Estimation method for position and attitude of cooperative target

A technology of cooperative goals and attitudes, which can be applied to measurement devices, electromagnetic wave re-radiation, and utilization of re-radiation.

Inactive Publication Date: 2019-12-03
SHANGHAI AEROSPACE CONTROL TECH INST
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Problems solved by technology

[0003] The distance measurement of space cooperation targets has the characteristics of large scale changes and drastic changes in the space environment, especially the impact of illumination changes on measurement is very obvious, which brings great challenges to the distance measurement of space cooperation targets
The traditional measurement method uses a visible light camera to obtain the target's relative position and attitude estimation accuracy is limited by the noise interference of the space environment, which will lead to measurement error amplification and poor robustness

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  • Estimation method for position and attitude of cooperative target
  • Estimation method for position and attitude of cooperative target
  • Estimation method for position and attitude of cooperative target

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Embodiment Construction

[0060] The present invention will be further elaborated below by describing a preferred specific embodiment in detail in conjunction with the accompanying drawings.

[0061] Such as figure 1 As shown, the present invention provides a method for estimating the position and attitude of a cooperative target, comprising the following steps:

[0062] S1. Extract the key feature points of the marked area of ​​the cooperative target from the intensity map and depth map collected by the lidar;

[0063] S2. Use deterministic annealing to match the key feature points of the mathematical model of the cooperation target marked area with the key feature points of the observation model;

[0064] S3. Using the key feature point matching information, calculate the rotation matrix and translation vector in the position and attitude calculation formula based on the singular value decomposition algorithm, and obtain the relative position and attitude information of the cooperation target.

[0...

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Abstract

The invention discloses an estimation method for a position and attitude of a cooperative target. The method comprises the following steps of extracting key feature points of a cooperative target marking area from an intensity map and a depth map collected by a laser radar; implementing matching between key feature points of a mathematic model and key feature points of an observation model in thecooperative target marking area by use of deterministic annealing; and solving a rotation matrix and a translation vector in a position and attitude solution formula based on a singular value decomposition algorithm by use of the matching information of the key feature points to obtain the relative position and attitude information of the cooperative target. According to the estimation method forthe position and attitude of the cooperative target disclosed by the invention, the influence of ambient light on the estimation result can be effectively reduced in a laser radar measurement manner;the intensity and the relative distance information of each pixel are provided by the image collected by the laser radar; the measurement robustness and real-time are enhanced, and meanwhile the calculation amount is small in the process of solving of the position and attitude information of the cooperative target.

Description

technical field [0001] The invention relates to the technical field of determining the relative position and attitude of a cooperative target of a spacecraft, in particular to a method for estimating the position and attitude of a cooperative target based on laser radar. Background technique [0002] With the increase of human space activities, the number of space operation missions is increasing year by year. Space operation missions usually involve two space vehicles, which are respectively called the target vehicle and the tracking vehicle. When carrying out control tasks such as spacecraft on-orbit service, it is necessary to accurately measure the position and attitude information of the cooperation target. The cooperation target refers to the space vehicle that can provide effective cooperation information, such as installing an artificially designed target in advance. In order to successfully perform space operation tasks, it is necessary to accurately obtain informat...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01S17/50G01S17/88
CPCG01S17/50G01S17/88
Inventor 牟金震方亚毜刘宗明李桂存温凯瑞
Owner SHANGHAI AEROSPACE CONTROL TECH INST
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