensional reconstruction of stereo vision, calculate the position coordinates of the observed and extracted target feature points in the tracking spacecraft coordinate system, and complete the relative position calculation; wherein, in step 1, the tracking spacecraft binocular vision system The image shooting...

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Abstract

The invention provides a characteristic relay method for relative position and attitude based on multi-vision. The method comprises the following steps: step 1. calculating position coordinates of the observed and extracted target characteristic points under a tracking spacecraft coordinate system by virtue of stereoscopic vision three-dimensional reconstruction to finish relative position calculation; step 2. establishing a coordinate system at each moment by virtue of any three points in the observed four characteristic points, and calculating an attitude matrix of every two coordinate systems; and step 3. calculating the attitude of the target body coordinate system at the current moment relative to the tracking spacecraft coordinate system, namely finishing the relative attitude relay calculation of a non-cooperative target. According to the method disclosed by the invention, the calculation of the relative position and attitude of non-cooperative targets such as spacecraft and space debris can be finished.

Description

technical field [0001] The invention relates to a relay method, in particular to a characteristic relay method based on relative position and attitude of multi-eye vision. Background technique [0002] With the development of aerospace technology, especially manned space technology and space stations, space rendezvous and docking technology has become an important field for the development of major aerospace countries. Prerequisites and Important Guarantees. The unmanned autonomous rendezvous and docking technology between spacecraft with the application background of non-cooperative target rendezvous plays a vital role in space missions such as cleaning up space debris, repairing faulty satellites, deep space exploration and asteroid landing. An important prerequisite for completing these tasks is to determine the relative position and attitude of the tracking spacecraft and the non-cooperative target with high precision. [0003] Visual measurement technology uses images...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01C21/24
CPCG01C21/24
Inventor 谭天乐吴猛谭龙玉朱东方王卫华耿淼宋婷
Owner SHANGHAI XINYUE METER FACTORY
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