Interferomeric synthetic aperture radar altimeter

• US 6,025,800 A
• Filed: 10/02/1998
• Issued: 02/15/2000
• Est. Priority Date: 10/02/1998
• Status: Expired due to Term

• Current Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Original Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Inventors: Hager, James R.
• Primary Examiner(s): Tarcza, Thomas H.
• Assistant Examiner(s): PHAN, DAO LINDA
• Application Number:
  US09/165,624
• Time in Patent Office: 501 Days
• Field of Search: 342/25, 342/450, 342/457, 342/462, 342/465, 342/463
• US Class Current: 342/450
• CPC Class Codes: G01C 5/005 altimeters for aircraft G01C5/02, G01C5/06 take precedence
• CPC Class Codes: G01S 13/18 wherein range gates are used
• CPC Class Codes: G01S 13/42 Simultaneous measurement of distance and other co-ordinates indirect measurement G01S13/46
• CPC Class Codes: G01S 13/524 based upon the phase or frequency shift resulting from movement of objects, with reference to the transmitted signals, e.g. coherent MTi
• CPC Class Codes: G01S 13/70 for range tracking only
• CPC Class Codes: G01S 13/882 for altimeters measuring height using barometric means G01C5/06
• CPC Class Codes: G01S 13/935 for terrain-avoidance
• CPC Class Codes: G01S 3/48 the waves arriving at the antennas being continuous or intermittent and the phase difference of signals derived therefrom being measured
• CPC Class Codes: G01S 7/292 Extracting wanted echo-signals

Abstract

Aircraft position determination system includes a transmitter to transmit a signal, and two receivers to receive the transmitted signal reflected from the terrain below the aircraft, and a phase comparison apparatus operating from the two receiver'"'"'s inputs. A processor determines position based on the output from the phase comparison apparatus.

Claims

1. System located on an aircraft for determining the position of the aircraft, comprising:

transmitter located on the aircraft transmitting a transmit signal to terrain below the aircraft which will be reflected;

first receiver located on the aircraft receiving a first reflected signal reflected back to the aircraft upon contact with terrain in a first area wherein the first area is terrain ahead of the aircraft;

second receiver located on the aircraft receiving a second reflected signal reflected back to the aircraft upon contact with terrain in a second area wherein the second area is the terrain the aircraft is currently over wherein the first and second receivers are separated by a separation distance; and

apparatus, located on the aircraft for determining position of the aircraft based on information received from the signal reflected back to the aircraft wherein the apparatus for determining first determines an approximate range to a highest point in the first area and an accurate range to a highest point in the second area.

2. The system of claim 1 wherein the approximate range is stored in a memory.

3. The system of claim 2 wherein the accurate range is determined by using the approximate range stored in memory to perform a range analysis to determine the accurate range.

4. The system of claim 3 wherein the first receiver and the second receiver receive a signal transmitted, by the transmitter, to the highest point in the second area to determine a first range and a second range and calculate the position of the aircraft to the highest point based on the difference between the first range and the second range, and the separation distance.

5. The system of claim 1 wherein the determining apparatus determines the altitude of the aircraft from the information received from the signal reflected back to the aircraft.

6. The system of claim 1 wherein the apparatus for determining compares the position of the aircraft, in regards to the highest points, to a map and determines a map position of the aircraft.

7. The system of claim 1 wherein both receivers further comprise:

an antenna;

a range gate;

a Doppler filter; and

a tracker.

8. The system of claim 1 wherein the apparatus for determining further comprises:

a phase comparitor; and

a position processor.

9. System, located on the aircraft for determining the position of an aircraft, comprising:

transmitter located on the aircraft transmitting a signal to terrain below the aircraft;

receiver located on the aircraft determining a highest point in the terrain below and receiving a plurality of signals reflected back to the aircraft from the highest point; and

an apparatus located on the aircraft comparing information received from the signals reflected back to the aircraft and processing the information to determine the position of the aircraft.

10. The system of claim 9 wherein the comparing apparatus determines the altitude of the aircraft from the information received from the signal reflected back to the aircraft.

11. The system of claim 9 wherein the apparatus for determining compares the position of the aircraft, in regards to the highest points, to a map and determines a map position of the aircraft.

12. The system of claim 9 wherein the apparatus for comparing further comprises:

a phase comparitor; and

a position processor.

13. The system of claim 9 wherein the receiver further comprises

a first antenna;

a second antenna;

a range gate;

a Doppler filter; and

a tracker.

14. The system of claim 13 wherein the signals received represent a first range received by the first antenna and a second range received by the second antenna and the comparing apparatus calculates the position of the aircraft to the highest point based on the difference between the first range and the second range and distance between the first antenna and the second antenna.