Interrupted track correlation method of maritime target of high-orbit optical satellite

A technology for optical satellite and track association, which is applied in navigation, surveying and navigation, complex mathematical operations, etc., and can solve problems such as poor correlation effect

Active Publication Date: 2020-01-14
NAT INNOVATION INST OF DEFENSE TECH PLA ACAD OF MILITARY SCI
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Problems solved by technology

The traditional interrupted track correlation method mainly deals with the problem of track interruption caused by target occlusion, target maneuvering, etc., and the track fragment correlation is mainly based on statistical distance, and the correlation effect is poor in complex situations such as long-term intervals and dense distribution of targets.

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  • Interrupted track correlation method of maritime target of high-orbit optical satellite
  • Interrupted track correlation method of maritime target of high-orbit optical satellite
  • Interrupted track correlation method of maritime target of high-orbit optical satellite

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Embodiment Construction

[0068] In order to make the purpose, technical solution and advantages of the present invention clearer, the technical solution of the present invention will be clearly and completely described below in conjunction with specific embodiments of the present invention and corresponding drawings. Apparently, the described embodiments are only some of the embodiments of the present invention, but not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts fall within the protection scope of the present invention.

[0069] The technical solutions provided by the embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings.

[0070] The embodiment of the present invention provides a high-orbit optical satellite maritime target interruption track correlation method, as shown in the attached figure 1 And attached image...

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Abstract

The invention discloses an interrupted track correlation method of a maritime target of a high-orbit optical satellite. The method comprises the steps of: performing backward extrapolation on a previous first track and performing forward extrapolation on a latter second track; performing preliminary correlation on the first track and the second track whose state estimation at the same moment meetsconstraint conditions; performing further correlation on the tracks in a preliminary correlation set to obtain a further correlation set; solving the further correlation set by using a two-dimensional optimal allocation principle to obtain a first stage correlation set with the minimal global cost; solving a possible correlation segment pair of a complementary set of the first stage correlation set in the preliminary correlation set by using distance two-dimensional optimal allocation; detecting and screening an intermediate correlation set by using an amplitude relationship to obtain a second stage correlation set; and fitting correlated tracks in the first stage correlation set and the second stage correlation set to obtain a continuous track. By adopting the interrupted track correlation method of the maritime target of the high-orbit optical satellite disclosed by the invention, the performance of track correlation is improved.

Description

technical field [0001] The invention relates to the technical field of space-based maritime target monitoring, in particular to a high-orbit optical satellite maritime target interruption track correlation method. Background technique [0002] The working modes of high-orbit (the present invention refers to geostationary orbit) optical satellites can be different according to the satellite observation tasks. Taking my country's "Gaofen No. 4" (GF-4) satellite as an example, its working modes are mainly divided into staring imaging , area imaging and mobile inspections. Among them, the staring imaging mode is continuous imaging of the surveillance area, the regional imaging mode is splicing imaging of the surveillance area, and the mobile inspection mode is based on mission requirements, using attitude maneuvers to quickly complete the imaging of multiple areas. Constrained by the resources on the satellite, the daily working hours of the satellite are limited and cannot be t...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01C21/20G06F17/18
CPCG01C21/203G06F17/18
Inventor 刘勇曹璐郭鹏宇李献斌王建
Owner NAT INNOVATION INST OF DEFENSE TECH PLA ACAD OF MILITARY SCI
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