Passive range estimating engagement system and method

• US 9,212,869 B1
• Filed: 03/14/2013
• Issued: 12/15/2015
• Est. Priority Date: 03/14/2013
• Status: Active Grant

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Inventors: Boardman, Jonathan A., Boka, Jeffrey B., Mookerjee, Purusottam, Patel, Naresh R.
• Primary Examiner(s): Bythrow, Peter
• Application Number:
  US13/803,907
• Time in Patent Office: 1,006 Days
• Field of Search: 342/52, 342/53, 342 89- 97, 342/175, 342/189
• US Class Current: 1/1
• CPC Class Codes: F41G 7/2206 using a remote control station
• CPC Class Codes: F41G 7/2253 Passive homing systems, i.e. comprising a receiver and do not requiring an active illumination of the target
• CPC Class Codes: F41G 7/2293 using electromagnetic waves other than radio waves
• CPC Class Codes: F41H 11/02 Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems cartridges or missiles for producing smoke or for dispensing radar chaff or infrared material F42B5/15, F42B12/48, F42B12/70; informative reference: details of radar or sonar systems G01S7/00; jamming or electronic countermeasures G01S7/38, G01S7/495, H04K3/00
• CPC Class Codes: G01S 13/66 Radar-tracking systems; Analogous systems
• CPC Class Codes: G01S 13/72 for two-dimensional tracking, e.g. combination of angle and range tracking, track-while-scan radar
• CPC Class Codes: G01S 13/726 Multiple target tracking
• CPC Class Codes: G01S 13/86 Combinations of radar systems with non-radar systems, e.g. sonar, direction finder
• CPC Class Codes: G01S 13/883 for missile homing, autodirectors missile guidance systems F41G7/22
• CPC Class Codes: G01S 3/783 using amplitude comparison of signals derived from static detectors or detector systems
• CPC Class Codes: G01S 5/0294 Trajectory determination or predictive filtering, e.g. target tracking or Kalman filtering
• CPC Class Codes: G01S 7/292 Extracting wanted echo-signals
• CPC Class Codes: G01S 7/2923 based on data belonging to a number of consecutive radar periods
• CPC Class Codes: G01S 7/295 Means for transforming co-ordinates or for evaluating data, e.g. using computers

Abstract

A system and method for determining a 3-dimensional target position and velocity using 2-dimensional IR sensor angular measurements for objects travelling in a ballistic manner within an IR sensor'"'"'s field of view (FOV). Resulting 3-dimensional states may be used to generate updated inputs for correlation and object selection to drive missile guidance and intercept operations.

Claims

1. A method for estimating range of an object of interest in a cloud of objects of lesser interest and travelling in a ballistic manner within the field of view of an IR sensor, the method comprising:

(a) receiving in an object selection and discrimination processor, RF sensor data associated with an object, the RF data including position and velocity data in a given coordinate frame;

(b) transforming in said object selection and discrimination processor, the RF sensor data from the given coordinate frame to an IR coordinate frame and subtracting the sensor location in the IR coordinate frame to generate an initial range measurement perpendicular to the IR sensor focal plane;

(c) receiving IR sensor data in said object selection and discrimination processor, associated with an object and generating an initial line of sight (LOS) vector in the IR coordinate frame;

(d) combining in said object selection and discrimination processor, the initial range measurement represented in the IR sensor focal plane with the initial line of sight (LOS) vector in the IR sensor coordinate frame to form an initial IR 3-D state estimate;

(e) initializing at least a 6-state estimation filter for providing a position estimate using the initial IR 3-D measurement represented in the IR sensor focal plane;

(f) receiving IR sensor data including IR angular measurements associated with an object and generating in said object selection and discrimination processor a line of sight (LOS) vector in the IR sensor coordinate frame;

(g) filtering using the at least 6-state estimation filter 3-D position and velocity estimates using the IR LOS measurements as inputs to generate in said object selection and discrimination processor, updated 3-D position and velocity state estimates; and

(h) comparing in said selection discrimination processor, said updated 3-D position and velocity state estimates with a threshold value, and repeating steps (f) and (g) over a given time interval until said threshold value is reached.

2. The method of claim 1, further comprising determining components of the IR sensor measurements in the sensor focal plane using a projection matrix.

3. The method of claim 2, further comprising rotating the LOS vector a given rotation amount to account for measurement errors.

4. The method of claim 1, further comprising updating covariance data of the object as sensed by the IR sensor based on said generated state estimates.

5. The method of claim 1, wherein said given coordinate frame is an Earth-Centered Inertial (ECI) coordinate frame.

6. The method of claim 1, wherein at least six state estimation filter comprises a Kalman filter.

7. The method of claim 1, wherein said steps (a)-(h) are performed at an interceptor missile including the IR sensor.

8. The method of claim 1, further comprising determining a range estimate based on the updated position and velocity estimates and providing as an output to a correlator.

9. The method of claim 1, further comprising determining a range uncertainty estimate based on the updated position and velocity estimates and providing as an output to a correlator.

19. The method of claim 1, wherein said threshold value corresponds to a predetermined target level of uncertainty associated with at least one of target range and position error.

10. A system for estimating range of an object of interest in a cloud of objects of lesser interest and travelling in a ballistic manner within the field of view of an IR sensor, comprising:

a processor configured to;

(a) receive RF sensor data associated with an object, the RF data including position and velocity data in a given coordinate frame;

(b) transform the RF sensor data from the given coordinate frame to an IR coordinate frame and subtract the sensor location in the IR coordinate frame to generate an initial range measurement perpendicular to the IR sensor focal plane;

(c) receive IR sensor data associated with an object and generate an initial line of sight (LOS) vector in the IR coordinate frame;

(d) combine the initial range measurement represented in the IR sensor focal plane with the initial line of sight (LOS) vector in the IR sensor coordinate frame to form an initial IR 3-D state estimate;

(e) initialize at least a 6-state estimation filter for providing a position estimate using the initial IR 3-D measurement represented in the IR sensor focal plane;

(f) receive IR sensor data including IR angular measurements associated with an object and generate a line of sight (LOS) vector in the IR sensor coordinate frame;

(g) generate updated 3-D position and velocity state estimates by filtering using the at least 6-state estimation filter 3-D position and velocity estimates using the IR LOS measurements as inputs; and

(h) compare said updated 3-D position and velocity state estimates with a threshold value corresponding to a predetermined uncertainty estimate, and repeat steps (f) and (g) over a given time interval until said threshold value is reached.

11. The system of claim 10, wherein the processor is further configured to receive IR sensor angular measurements of said object and determine components of the measurement in the sensor focal plane using a projection matrix.

12. The system of claim 11, wherein the processor is further configured to provide an offset to the determined LOS vector to account for measurement errors.

13. The system of claim 10, wherein the processor is further configured to update covariance data of the object as sensed by the IR sensor based on said generated state estimates.

14. The system of claim 10, wherein said given coordinate frame is an Earth-Centered Inertial (ECI) coordinate frame.

15. The system of claim 10, wherein the at least six state estimation filter comprises a Kalman filter.

16. The system of claim 10, wherein the processor is configured on an interceptor missile including the IR sensor.

17. The system of claim 10, wherein the processor is configured to determine a range estimate based on the updated position and velocity estimates and provide as an output to a correlator.

18. The system of claim 10, wherein the processor is configured to determine a range uncertainty estimate based on the updated position and velocity estimates and provide as an output to a correlator.

20. The system of claim 10, wherein said threshold value corresponds to a predetermined target level of uncertainty associated with at least one of target range and position error.