Satellite dynamic strip region resolution method described by static mesh

A static grid and area technology, applied in the field of satellite observation, can solve the problems of accuracy loss, inconsistent grid cell size, inconvenient use, etc., to avoid differences and facilitate unified processing.

Inactive Publication Date: 2017-05-31
SPACE STAR TECH CO LTD
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Problems solved by technology

The division method based on the actual geographical distance needs to be calculated to clarify the latitude and longitude values ​​of the four corner points of each grid cell, and the calculated latitude and longitude values ​​are not integer values, which is not convenient to use, and the accuracy is also lost during the calculation process
At the same time, the curvature of the earth's ellipsoid causes the n×n km grid cells to be trapezoidal instead of square, and t

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  • Satellite dynamic strip region resolution method described by static mesh
  • Satellite dynamic strip region resolution method described by static mesh
  • Satellite dynamic strip region resolution method described by static mesh

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Embodiment Construction

[0046] The following description with reference to the accompanying drawings is provided to assist in a comprehensive understanding of various embodiments of the present disclosure as defined by the claims and their equivalents. The following description includes various specific details to aid in understanding, but these are to be regarded as merely exemplary. Accordingly, those of ordinary skill in the art will recognize that various changes and modifications of the various embodiments described herein can be made without departing from the scope and spirit of the disclosure. Also, descriptions of well-known functions and constructions may be omitted for clarity and conciseness.

[0047] The terms and words used in the following description and claims are not limited to the bibliographical meanings, but, are merely used by the inventor to enable a clear and consistent understanding of the present disclosure. Accordingly, it should be apparent to those skilled in the art tha...

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Abstract

The invention discloses a satellite dynamic strip region resolution method described by static mesh. The satellite dynamic strip region resolution method comprises the following steps: firstly, dynamically generating an observation strip through satellite parameter characteristics according to a satellite track; secondly, dividing the observation strip by utilizing a static mesh, so as to calculate observation earnings of the mesh and an observation region. A region observation task is dynamically divided into mask tasks according to characteristics of a satellite, and the capability characteristics and observation earnings of the satellite can be sufficiently considered, so that the satellite dynamic strip region resolution method is especially suitable for optimizing the satellite task in a joint observation process of the plurality of satellites. The observation region is divided into a plurality of sub-regions by utilizing the static mesh; the meta tasks are uniformly described and processed; difference between an imaging target and imaging region coverage in the aspect of layout processing is avoided; under the condition that the resolution calculation amount of the strip is remarkably increased, the satellite observation strip is resolved dynamically and rapidly, and uniform processing of the tasks is convenient to realize when the satellite accesses a calculation plan.

Description

technical field [0001] The invention relates to the technical field of satellite observation, in particular to a satellite dynamic strip region splitting method described by a static grid. Background technique [0002] When remote sensing satellites perform regional observation tasks, they usually cannot be completed only by a single scouting, so the observation area must be split into appropriate strips in order to achieve efficient observation. [0003] Region splitting mainly includes: 1) The region is decomposed into a set coverage problem after single scene decomposition; 2) The pre-defined reference system is used to decompose, and the reference system divides the whole world into grids with different numbers according to a certain coordinate system. The regional decomposition is equivalent to "Counting grids"; 3) Decompose the area into parallel strips of fixed width according to the satellite flight radial direction and load width; 4) Decompose the area into dynamic ...

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Application Information

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IPC IPC(8): G01C15/00
CPCG01C15/00
Inventor 罗冠辰齐昕浒任霁辉刘辰龙高越
Owner SPACE STAR TECH CO LTD
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