Precision landing system

• US 5,017,930 A
• Filed: 01/25/1990
• Issued: 05/21/1991
• Est. Priority Date: 01/25/1990
• Status: Expired due to Term

• Current Assignee: Integrated Aviation Solutions, Inc.
• Original Assignee: John R. Stoltz
• Inventors: Clawson, Carl W., Stoltz, John R.
• Primary Examiner(s): Blum, Theodore M.
• Application Number:
  US07/470,643
• Time in Patent Office: 481 Days
• Field of Search: 342/410, 342/411, 342/412, 342/413, 342/463, 342/465, 342/33, 342/47, 364/451
• US Class Current: 342/465
• CPC Class Codes: G01S 13/74 Systems using reradiation of radio waves, e.g. secondary radar systems; Analogous systems
• CPC Class Codes: G01S 5/0009 Transmission of position information to remote stations involving assistance data G01S5/0236
• CPC Class Codes: G01S 5/14 Determining absolute distances from a plurality of spaced points of known location

Abstract

A precision aircraft landing system comprising at least four receivers which are located at different predetermined positions. Each receiver includes a precision timer for measuring the timer interval between the receiver'"'"'s detection of an interrogation signal and a reply signal from a transponder onboard the aircraft. The system also includes a central processing unit (computer) at a base station which collects the time measurements from the receivers, and calculates the location of the aircraft. Because more than three independent measurements are used, the base station can compute not only the three-dimensional coordinates of the aircraft, but also the transponder reply time. Preferably estimation filtering calculations, such as Kalman filtering, are used to improve the accuracy. The aircraft'"'"'s position is compared with a mathematical description of a desired approach path, and the position error is then communicated to the aircraft. Any desired approach path than can be mathematically represented may be used in the system, including paths having curves, steps and segments.

Claims

1. A precision landing system for guiding an aircraft along a predetermined approach path within operable range of a ground-based interrogator which transmits an interrogation signal, said aircraft having onboard a transponder which transmits a transponder reply signal in response to receiving said interrogation signal, said system comprising:

(a) at least four ground-based receiver, each of said receivers being positioned at a predetermined position and comprising

(i) means for receiving said interrogation signal,

(ii) means for receiving said transponder reply signal, and

(iii) means for determining an elapsed time between receiving said interrogation signal and receiving said transponder reply signal;

(b) a computer comprising

(i) means for receiving said respective elapsed times from said respective receivers,

(ii) means for calculating from said respective elapsed times a position of said aircraft,

(iii) for comparing said position with said predetermined approach path, resulting in the determination of a position error; and

(c) means for communicating said position error to said aircraft.

2. The precision landing system of claim 1 wherein all of said receivers are contained within a single, substantially horizontal, geometric plane.

3. The precision landing system of claim 1 wherein said means for calculating includes an estimation filter.

4. The precision landing system of claim 3 wherein said estimation filter is a Kalman filter.

5. A precision landing system for guiding an aircraft along a predetermined approach path, said aircraft having onboard a transponder which transmits a transponder reply signal in response to receiving an interrogation signal from a ground-based transmitter, said system comprising:

(a) ground-based interrogation means for transmitting an interrogation signal;

(b) at least four ground-based receivers, each of said receivers being positioned at a predetermined position and comprising

(i) means for receiving said interrogation signal,

(ii) means for receiving said transponder reply signal, and

(iii) means for determining an elapsed time between receiving said interrogation signal and receiving said transponder reply signal;

(c) a computer comprising

(i) means for receiving said respective elapsed times from said respective receivers,

(ii) means for calculating from said respective elapsed times a position of said aircraft,

(iii) means for comparing said position with said predetermined approach path, resulting in the determination of a position error; and

(d) means for communicating said position error to said aircraft.

6. A precision landing system for guiding an aircraft along a predetermined approach path, comprising:

(a) ground-based interrogation means for transmitting an interrogation signal;

(b) transponder means onboard said aircraft for receiving said interrogation signal, and, in response, transmitting a transponder reply signal;

(c) at least four ground-based receivers, each of said receivers being positioned at a predetermined position and comprising

(i) means for receiving said interrogation signal,

(ii) means for receiving said transponder reply signal, and

(iii) means for determining an elapsed time between receiving said interrogation signal and receiving said transponder reply signal;

(d) a computer comprising

(i) means for receiving said respective elapsed times from said respective receivers,

(ii) means for calculating from said respective elapsed times a position of said aircraft,

(iii) means for comparing said position with said predetermined approach path, resulting in the determination of a position error; and

(e) means for communicating said position error to said aircraft.

7. A precision landing system for guiding an aircraft along a predetermined approach path, said aircraft having onboard a transponder which transmits an transponder reply signal, said system comprising:

(a) at least four ground-based receivers, each of said receivers being positioned at a predetermined position and comprising

(i) means for receiving said transponder reply signal, and

(ii) timer means for determining an arrival time corresponding to the receiving of said transponder reply signal;

(b) means for synchronizing said timer means of each of said receivers;

(c) a ground-based computer comprising

(i) means for receiving signals representing said respective arrival times from said respective receivers,

(ii) means for calculating, from said signals representing said respective arrival times, a position of said aircraft, and

(iii) means for comparing said calculated position with said predetermined approach path, resulting in the determination of a position error; and

(d) means for communicating said position error to said aircraft.

8. The precision landing system of claim 7 wherein said means for synchronizing said timer means includes means within each said receiver for receiving a synchronization signal.

9. The precision landing system of claim 8 wherein said means for synchronizing said timer means includes means for receiving an interrogation signal transmitted by an interrogator.

10. The precision landing system of claim 7 wherein all of said receivers are contained within a single, substantially horizontal, geometric plane.

11. The precision landing system of claim 7 wherein said means for calculating includes an estimation filter.

12. The precision landing system of claim 7 wherein said estimation filter is a Kalman filter.

13. The precision landing system of claim 7 wherein said means for communicating said position error transits a signal received by an ILS instrument on board said aircraft.

14. A precision landing system for guiding an aircraft along a predetermined approach path within operable range of a ground-based interrogator which transmits an interrogation signal, said aircraft having onboard a transponder which transmits a transponder reply signal in response to receiving said interrogation signal, said system comprising:

(a) at least three ground-based receivers, each of said receivers being positioned at a predetermined position and comprising

(i) means for receiving said transponder reply signal, and

(ii) timer means for determining an arrival time corresponding to said receiving of said transponder reply signal;

(b) means for synchronizing said timer means of each of said receivers;

(c) a computer comprising

(i) means for receiving signals representing said respective arrival times from said respective receivers,

(ii) means for calculating from said signals representing said respective arrival times a position of said aircraft, said means for calculating including an estimation filter, and

(iii) means for comparing said calculated position with said predetermined approach path, resulting in the determination of a position error; and

(d) means for communicating said position error to said aircraft.

15. The precision landing system of claim 14 wherein said means for synchronizing said timer means includes means within each receiver for receiving a synchronization signal.

16. The precision landing system of claim 15 wherein said means for synchronizing said timer means includes means for receiving said interrogation signal.