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Passive positioning method based on antenna periodic scanning time difference

A passive positioning and time difference technology, which is applied to the beacon system using radio waves and other directions, can solve the problems of scanning time difference, slow tracking convergence speed, and low accuracy, and achieve the effect of improving positioning accuracy.

Active Publication Date: 2017-08-25
HARBIN INST OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The present invention aims to solve the problems of slow tracking convergence speed, low precision and certain maneuvering in the current passive positioning method, and proposes a passive positioning method based on antenna cycle scanning time difference

Method used

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  • Passive positioning method based on antenna periodic scanning time difference
  • Passive positioning method based on antenna periodic scanning time difference
  • Passive positioning method based on antenna periodic scanning time difference

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Experimental program
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specific Embodiment approach 1

[0070] Embodiment 1: The passive positioning method based on antenna periodic scanning time difference includes the following steps:

[0071] Considering the two-dimensional single-station passive tracking problem, figure 1 A schematic diagram of the geometric relationship between the target Tar and the observer O is given, in the figure T ar (x, y) represents the coordinates of the target Tar in the coordinate system of the observation platform, (X T ,Y T ) indicates the coordinates of the target in the geodetic coordinate system, X(E) indicates that the X axis is due east, and Y(N) indicates that the Y axis is due north.

[0072] The target Tar is in a static state, and the observation platform O moves in a straight line at a uniform speed along the y direction. The observer passively receives the signal radiated by the target Tar, and uses the passive measurement of the signal to locate and track the target. The target radar antenna performs circular scanning at a fixed ...

specific Embodiment approach 2

[0089] Specific embodiment two: the difference between this embodiment and specific embodiment one is: obtain x in the described step 2 in the solution equation, y, the specific process of the three equations that T three unknown quantities need are:

[0090] Since the geodetic coordinate system and the platform coordinate system have the conversion relationship of formula (1) - formula (3), it can be directly obtained from image 3 or Figure 4 To locate the target, the present invention only requires θ in the figure i For an angle greater than zero, avoid that the latter point is on the lower side of the line connecting the previous point and the target. When such a large corner is necessary, the front and rear segments can be positioned as independent positioning segments, and then converted to the absolute coordinate system Click below to get the positioning results.

[0091] exist image 3 and Figure 4 Medium θ i In the triangle, there is the following expression: ...

specific Embodiment approach 3

[0103] Specific embodiment three: the difference between this embodiment and specific embodiment one or two is: in the described step 4, solve the parameter R of the recursive least squares method i , and P 0 The specific process is:

[0104] R i The solution process is:

[0105] Deriving both sides of formula 24 with respect to time t, formula (26) can be obtained:

[0106]

[0107] where ψ=2π(τ i -T);

[0108] Take four consecutive points, each adjacent two points as a group, and substitute them into the formula (26) to get three equations, which can be expressed as A 3× 3 f 3×1 =b 3×1 , then it can be obtained by formula (14)

[0109]

[0110] will f 3×1 Substituting each element into formula (27) can get R i :

[0111]

[0112] said is the variance of the error of the time measurement;

[0113] and P 0 The solution process is:

[0114] said is the initial state estimate, P 0 is the initial state covariance, if not given and P 0 , then ...

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Abstract

The invention provides a time difference passive location method based on antenna cycle scanning, relates to a time difference location method, and aims at solving the problems of low tracking convergence speed, low precision and the requirement for certain maneuvering of the currently used passive location method. Coordinate systems between a platform and a target are established, and a calculation method for target position is acquired according to the established coordinate systems and the conversion relationship. The solution of the target position is selected by utilizing the limit of detection range, and finally a location result with measurement error is optimized by adopting a recursive least square method so that position estimation after optimization is obtained. Target location can be completed only by utilizing an antenna scanning time observation value and the platform state. Besides, the limit of the movement form of the observation platform is less, and location precision increases along with increasing of time measurement precision so that the method is a new location method and is an effective supplement for the present passive location system and can be applied to the field of passive location.

Description

technical field [0001] The invention relates to a time difference positioning method. Background technique [0002] Passive radar has the advantages of good concealment and strong ability to detect stealth and low-altitude targets in application, but due to its passive characteristics, it cannot effectively locate silent targets, and it also brings measurement accuracy problems. The passive positioning methods generally studied include time-of-arrival method and direction-finding cross-location method. Although the accurate measurement of the arrival time based on the arrival time method can reflect the change of the radial distance of the target, this method has the disadvantages of slow speed and low accuracy of arrival time; the direction finding line cross positioning method requires the observation platform to have a certain maneuvering flight , which brings a lot of inconvenience to the application of this technology. In addition, the slow convergence speed and low pr...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01S1/08
CPCG01S1/08
Inventor 刘梅邓展涛高扬
Owner HARBIN INST OF TECH