Site-specific doppler navigation system for back-up and verification of GPS

• US 6,593,875 B2
• Filed: 06/29/2001
• Issued: 07/15/2003
• Est. Priority Date: 06/29/2001
• Status: Active Grant

• Current Assignee: Information Systems Laboratories, Inc.
• Original Assignee: Information Systems Laboratories, Inc.
• Inventors: Bergin, Jameson, Carlos, John Don, Halsey, J. Doss
• Primary Examiner(s): Tarcza, Thomas H.
• Assistant Examiner(s): ALSOMIRI, ISAM A
• Application Number:
  US09/895,613
• Publication Number:
  US 20030102999A1
• Time in Patent Office: 746 Days
• Field of Search: 342/65, 342/64, 342/107, 342/108, 342/120, 342/121, 342/123
• US Class Current: 342/121
• CPC Class Codes: G01S 13/06 Systems determining position data of a target
• CPC Class Codes: G01S 13/522 using transmissions of interrupted pulse modulated waves
• CPC Class Codes: G01S 13/60 wherein the transmitter and receiver are mounted on the moving object, e.g. for determining ground speed, drift angle, ground track G01S13/64 takes precedence
• CPC Class Codes: G01S 13/86 Combinations of radar systems with non-radar systems, e.g. sonar, direction finder
• CPC Class Codes: G01S 13/87 Combinations of radar systems, e.g. primary radar and secondary radar
• CPC Class Codes: G01S 13/874 Combination of several systems for attitude determination in general G01C, control of attitude G05D1/49
• CPC Class Codes: G01S 19/15 Aircraft landing systems
• CPC Class Codes: G01S 19/23 Testing, monitoring, correcting or calibrating of receiver elements
• CPC Class Codes: G01S 19/48 by combining or switching between position solutions derived from the satellite radio beacon positioning system and position solutions derived from a further system
• CPC Class Codes: G01S 7/412 based on a comparison between measured values and known or stored values

Abstract

A system and method for identifying the position of an airborne platform on a flight path includes at least three radar transceivers that are directed along respective beam paths to generate return signals. Each of the return signals respectively indicate a speed and a direction of the platform relative to points on the surface of the earth. A computer uses the return signal to establish a ground speed, an altitude and a direction of flight for the platform. This information is then used to identify the position of the platform on its flight path. Additionally, the system can include a last known position, or a site-specific radar clutter model, to establish a start point for the platform. The computer can then calculate the position of the platform relative to the start point.

Claims

1. A system for identifying a position of an airborne platform on a flight path which comprises:

a radar means mounted on the platform for directing an “

n”

number of radar beams on respective predetermined paths toward the surface of the earth to generate an “

n”

number of return signals, wherein “

n”

is at least equal to three;

an electronic means connected with said radar means for using said “

n”

number of return signals to compute a ground speed, a direction of flight and an altitude for the platform to identify the position of the platform on its flight path; and

a computer means preprogrammed with site-specific radar clutter model data for matching with said return signals to establish a start point location on the flight path to determine a route of flight for the platform.

2. A system as recited in claim 1 wherein said radar means comprises:

a first transceiver for generating a first return signal indicative of a first speed and a first distance of the platform relative to a first point on the surface of the earth;

a second transceiver for generating a second return signal indicative of a second speed and a second distance of the platform relative to a second point on the surface of the earth; and

a third transceiver for generating a third return signal indicative of a third speed and a third distance of the platform relative to a third point on the surface of the earth.

3. A system as recited in claim 2 wherein said electronic means compares said first return signal, said second return signal and said third return signal to each other, to determine a ground speed, an altitude, and any change in the direction of flight for the platform, to therewith identify the position of the platform on its flight path.

4. A system as recited in claim 2 wherein said electronic means compares said first return signal, said second return signal and said third return signal to each other, to determine a slope for the surface of the earth relative to the flight path of the platform to indicate a preferred flight path for terrain avoidance.

5. A system as recited in claim 2 wherein said first transceiver and said second transceiver are pulse Doppler radars.

6. A system as recited in claim 5 wherein said third transceiver is a radar altimeter.

7. A system as recited in claim 1 further comprising means for individually directing each of said “

n”

number of radar beams, in sequence, along said respective predetermined paths.

8. A system as recited in claim 1 wherein said electronic means computes the position of the platform relative to the start point.

9. A system as recited in claim 8 wherein said site-specific radar clutter model data is derived from National Imagery and Mapping Agency (NIMA) Digital Terrain Elevation Data (DTED).

10. A system as recited in claim 9 further comprising means for matching said return signals with said site-specific radar clutter model to generate a terrain-avoidance alarm.

11. A system as recited in claim 1 wherein one said predetermined path is oriented forward and downward from the flight path at an angle α

and laterally therefrom at a positive angle β

, and further wherein another said predetermined path is oriented forward and downward from the flight path at the angle α and

laterally therefrom at a negative angle β

.

12. A system for identifying a position of an airborne platform on a flight path which comprises:

a radar means for detecting a projection of the flight path onto the surface of the earth, for determining a ground speed for the platform along the projection, and for establishing a vertical distance for the platform above the projection; and

a computer means preprogrammed with site-specific radar clutter model data for matching with data from said radar means to establish a start point location and for using the projection, the ground speed and the vertical distance to identify the position of the platform on its flight path and further, for using the start point location on the flight path to determine a route of flight for the airborne platform.

13. A system as recited in claim 12 wherein said radar means comprises:

a first transceiver mounted on the platform for directing a radar beam on a first path toward the surface of the earth to generate a first return signal, said first return signal being indicative of a first speed and a first distance of the platform relative to a first point on the surface of the earth;

a second transceiver mounted on the platform for directing a radar beam on a second path toward the surface of the earth to generate a second return signal, said second return signal being indicative of a second speed and a second distance of the platform relative to a second point on the surface of the earth; and

a third transceiver mounted on the platform for directing a radar beam on a third path toward the surface of the earth to generate a third return signal, said third return signal being indicative of a third speed and a third distance of the platform relative to a third point on the surface of the earth.

14. A system as recited in claim 13 wherein said computer means compares said first return signal, said second return signal and said third return signal to each other to establish the ground speed for the platform and the projection of the flight path onto the surface of the earth.

15. A system as recited in claim 14 wherein said first transceiver and said second transceiver are pulse Doppler radars and said third radar means is a radar altimeter.

16. A system as recited in claim 13 wherein said computer means compares said first return signal, said second return signal and said third return signal to each other, to determine a slope for the surface of the earth relative to the flight path of the platform to indicate a preferred flight path for terrain avoidance.

17. A system as recited in claim 13 wherein said predetermined path for said first transceiver is forward looking and is oriented downward from the flight path at an angle α

and away from the direction of flight at a positive angle β

, and further wherein said predetermined path for said second transceiver is forward looking and is oriented downward from the flight path at an angle α and

away from the direction of flight at a negative angle β

.

18. A method for identifying a position of an airborne platform on a flight path which comprises the steps of:

directing a first radar beam on a predetermined path to generate a first return signal, said first return signal being indicative of a first speed and a first distance of the platform relative to a first point on the surface of the earth;

directing a second radar beam on a predetermined path to generate a second return signal, said second return signal being indicative of a second speed and a second distance of the platform relative to a second point on the surface of the earth;

directing a third radar beam on a predetermined path to generate a third return signal, said third return signal being indicative of a third speed and a third distance of the platform relative to a third point on the surface of the earth;

comparing said first return signal, said second return signal and said third return signal to each other to establish a ground speed, an altitude, and a direction of flight for the platform;

matching said first return signal, said second return signal and said third return signal with preprogrammed site-specific radar clutter model data to establish a start point location for the platform;

calculating the position of the platform relative to the start point location; and

using the start point location on the flight path to determine a route of flight for the airborne platform.

19. A method as recited in claim 18 wherein said comparing step includes determining a slope for the surface of the earth relative to the flight path of the platform to indicate a preferred flight path for terrain avoidance.