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Method for extracting space conical reentry target micro-motion features based on empirical mode decomposition

An empirical mode decomposition and feature extraction technology, applied in the field of radar, can solve the problems of increased computational complexity, failure of micro-motion feature extraction, errors, etc., to achieve the effect of improving the efficiency of feature extraction

Inactive Publication Date: 2017-06-13
XIDIAN UNIV
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AI Technical Summary

Problems solved by technology

The micro-movement feature extraction methods based on time-frequency diagrams all need to solve the problem of frequency point correlation, but there are two shortcomings in frequency point correlation. The extraction of motion features fails; on the other hand, time-frequency correlation will increase the computational complexity and reduce the efficiency of micro-motion feature extraction

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  • Method for extracting space conical reentry target micro-motion features based on empirical mode decomposition
  • Method for extracting space conical reentry target micro-motion features based on empirical mode decomposition
  • Method for extracting space conical reentry target micro-motion features based on empirical mode decomposition

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Embodiment Construction

[0028] The present invention will be further described below in conjunction with accompanying drawing:

[0029] A transceiver co-located radar aimed at by the present invention, the radar transmitting carrier frequency is f c , the pulse width is T p , a narrow-band chirp signal with a modulation frequency of γ, and is observed below the cone target's advancing direction.

[0030] refer to figure 1 , for the realization steps of the present invention are as follows:

[0031] Step 1: Calculate the transmitted signal sf according to the narrowband chirp signal model.

[0032] 1a) The narrowband chirp signal model is as follows:

[0033]

[0034] Among them, rect(·) represents unit rectangular signal, exp(·) represents exponential operation, j represents imaginary number unit, t is sampling time, γ is modulation frequency, f c is the transmitting carrier frequency, T p is the pulse width;

[0035] 1b) According to the narrow-band linear frequency modulation signal model...

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Abstract

The invention discloses a method for extracting space conical reentry target micro-motion features based on empirical mode decomposition, which mainly solves the problem of easiness in failure of feature extracting in the prior art. The method adopts the scheme with the following steps of 1, according to a narrow-band linear frequency modulating signal model, calculating a transmitting signal sequence in a pulse repeating cycle; 2, according to a transmitting signal and a received target echo signal, establishing a pulse compression signal matrix, and establishing a Doppler echo signal of a conical reentry target according to the matrix; 3, according the calculated Doppler echo signal of the conical reentry target, utilizing the empirical mode decomposition to obtain a plurality of feature mode functions; 4, according to the obtained feature mode functions, reestablishing a Doppler signal of a conical reentry target scattering center; 5, according to the reestablished scattering center signal, establishing a time-frequency map of the conical reentry target scattering center; 6, extracting the micro-motion features of the target from the time-frequency map. The method has the advantage that while the micro-motion features are accurately extracted, the feature extracting efficiency is improved, so that the method can be used for identifying the target.

Description

technical field [0001] The invention belongs to the technical field of radar, in particular to a method for extracting micro-movement features of a space cone target, which can be used for target recognition. Background technique [0002] When the space cone target or component moves on its orbit, it is usually accompanied by some small movements such as rotation and vibration. These small movements are called fretting. Moving objects are usually accompanied by micro-movements, such as the swing of the limbs when walking, the chest vibration caused by human breathing and heartbeat, the rotation of the wheel when the vehicle is moving forward, the rotation of the helicopter rotor, the rotation of the antenna, the vibration of the engine when it is working, etc. The fretting phenomenon was first observed in coherent lidar and applied to vibration measurement. In 2000, Professor V.C. Chen of the U.S. Naval Laboratory introduced it into the research of microwave radar, and defi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01S13/50
CPCG01S13/505
Inventor 纠博时玉春刘宏伟王鹏辉戴奉周
Owner XIDIAN UNIV
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