Differential ground station repeater

• US 5,852,412 A
• Filed: 10/30/1995
• Issued: 12/22/1998
• Est. Priority Date: 10/30/1995
• Status: Expired due to Term

• Current Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Original Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Inventors: Stangeland, Rodney L.
• Primary Examiner(s): Hofsass, Jeffrey
• Assistant Examiner(s): Lee, Benjamin C.
• Application Number:
  US08/550,488
• Time in Patent Office: 1,149 Days
• Field of Search: 340/988, 340/945, 342/357, 364/449, 364/460, 701/66, 701/215
• 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 global position system wherein a DGPS ground station encodes signals from a plurality of satellites and transmits the encoded signal with satellite-specific pseudo range error signals and a ground station repeaters located remote from the DGPS ground station to receive the encoded signal and retransmit it to an airborne object.

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 at a first known location and including a receiver to receive the information from the satellites and to produce an output signal indicative of the errors;

means located proximate the ground receiving station for encoding the output signal in accordance with requirements for data transmission between the ground receiving station and the object;

a first transmitter located proximate the ground receiving station for broadcasting the encoded output signal to the object; and

a second transmitter located at a second position remote from the receiving station to receive the broadcast encoded output signal from the first transmitter and to retransmit it to the object.

2. Apparatus according to claim 1 wherein the first transmitter transmits the encoded output signal in a first time slot and the second transmitter transmits the encoded output signal in a second time slot.

3. Apparatus according to claim 1 wherein the object is an aircraft and the first and second transmitters are located proximate a first airport with the first and second positions chosen to provide the error information to the aircraft free of obscuration by interfering structures.

4. 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.

5. Apparatus according to claim 1 wherein the second transmitter includes a demodulator to demodulate the encoded output signal, a time delay to delay the demodulated encoded output signal into the second time slot and a modulator to remodulate the demodulated delayed encoded output signal for transmission to the object.

6. Apparatus according to claim 1 further including a third transmitter located remote from the ground station to receive the encoded output signal from the first transmitter and transmit it to the object.

7. Apparatus according to claim 6 wherein the third transmitter transmits the encoded output signal to the object in a third time slot.

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 is encoded for transmission to aircraft within transmission range of the ground station, an improvement permitting a single encoding of the processed information comprising the steps of:

A. connecting the ground station to a first transmitter located proximate the ground station to receive the processed and encoded information and transmit it to the aircraft in a first time slot at a frequency;

and

B. transmitting the processed and encoded information from the first transmitter to a second transmitter located remote from the grounds station for transmission to the aircraft in a second time slot a the same frequency.

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

10. 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 to verify the transmissions to the aircraft.

11. The process of claim 8 wherein Step B includes the steps of:

B1. demodulating the signal from the first transmitter;

B2. time delaying the demodulated signal to the second time slot; and

B3. remodulating the demodulated time delayed signal for transmission to the aircraft in the second time slot.

12. A multiple access transmission system for use in communicating common information to an object from multiple transmitters broadcasting in different time slots, comprising:

a ground receiving station at a first known location operable to produce an encoded output signal in accordance with requirements for data transmission between the ground receiving station and the object;

a first transmitter located proximate the ground receiving station for broadcasting the encoded output signal to the object; and

a second transmitter located at a second position remote from the receiving station to receive the broadcast encoded output signal from the first transmitter, to delay it into a proper time slot and to retransmit it to the object wherein the first transmitter transmits the encoded output signal in a first time slot at a frequency and the second transmitter transmits the encoded output signal in the proper time slot at the same frequency. pg,11

13. Apparatus according to claim 12 wherein the ground station is a DGPS receiver and processor which is operable to receive signals and the encoded output signal is indicative of satellite specific pseudo range error signals.

14. Apparatus according to claim 12 wherein the object is an aircraft.

15. Apparatus according to claim 14 wherein the aircraft includes means for receiving the encoded signal and reconstituting it.