High precision range measurement technique

• US 6,492,937 B1
• Filed: 11/02/2001
• Issued: 12/10/2002
• Est. Priority Date: 11/02/2001
• Status: Expired due to Fees

• Current Assignee: Harris Corporation (L3Harris Technologies, Inc.)
• Original Assignee: ITT Manufacturing Enterprises, Inc. (ITT, Inc.)
• Inventors: Cikalo, Joseph, Sparrow, Mitchell J.
• Primary Examiner(s): Gregory, Bernarr E.
• Application Number:
  US09/985,297
• Time in Patent Office: 403 Days
• Field of Search: 342/52, 342/58, 342/60, 342/118-146, 342/175, 342/195, 342/357-1-3, 342/42-51, 342/165, 342/173, 342/174, 342/13-20, 342/25, 701/300, 701/301, 701/302
• US Class Current: 342/125
• CPC Class Codes: G01S 13/76 wherein pulse-type signals are transmitted
• CPC Class Codes: G01S 13/86 Combinations of radar systems with non-radar systems, e.g. sonar, direction finder
• CPC Class Codes: G01S 7/38 Jamming means, e.g. producing false echoes

Abstract

Electronic Warfare (EW) systems aboard aircrafts are used to protect them from guided missile by denying threat radar systems the ability to track the aircrafts. In a typical operation, a threat radar system transmits RF signals aimed at the target aircraft. The surface of the target reflects a portion of the incident signal back towards the threat radar antenna where the reflected signal is detected, allowing the threat radar system to determine the target'"'"'s range, angle and velocity. The present invention relates to EW systems that are dependent on measuring the RF phase of a signal transmitted by a target tracking threat radar. The use of the invented technique will make it possible to implement a robust Electronic Counter-Measures (ECM) technique, known as Cross-Eye, using two airborne platforms. The technique is very effective in preventing a threat radar from tracking a target aircraft and guiding a launched missile to the target aircraft.

Claims

1. A method of measuring distance between two platforms with high precision, comprising the steps of:

determining an estimate of distance D between the two platforms within a first range of error;

transmitting an RF signal from a range-only radar located on a first platform;

receiving the RF signal transmitted by the range-only radar on the first platform by a repeater located on a second platform;

retransmitting the RF signal by the repeater on the second platform;

receiving the retransmitted RF signal by the range-only radar located on the first platform;

measuring phase difference between the RF signal transmitted by the range-only radar located on the first platform and the RF signal retransmitted by the repeater located on the second platform;

converting the measured phase difference to a measure of distance δ

; and

adding the estimate of the distance D to the measure of distance δ

, to obtain a measure of total distance between the two platforms.

2. The method of claim 1 where the estimate of distance D between the two platforms is determined using a global positioning system.

3. The method of claim 2 where the first and the second platforms are on airborne vehicles.

4. The method of claim 2 wherein the wavelength of the RF signal transmitted from the range-only radar located on the first platform is greater than the first range of error.

5. The method of claim 4 wherein the RF signal transmitted by the range-only radar is in the form of a stream of coherent pulses.

6. The method of claim 2 further comprising the steps of:

dividing the measure of total distance between the two platforms by wavelength of signal generated by a second local oscillator on the second platform;

converting the remainder from the division to a phase shift value; and

inserting the phase shift to the local oscillator on the second platform.

7. The method of claim 6 further comprising:

transmitting of a first ECM signal by a first local oscillator on the first platform; and

transmitting of a second ECM signal by the second local oscillator on the second platform.

8. The method of claim 7 wherein the frequency of the first local oscillator on the first platform and the frequency of the second local oscillator on the second platform is equal to the frequency of a signal generated by a threat radar system and reflected by a target vehicle.

9. The method of claim 8 wherein the ECM signal transmitted by the first local oscillator on the first platform and the ECM signal transmitted by the second local oscillator on the second platform combine spatially such that the combined signal is 180°

degrees out of phase with the signal generated by the threat radar system and reflected by the target vehicle.

10. A system for measuring distance between two platforms with high precision comprising:

a system for measuring an estimate of distance D between the two platforms within a first range of error;

a range-only radar located on a first platform for transmitting an RF signal;

a repeater located on a second platform for receiving the RF signal transmitted by the range-only radar located on the first platform and for retransmitting an RF signal;

the range-only radar receiving the RF signal retransmitted by the repeater and measuring phase difference between the RF signal transmitted by the range-only radar and the RF signal retransmitted by the repeater;

a processor for converting the measured phase difference value to a measure of distance δ and

adding the measure of distance δ

to the estimate of distance D, to obtain a measure of total distance between the two platforms.

11. The system of claim 10 wherein the system for measuring the estimate of distance D between the two platforms is a global positioning system.

12. The system of claim 11 wherein the first and second platforms are on airborne vehicles.

13. The system of claim 11 wherein the wavelength of the RF signal transmitted from the range-only radar located on the first platform is greater than the first range of error.

14. The system of claim 13 wherein the RF signal transmitted by the range-only radar is in the form of a stream of coherent pulses.

15. The system of claim 11 further comprising a first local oscillator on the first platform and a second local oscillator on the second platform, wherein:

the processor divides the measure of total distance between the two platforms by the wavelength of the signal of the second local oscillator on the second platform, converts the remainder of the division to a phase shift value, and inserts the phase shift to the second local oscillator on the second platform.

16. The system of claim 15 wherein:

the first local oscillator on the first platform transmits an ECM signal and the second local oscillator on the second platform transmits an ECM signal.

17. The system of claim 16 wherein the frequency of the ECM signal transmitted by the first local oscillator on the first platform and the frequency of the ECM signal transmitted by the second local oscillator on the second platform are equal to the frequency of a signal generated by a threat radar system and reflected by a target vehicle.

18. The system of claim 17 wherein the ECM signal transmitted by the first local oscillator on the first platform and the ECM signal transmitted by the second local oscillator on the second platform combine spatially such that the combined signal is 180°

degrees out of phase with the signal generated by the threat radar system and reflected by the target vehicle.