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Ground object coordinate information-based rapid target positioning method, device, satellite-mounted device and storage medium

A technology of ground object coordinates and satellites, which is applied to satellite radio beacon positioning systems, measurement devices, instruments, etc., can solve the problems that the satellite attitude determination method cannot meet the accuracy, affects the satellite positioning accuracy, and the attitude determination accuracy declines, etc. Carrying capacity, solving the effect of decreasing accuracy and improving accuracy

Active Publication Date: 2018-05-18
HARBIN INST OF TECH
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Problems solved by technology

When the satellite locates the target through the attitude of the satellite, due to the interference of thermal deformation and other interference in the space environment during the orbital movement of the satellite, the original satellite attitude determination method cannot meet the accuracy requirements
In addition, because the satellite attitude determination system may have deviations and failures, it will also lead to a decrease in the accuracy of attitude determination, which in turn affects the accuracy of satellite positioning

Method used

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  • Ground object coordinate information-based rapid target positioning method, device, satellite-mounted device and storage medium
  • Ground object coordinate information-based rapid target positioning method, device, satellite-mounted device and storage medium
  • Ground object coordinate information-based rapid target positioning method, device, satellite-mounted device and storage medium

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Embodiment Construction

[0053] The attitude of the satellite refers to the attitude of the satellite body relative to the reference object on which the satellite operates. The positioning of the target point by the satellite needs to be obtained from the attitude of the satellite and the relative position between the satellite and the target point. Therefore, accurately obtaining the attitude information of the satellite is the key to the accurate positioning of the satellite.

[0054] In the embodiment of the present invention, the position information of the reference point is acquired through the imaging payload carried by the satellite, and relatively accurate attitude information can be obtained, which can be used to determine the attitude deviation of the satellite. Then, the satellite attitude information obtained through the satellite attitude system is compensated by the obtained attitude deviation, and the target point can be accurately located by using the compensated satellite attitude inf...

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Abstract

The invention discloses a ground object coordinate information-based rapid target positioning method. The method includes the following steps that: the attitude deviation quantity of a satellite is determined according to the position information of a reference point and the orbit information of the satellite; deviation compensation is performed on the attitude information of the satellite based on the attitude deviation quantity; and the position information of a target point is determined according to the compensated attitude information. The present invention also discloses a ground objectcoordinate information-based rapid target positioning device, a satellite-mounted device and a storage medium.

Description

technical field [0001] The invention relates to satellite imaging positioning technology in the field of satellite positioning, in particular to a method, device, satellite carrying equipment and storage medium for fast target positioning based on ground object coordinate information. Background technique [0002] With the development of aerospace technology, the positioning of ground targets can be realized through satellites. Followed by the requirements for satellite positioning accuracy. When a satellite locates a target through the attitude of the satellite, due to the interference of thermal deformation and other interferences in the space environment during the orbital movement of the satellite, the original satellite attitude determination method cannot meet the accuracy requirements. In addition, because the satellite attitude determination system may have deviations and failures, it will also lead to a decrease in the accuracy of attitude determination, which in t...

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Application Information

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IPC IPC(8): G01S19/42G01S19/40G01S19/02
CPCG01S19/02G01S19/40G01S19/42
Inventor 曹喜滨王峰吴云华陈凌峰
Owner HARBIN INST OF TECH
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