Apparatus and methods for locating a target utilizing signals generated from a non-cooperative source

• US 4,746,924 A
• Filed: 11/20/1985
• Issued: 05/24/1988
• Est. Priority Date: 09/30/1985
• Status: Expired due to Fees

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Lightfoot, Fred M.
• Primary Examiner(s): Blum, Theodore M.
• Assistant Examiner(s): Cain, David
• Application Number:
  US06/799,912
• Time in Patent Office: 916 Days
• Field of Search: 342/453, 342/487, 342/424, 342/192, 342/13, 342/14, 342/17, 342/18, 342/159, 455/133-135, 455/62
• US Class Current: 342/453
• CPC Class Codes: G01S 13/003 Bistatic radar systems; Multistatic radar systems
• CPC Class Codes: G01S 5/12 by co-ordinating position lines of different shape, e.g. hyperbolic, circular, elliptical or radial

Abstract

The positions of a non-cooperative emitter (illuminator) and reflector (target) relative to a receiver of electromagnetic energy, which neither directly nor indirectly controls the illuminator, is determined utilizing emissions received directly from the illuminator as well as reflected emissions from the target. A range R_I between the receiver and the non-cooperative illuminator is determined by measuring the time difference between receiving the reflected signals at a pair of interferometer antennas located at the wing tips of a receiver aircraft. Calculation of the location of the target is accomplished by utilizing range R_I, as well as a time differential Δt between the receipt of the reflected signals at the interferometer antennas and the receipt of a corresponding direct signals at a radar antenna located at the aircraft. In the event there is clutter in the reflected signal which hinders the determination of the time differential Δt, clutter processing is performed utilizing the direct signals as a coherent reference and by cross-correlating the direct and reflected signals. The determination of the bearing of the target and the illuminator relative to the receiver is accomplished by an amplitude comparison of the signals received at multiple ports of a multiple beamed phased array radar antenna. The bearing information together with the range and time differential is processed to provide the necessary commands for generating a visual display of the positions of target and illuminator relative to the receiver.

Claims

1. In a receiver aircraft on a predetermined route of flight, apparatus for locating a position of a reflector of electromagnetic signals relative to a receiver of said electromagnetic signals, said apparatus comprising:

a. first means for processing a plurality of said received electromagnetic signals which are characterized by their generation from a plurality of signal emitters which are both unassociated from and non-cooperative with said receiver, and for generating a first signal output of said processed signals, said signal emitters including (i) known signal emitters having locations and signal characteristics which are known prior to said flight and which are known to be receivable along said route of flight, and (ii) unknown signal emitters having locations and signal characteristics which are not known prior to said flight and which are also receivable along said route of flight;

b. second means for selecting one of said received signals having a first component which is reflected from said reflector, and a second nonreflected component, in a manner that said selected signal is an optimum signal for locating the position of said reflector, said second means including

(1) means for determining the geographical locations of said signal emitters relative to the aircraft,

(2) computer means including

(a) memory means for storing, prior to the flight,

(i) known signal characteristics including signal frequencies, of the known signal emitters,

(ii) known geographical locations of the known signal emitters, and (iii) selection data for selecting signal characteristics and geographical locations of said unknown signal emitters which are optimum for locating the position of the reflector,

(b) means, responsive to said first signal output, for comparing the characteristics and locations of the received signals with the signal characteristics and locations of the known signal emitters, so as to identify the known received signals along the route of flight,

(c) means, responsive to said first signal output, for comparing the characteristics and locations of the unknown signal emitters with the selection data so as to select at least one unknown signal emitter for locating the position of the reflector,

(d) means for comparing the identified known signals with the selected unknown signal and for selecting the optimum signal therefrom based on their relative signal qualities including signal strength and freedom from clutter;

c. third processing means including

(1) means for determining a time interval between receipt of the first reflected signal component and the second nonreflected signal component, and

(2) means, responsive to the determined time interval, for defining a length of an electromagnetic signal path of the first signal component.

2. The apparatus as set forth in claim 1 wherein said geographical location determining means includes:

a. means for determining a range between said receiver and said signal emitter; and

b. means for determining an angle of arrival of said reflected signal component.

3. The apparatus as set forth in claim 2 wherein the length of said electromagnetic signal path is defined as a path extending from said selected signal emitter via said reflector to said receiver.

4. The apparatus as set forth in claim 1 additionally comprising display means for generating a symbolic display of said position of said reflector and said selected signal emitter relative to said position of said receiver.

5. The apparatus as set forth in claim 1 wherein said range determining means includes:

a. interferometer means for measuring a time delay between receipt of said second non-reflected signal component at spaced apart antenna locations; and

b. means for calculating said range as a function of said time delay and said angle of arrival of said non-reflected signal component.

6. The apparatus as set forth in claim 1 wherein said third processing means includes signal discrimination means for determining said time interval between receipt of said first component when said first component contains unwanted signals, and receipt of said second component, said signal discrimination means including means for processing said first component and said second component to generate an equivalent cross-correlation output which has a maxima at a time corresponding to said time interval.

7. The apparatus as set forth in claim 6 wherein said equivalent cross-correlation output is obtained by processing said first and second components at matched filter means.

8. The apparatus as set forth in claim 7 wherein said equivalent cross-correlation output is obtained by processing said first and second components at cross-correlation means.

9. The apparatus as set forth in claim 1 wherein said third processing means includes a signal discrimination means for determining said time interval when said first component contains clutter signals, said signal discrimination means including:

a. means for cross-correlating said first component with said second component at selected delay intervals, and for generating an output indicative of each of said cross-correlations; and

b. means for detecting a maximum of said cross-correlation outputs and for providing a second output of said selected delay interval which corresponds to said cross-correlation maximum in a manner that said second output is indicative of said time interval between receipt of said first signal component and said second signal component.

10. The apparatus as set forth in claim 9 wherein said received signals include a non-coherent carrier component.

11. The apparatus as set forth in claim 10 wherein said cross-correlation is defined by the equation:

##EQU6## where τ

=the selected delay interval between the first signal component S_R (t) and the second signal component S_D (t), C_L (t)=the clutter signal, T=an integration time to process a selected number of signal pulses, and S_C (τ

,t) is the cross-correlation output.

12. In a receiver aircraft on a predetermined route of flight, a method for locating a position of a reflector of electromagnetic signals relative to a receiver of said electromagnetic signals, said method comprising:

(a) processing a plurality of said received electromagnetic signals which are characterized by their generation from a plurality of signal emitters which are both unassociated from and non-cooperative with said receiver, and generating a first signal output of said processed signals, where said signal emitters include (i) known signal emitters having locations and signal characteristics which are known prior to said flight and which are known to be receivable along said route of flight, and (ii) unknown signal emitters having locations and signal characteristics which are not known prior to said flight and which are also receivable along said route of flight;

(b) selecting one of said received signals having a first component which is reflected from said reflector, and a second nonreflected component, in a manner that said selected signal is an optimum signal for locating the position of said reflector, said selecting being accommplished by;

(1) determining geographical locations of said signal emitters relative to the aircarft,

(2) utilizing computer means by;

a. storing in memory means of said computer means, prior to the flight, (i) known signal characteristics including signal frequencies, of the known signal emitters, (ii) known geographical locations of the known signal emitters, and (iii) selection data for selecting signal characteristics and geographical locations of said unknown signal emitters which are optimum for locating the position of the reflector,

b. in response to said first signal output, comparing the characteristics and locations of the received signals with the signal characteristics and locations of the known signal emitters, so as to identify the known received signals along the route of flight,

c. in response to said first signal output, comparing the characteristics and locations of the unknown signal emitters with the selection data and selecting at least one unknown signal emitter for locating the position of the reflector,

d. comparing the identified known signals with the selected unknown signal and selecting the optimum signal therefrom based on their relative signal qualities including signal strength and freedom from clutter;

(c) determining a time interval between receipt of the first reflected signal component and the second nonreflected signal component of said selected signal, and

(d) in response to the determined time interval, defining a length of an electromagnetic signal path of the first signal component of said selected signal.

13. The method as set forth in claim 12 additionally comprising the steps of:

(a) determining a range between the receiver and the signal emitter of the selected signal;

(b) determining an angle of arrival of the first reflected signal component of the selected signal; and

(c) defining a geographical location of the reflector relative to the receiver in response to the determined time interval, the determined range, and the determined angle of arrival of the first reflected signal component of the selected signal.

14. The method as set forth in claim 13 additionally comprising the steps of:

(a) identifying the characteristics of the received signals and a location of each of the signal emitters; and

(b) selecting the optimum signal on the basis of (i) the selected signal having optimum signal characteristics for locating the position of the reflector, and (ii) the emitter of the selected signal occupying an optimum location for generating signals to locate the position of the reflector.

15. The method as set forth in claim 12 additionally comprising the step of determining the time interval between receipt of the first component and receipt of the second component when the first component contains unwanted signals by processing the first component and the second component to generate an equivalent cross-correlation output which has a maxima at a time corresponding to the time interval between receipt of the first component and the second component.

16. The method as set forth in claim 15 additionally comprising the step of determining the time interval by discriminating the cross-correlation output from the unwanted signals by means of a frequency difference between the cross-correlation output and the unwanted signals.

17. The method as set forth in claim 12 additionally comprising the step of determining the time interval between receipt of the first component when the first component contains unwanted signals, and receipt of the second component by:

(a) cross-correlating the first component with the second component at selected delay intervals, and generating an output indicative of each of the cross-correlations; and

(b) detecting a maximum of the cross-correlation outputs and providing a second output of the selected delay interval which corresponds to the cross-correlation maximum in a manner that the second output is indicative of the time interval between receipt of the first signal component and the second signal component.