Method of measuring the altitude of a target maneuvering at a very low elevation, and a tracking radar using same

• US 4,163,975 A
• Filed: 01/03/1978
• Issued: 08/07/1979
• Est. Priority Date: 01/07/1977
• Status: Expired due to Term

• Current Assignee: Thomson-CSF (Thales SA)
• Original Assignee: Thomson-CSF (Thales SA)
• Inventors: Guilhem, Robert, Rivron, Maurice, Weulersse, Bruno
• Primary Examiner(s): Tubbesing, T. H.
• Application Number:
  US05/866,774
• Time in Patent Office: 581 Days
• Field of Search: 343/16 M
• US Class Current: 342/94
• CPC Class Codes: G01S 13/4418 with means for eliminating radar-dependent errors in angle measurements, e.g. multipath effects
• CPC Class Codes: G01S 13/685 using simultaneous lobing techniques

Abstract

A method of measuring the altitude of a target maneuvering at very low elevations is used to determine the instantaneous deviation of the target at various operating frequencies of a monopulse tracking radar. The quadrature component of the difference signal is evaluated at these frequencies, the mean values of the instantaneous deviation and of the quadrature component are determined for a certain number of frequency samples, and an extreme value of the mean value of the quadrature component is found to allow the corresponding mean value of deviation to be validated.

Claims

1. A method of operating a monopulse tracking radar with a given pass band for measuring the altitude of a target maneuvering at a very low elevation by determining the angular aiming error existing between the direction of the target and the aiming axis of said radar, comprising the following steps:

deriving sum and difference signals from incoming energy reflected by a target and received by an antenna of the radar with the vector representing the sum signal;

separating an in-phase component of said difference signal colinear with the sum signal from a quadrature component thereof perpendicular to said sum signal;

successively generating a multiplicity of sampling frequencies within said pass band;

measuring said quadrature component and a deviation signal representative of an instantaneous angular aiming error, extracted from said sum signal and said in-phase component, for each of said sampling frequencies;

averaging said deviation signal and said quadrature components measured with overlapping series of successive sampling frequencies to obtain respective mean values therefor;

detecting an extreme point of substantially zero slope on a curve formed from said quadrature component; and

validating the mean value of said deviation signal for a sampling frequency corresponding to said extreme point.

2. A method as defined in claim 1 wherein measured voltages representing said deviation signal and said quadrature component are averaged in each of said overlapping series over a number N of successive sampling frequencies, less than the total number of sampling frequencies in said pass band, said mean values being respectively represented by ##EQU15## wherein E_i, E_m, DQ_i, DQ_m are, respectively, the mean value of the voltage representing said deviation signal, the instantaneous value of a voltage representing said deviation signal at a frequency m, the mean value of the voltage representing said quadrature component, and the instantaneous value of the voltage representing said quadrature component at the frequency m.

3. A method as defined in claim 2 wherein the values representing the mean deviation signal E_i and the mean quadrature component DQ_i are derived from differently weighted voltages representing the instantaneous values of the voltages and, respectively.

4. A method as defined in claim 2 wherein the detection of said extreme point includes the steps of algebraically summing the last 2p instantaneous values of voltages obtained from successive measurements of said quadrature component, weighting the algebraic sums of the last p instantaneous values and of the immediately preceding p instantaneous values with coefficients of opposite sign, and monitoring a change in sign of the difference between said algebraic sums.

5. A method as defined in claim 4 wherein said weighting coefficients are +1 and -1.

6. A method as defined in claim 1 wherein said quadrature component is obtained by shifting by π

/2 the phase of said difference signal and by demodulating the phase-shifted difference signal with respect to the vector of said sum signa.

7. A tracking radar of monopulse type for acertaining the altitude of a target, maneuvering at very low elevation, by processing reflected energy constituting a sum signal and a difference signal, said difference signal having an in-phase component colinear with said sum signal and a quadrature component perpendicular to said sum signal, comprising:

a first and a second channel for respectively processing said sum signal and said difference signal;

a third channel in parallel with said second channel including a π

/2 phase shifter for processing the quadrature component of said difference signal;

a first demodulator with input connections to said first and second channels for deriving from the ratio of said difference and sum signals a deviation signal proportional to an angular aiming error between the direction of said target and an aiming axis of the radar at an operating frequency thereof;

a second demodulator with input connections to said first and third channels for delivering a signal voltage representing said quadrature component;

oscillator means for successively generating a multiplicity of different operating frequencies within a predetermined pass band, said channels being provided with mixer means connected to said oscillator means;

first filter means connected to said first demodulator for smoothing short-term variations of said deviation signal to provide a frequency-dependent error signal;

second filter means connected to said second demodulator for smoothing short-term variations of said signal voltage, thereby producing a resulting voltage varying with said operating frequencies;

validating means connected to said second filter means for detecting an extreme value of said resulting voltage; and

output means connected to said first filter means and to said validating means for passing said error signal upon the occurrence of said extreme value.

8. A tracking radar as defined in claim 7 wherein said first filter means comprises an integrating network including a series inductance and a shunt capacitance.

9. A tracking radar as defined in claim 7 wherein said validating means comprises a differential amplifier with two inputs respectively connected to said first filter means by a direct path and by a delay line.

10. A tracking radar as defined in claim 7 wherein said oscillator means comprises a frequency synthesizer.

11. A tracking radar as defined in claim 7 wherein said output means comprises a differentiation circuit connected to said validating means for producing a trigger pulse derived from said resulting voltage upon a change in the polarity of said resulting voltage, a delay network connected to said first filter means, and a normally blocked gate in series with said delay network controlled by said trigger pulse for conducting upon a triggering of the latter.

12. A tracking radar as defined in claim 11 wherein said output means further comprises a monostable circuit connected to said differentiation circuit for actuation by said trigger pulse, said gate having a control input connected to said monostable circuit.

13. A tracking radar as defined in claim 7 wherein said first, second and third channels include respective first, second and third intermediate-frequency amplifiers downstream of said mixer means, further comprising automatic-gain-control means connected in parallel with said first and second demodulators to said first channel for generating a first control voltage for said first and second intermediate-frequency amplifiers and a second control voltage of half the dynamic range of said first control voltage for said third intermediate-frequency amplifier.

14. A tracking radar as defined in claim 13 wherein said automatic-gain-control means includes a first operational amplifier receiving said first control voltage, a voltage divider in series with a blocking capacitor in an output of said first operational amplifier, and a second operational amplifier having an input connected to a tap of said voltage divider for producing said second control voltage.