Differential ground station repeater

• US 5,608,393 A
• Filed: 03/07/1995
• Issued: 03/04/1997
• Est. Priority Date: 03/07/1995
• Status: Expired due to Term

• Current Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Original Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Inventors: Hartman, Randolph G.
• Primary Examiner(s): Hofsass, Jeffery
• Assistant Examiner(s): Lee, Benjamin C.
• Application Number:
  US08/400,168
• Time in Patent Office: 728 Days
• Field of Search: 340/988, 340/947, 364/428, 364/429, 364/660, 342/357, 342/358, 342/33, 342/34, 342/35, 342/457, 342/450, 342/463, 244/114 R, 455/7, 455/11.1, 455/9, 455/51.1
• US Class Current: 340/988
• CPC Class Codes: G01S 19/071 DGPS corrections
• CPC Class Codes: G01S 5/009 Transmission of differential positioning data to mobile

Abstract

A differential ground station repeater in which a plurality of transmitters are utilized to relay information to an aircraft from a single ground station situated to receive satellite information and to transmit the satellite and other information to the plurality of correction transmitters in which the transmitters utilize a single frequency but transmit at different described sub-time slots so that the aircraft may utilize the signal of any of the transmitters it may be receiving signals.

Claims

1. A differential global position system for use in determining one or more parameters of an object with respect to earth by use of information transmitted to the object from a plurality of satellites which information may contain errors due to path distortions, comprising:

a ground receiving station fixed to earth at a known location and including a receiver to receive the information from the satellites and a microprocessor to determine the error information due to path distortion;

first transmitter means located at a first position remote from the receiver and connected thereto to receiver the error information and to transmit it to the object in a transmission at a first frequency with a first characteristic; and

second transmitter means located at a second position remote from the first transmitter means and the receiver and connected to the receiver to receive the error information and to transmit it to the object in a transmission at the first frequency with a second characteristic distinguishable from the first characteristic, so that the transmissions are individually distinguishable.

2. Apparatus according to claim 1 further including a data link wrap around receiving antenna positioned to receive the transmissions from the first and second transmitters and connected to the ground station to feedback the transmission information thereto.

3. Apparatus according to claim 1 wherein the first and second transmitter means transmit the error information to the object at the same transmission frequency but in different time slots.

4. Apparatus according to claim 3 wherein the object is an aircraft having a receiver, the first and second transmitter means are located proximate a first airport and the first and second positions are chosen to provide the error information to the aircraft free of obscuration by interfering structures.

5. Apparatus according to claim 3 wherein the parameters include satellite specific pseudo range error, and other airport data for use by the aircraft in landing at the airport and taxiing to its terminal.

6. Apparatus according to claim 3 wherein the object is an aircraft having a receiver and the first and second transmitter means are located at separate airports within a normal transmission range of each other, the error information being provided at different times so that the aircraft can determine the location of the transmitter without using multiple frequencies.

7. Apparatus according to claim 6 wherein the parameters include range error, rate of range error and other airport data for use by the aircraft in landing at a chosen one of the airports and taxing to its terminal.

8. A process for use with a differential global position system in which information from a plurality of satellites is received at a ground station and processed to determine any errors therein and the processed information being transmitted to aircraft within transmission range of the ground station, an improvement permitting transmission of the processed information over a single frequency from several locations remote from the ground station and from each other all within the transmission range comprising the steps of:

A. connecting a single ground station to a plurality of transmitters, at least one of which is located at each of the remote locations;

B. assigning to each transmitter a separate time slot for the transmission of the processed information; and

C. causing each transmitter to transmit the processed information at the single frequency only during its assigned time slot.

9. The process of claim 8 wherein the transmission of the processed information by the transmitters during each time slot is periodically repeated.

10. The process of claim 8 further including the step of positioning the transmitters so that an unobscured obscured transmission to the aircraft is possible from at least one transmitter at all aircraft positions.

11. The process of claim 8 further including the step of monitoring the transmissions of the plurality of transmitters and feeding the transmissions back to the ground station.

12. The process of claim 8 where the aircraft can receive the corrections from two transmitters on a single frequency so as to maintain the signal when one or the other transmitter is masked or interfered with.

13. The process of claim 8 where the aircraft can receive the corrections from two transmitters on a single frequency so as to maintain the signal when a highly reliable link must remain active as when used in CAT 111 B approaches.