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US4746922A Expired / Lapsed US ⏱️ 0.0 years remaining

Method of and device for removing range ambiguity in a pulse-doppler radar and radar including such a device

Assignee: Thales SA
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Filing: 1982-05-06
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Granted: 1988-05-24
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Expires: 2002-05-06
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Abstract

Abstract This invention relates to a method of and a device for removing range ambiguity in a pulse Doppler radar and to a radar including such a device especially for missile guidance. On tracking operation at a high pulse repetition frequency the method consists in switching the repetition frequency f R (k) for each time interval Δt, over a new value f R (k+1) obtained in a circuit from the measured ambiguous range y(k) and from the ambiguity number n(k), as estimated in a circuit from radar information supplied by the radar, in order to remove eclipsing, to maintain the ambiguity number constant and to estimate the range with a growing accuracy in the course of the tracking operation.

Inventors

  • 👤 Michel Prenat

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-28 19:09
CPC Classifications
G; G01; G01S; G01S13/00; G01S13/02; G01S13/06; G01S13/08; G01S13/10; G01S13/22

Claims Analysis

Total Claims: 3
Claim 1
Independent Claim 388 words
A device for removing range ambiguity in a pulse Doppler radar having a high repetition frequency f R (k) which varies at times T k =kΔt, where Δt is the duration of a measurement cycle, operating in the tracking mode, and including a measurement circuit which supplies the measured ambiguous range corresponding to the repetition frequency f R (k) and an estimation circuit which supplies an estimation of the ambiguity number and of the radar-to-target range as well as the standard deviation of the error in the estimated range corresponding to the repetition frequency f R (k), device wherein the repetition frequency is controlled by a servo-loop which, from the measured ambiguous range and from the estimated ambiguity number at the repetition frequency f R (k) calculates the repetition frequency f R (k+1) to be used for the following measurement cycle, such that the ambiguity number at f R (k+1) remains constant, the servo-loop having a transfer function which is of the first order and being composed of the following circuits connected in series: a first subtraction circuit in which the quantity c/4 f R (k), is subtracted from the measured ambiguous range supplied by the radar, c being the velocity of the light; an amplifier having a gain G; a second substration circuit in which the output signal of the amplifier is reduced by the variation of the radar-to-target range during the time lapse Δt, said variation being calculated by a first circuit which multiplies by the duration Δt the radial velocity of the target relative to the radar as supplied by the pulse Doppler tracking radar; a second circuit multiplying the output signal of the second subtraction circuit by a coefficient 1/[n(k)+0.5] calculated by a first calculating circuit supplied with the estimated ambiguity number n(k) corresponding to the repetition frequency f R (k); an adding circuit the first input of which receives the output signal of the second multiplying circuit and which delivers a signal equal to c/2 f R (k+1) and applied to its second input through a delay circuit having a transfer function z -1 ; a second calculating circuit supplied with the output signal c/2 f R (k+1) of the adding circuit and delivering the repetition frequency f R (k+1) which is supplied to the pulse Doppler radar for the following measurement cycle.
Claim 2
Independent Claim 388 words
A device for removing range ambiguity in a pulse Doppler radar having a high repetition frequency f R (k) which varies at times T k =kΔt, where Δt is the duration of a measurement cycle, operating in the tracking mode, and including a measurement circuit which supplies the measured ambiguous range corresponding to the repetition frequency f R (k) and an estimation circuit which supplies an estimation of the ambiguity number and of the radar-to-target range as well as the standard deviation of the error in the estimated range corresponding to the repetition frequency f R (k), device wherein the repetition frequency is controlled by a servo-loop which, from the measured ambiguous range and from the estimated ambiguity number at the repetition frequency f R (k) calculates the repetition frequency f R (k+1) to be used for the following measurement cycle, such that the ambiguity number at f R (k+1) remains constant, the servo-loop having a transfer function which is of the first order and being composed of the following circuits connected in series: a first subtraction circuit in which the quantity c/4 f R (k), is subtracted from the measured ambiguous range supplied by the radar, c being the velocity of the light; an amplifier having a gain G; a second substration circuit in which the output signal of the amplifier is reduced by the variation of the radar-to-target range during the time lapse Δt, said variation being calculated by a first circuit which multiplies by the duration Δt the radial velocity of the target relative to the radar as supplied by the pulse Doppler tracking radar; a second circuit multiplying the output signal of the second subtraction circuit by a coefficient 1/[n(k)+0.5] calculated by a first calculating circuit supplied with the estimated ambiguity number n(k) corresponding to the repetition frequency f R (k); an adding circuit the first input of which receives the output signal of the second multiplying circuit and which delivers a signal equal to c/2 f R (k+1) and applied to its second input through a delay circuit having a transfer function z -1 ; a second calculating circuit supplied with the output signal c/2 f R (k+1) of the adding circuit and delivering the repetition frequency f R (k+1) which is supplied to the pulse Doppler radar for the following measurement cycle.
Claim 3
Dependent Claim 55 words
A device according to claim 1, wherein the estimation circuit is a Kalman filter supplied with radar information including the radial velocity of the target relative to the radar and the power of the useful signal at the pulse repetition frequency f R (k) as well as the pulse repetition frequency f R (k) itself.

References Cited (Backward Citations)

US4106019A Cited
US3935572A Cited
US4064510A Cited
US4143373A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1991-05-24 1991-11-23 1992-05-24 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1995-05-24 1995-11-23 1996-05-24 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1999-05-24 1999-11-23 2000-05-24 $7700.00 Window Closed / Lapsed

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