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US5124708A Expired / Lapsed US ⏱️ 0.0 years remaining

RF stability measuring system for MTI radars

Assignee: United States Department of the Air Force
•
Filing: 1991-02-25
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Granted: 1992-06-23
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Expires: 2011-02-25
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Abstract

Abstract The disclosed system comprises a testing system which measures the stability of a moving target indicator radar transmitter. It automatically measures the imperfections of its internal in-phase (I)/quadrature (Q) demodulator, and it consists of a control computer, a synchronizer, a frequency synthesizer, an IQ demodulator, a low noise amplifier and a waveform recorder. A unit under test is inserted across the test set for measurement and calibration. The system set has the following features: (a) An automatic calibration routine that requires a tunable RF source. This source provides the RF drive to the UUT. (b) A discontinuous analog to digital (A/D) sample clock that has a precise controllable relationship with the RF pulse. The A/D sample clock samples only during the presence of the RF. (c) A method for computing stability using a table of amplitude and phase weighting coefficients and pulse positions. This table is generated by the user and any desired combination of values is possible. The discontinuous sample clock is used in the acquisition of the raw stability data. During data collection, the computer commands the synchronizer to output a pulse train. The pulse train contains pulses with various pulse widths and pulse repetition frequencies. The synchronizer output turns on the UUT causing it to provide an RF output signal. The synchronizer also sends out bursts of pulses that make the waveform recorder digitize and I and Q video signal from the low noise amplifier. Under the control of the computer, the synthesizer generates two RF signals. One RF signal is applied to the UUT and the other RF is applied directly to the IQ demodulator where the two signals are compared. The IQ demodulator provides the I and Q signal inputs to the low noise amplifier.

Inventors

  • 👤 David C. Mackes
  • 👤 Franklin B. Jones

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-29 14:27
CPC Classifications
G; G01; G01S; G01S7/00; G01S7/02; G01S7/40; G01S7/4004; G01S7/4008

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 281 words
In a system for calibrating the stability of an MTI radar unit under test, said system including a frequency synthesizer, an IQ demodulator having first and second input terminals and first and second output terminals, a synchronizer, a waveform recorder and a control computer for controlling the operation of said system in accordance with a user program, said frequency synthesizer supplying RF to said unit and to one input terminal of said IQ demodulator, the RF output of said unit being supplied to the other input terminal of said IQ demodulator; means, under the control of said computer generating sync pulses from the output of said synchronizer, said sync pulses enabling said unit under test, said frequency synthesizer and said waveform recorder, the method, under the control of said computer, comprising the steps of: a. stepping up the synthesizer RF output to said unit from a lower frequency to a higher frequency until a positive going zero crossing is detected in the I output of said IQ demodulator; b. stepping down the synthesizer RF output to said unit from said higher frequency to said lower frequency until a negative going zero crossing is detected in the I output of said IQ demodulator; c. sweeping the synthesizer RF output to said unit from the lower frequency to the higher frequency; d. during step c, digitizing the I and Q outputs of said IQ demodulator and storing such digitized information in said computer; e. calculating the quadrature error in said computer in accordance with the following equation: Quadrature Error=[(N/4)-X]* (360/N) degrees where: N=the number of points in 360 degrees, and X=the number of points between the I and Q negative going zero crossings.
Claim 2
Dependent Claim 281 words
In a system for calibrating the stability of an MTI radar unit under test, said system including a frequency synthesizer, an IQ demodulator having first and second input terminals and first and second output terminals, a synchronizer, a waveform recorder and a control computer for controlling the operation of said system in accordance with a user program, said frequency synthesizer supplying RF to said unit and to one input terminal of said IQ demodulator, the RF output of said unit being supplied to the other input terminal of said IQ demodulator; means, under the control of said computer generating sync pulses from the output of said synchronizer, said sync pulses enabling said unit under test, said frequency synthesizer and said waveform recorder, the method, under the control of said computer, comprising the steps of: a. stepping up the synthesizer RF output to said unit from a lower frequency to a higher frequency until a positive going zero crossing is detected in the I output of said IQ demodulator; b. stepping down the synthesizer RF output to said unit from said higher frequency to said lower frequency until a negative going zero crossing is detected in the I output of said IQ demodulator; c. sweeping the synthesizer RF output to said unit from the lower frequency to the higher frequency; d. during step c, digitizing the I and Q outputs of said IQ demodulator and storing such digitized information in said computer; e. calculating the quadrature error in said computer in accordance with the following equation: Quadrature Error=[(N/4)-X]* (360/N) degrees where: N=the number of points in 360 degrees, and X=the number of points between the I and Q negative going zero crossings.
Claim 3
Dependent Claim 54 words
The method of claim 1, wherein prior to calculating said quadrature error, computations are made in said computer to calculate (1) DC offset between the voltages measured in the I and Q channels, and (2) the I and Q channel imbalance, in accordance with the following equations: DC Offset=(|Vmax|-Vmin|)/2 Vpeak=Vmax-DC Offset, and Channel Imbalance=VpeakQ/VpeakI.
Claim 4
Dependent Claim 23 words
The method of claim 1 wherein the period of generation of the RF applied to said IQ demodulator is controlled by said computer.
Claim 5
Dependent Claim 34 words
The method of claim 3 wherein the outputs of said IQ demodulator are digitized and stored in said computer only during the periods of generation of said RF pulses applied to said IQ demodulator.

References Cited (Backward Citations)

US3701153A Cited
US4768035A Cited
US4851853A Cited
US4783660A Cited
US4940985A Cited
US4931800A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1995-06-23 1995-12-23 1996-06-23 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1999-06-23 1999-12-23 2000-06-23 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2003-06-23 2003-12-23 2004-06-23 $7700.00 Window Closed / Lapsed

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