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Method for estimating target track dynamics of electronic reconnaissance satellite and implementation device of method

A technology for reconnaissance satellites and target tracks, used in satellite radio beacon positioning systems, measurement devices, navigation calculation tools, etc.

Active Publication Date: 2019-01-08
SHANGHAI ENG CENT FOR MICROSATELLITES
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

On the other hand, the electronic reconnaissance satellite is affected by factors such as technical system and measurement error, and the measured signal source position has a random error of 5-10 kilometers

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  • Method for estimating target track dynamics of electronic reconnaissance satellite and implementation device of method
  • Method for estimating target track dynamics of electronic reconnaissance satellite and implementation device of method
  • Method for estimating target track dynamics of electronic reconnaissance satellite and implementation device of method

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Embodiment Construction

[0034] In the following description, the present invention is described with reference to various examples. One skilled in the art will recognize, however, that the various embodiments may be practiced without one or more of the specific details, or with other alternative and / or additional methods, materials, or components. In other instances, well-known structures, materials, or operations are not shown or described in detail so as not to obscure aspects of the various embodiments of the invention. Similarly, for purposes of explanation, specific quantities, materials and configurations are set forth in order to provide a thorough understanding of embodiments of the invention. However, the invention may be practiced without these specific details. Furthermore, it should be understood that the various embodiments shown in the drawings are illustrative representations and are not necessarily drawn to scale.

[0035] In this specification, reference to "one embodiment" or "the...

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Abstract

The invention discloses a method for estimating target track dynamics of an electronic reconnaissance satellite. The method is proposed according to different distribution variances of the projectionof position data of a measured moving target in different navigation directions, and comprises the following steps: generating projection bases of all possible navigation directions of the moving target; projecting measured two-dimensional position data on each projection base to achieve dimensionality reduction; calculating a data variance after the projection of the position data, and taking thedata variance as an estimated decision condition; comparing variances of projected data in all the navigation directions, selecting the projection base navigation direction with the largest varianceas the navigation direction estimation of the moving target, and taking the projected target data as a preliminary estimation result of the track; averaging the preliminary estimation result in a multi-point manner, and taking an averaged track estimation result as a final output result.

Description

technical field [0001] The invention relates to a data processing algorithm and its hardware realization, in particular to a track estimation data processing algorithm for electronic reconnaissance satellite identification target and its realization device. Background technique [0002] Electronic Reconnaissance Satellite (Electronic Reconnaissance Satellite) is a reconnaissance satellite used for reconnaissance, intercepting electromagnetic signals sent by enemy radar, communication and weapon telemetry systems, and measuring the location of the signal source. Limited by satellite computing capabilities, reconnaissance satellites are only responsible for intercepting the original information of enemy targets. The original information is transmitted to the ground by satellites, and the final intelligence information is completed by ground computing equipment. [0003] Electronic reconnaissance satellites can be divided into radar intelligence reconnaissance satellites and co...

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Application Information

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IPC IPC(8): G01C21/20G01C21/24
CPCG01S19/42
Inventor 常凯梁广王晓梅马菁涛吕松玲赵元瑞刘会杰
Owner SHANGHAI ENG CENT FOR MICROSATELLITES
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