Satellite radiodetermination

• US 6,040,798 A
• Filed: 10/15/1996
• Issued: 03/21/2000
• Est. Priority Date: 10/24/1995
• Status: Expired due to Term

• Current Assignee: Inmarsat Global Limited (Inmarsat PLC)
• Original Assignee: International Mobile Satellite Organization
• Inventors: Ryan, Fintan Richard, Kinal, George Vladimir, Nagle, James Robert II, Soddu, Claudio
• Primary Examiner(s): Tarcza, Thomas H.
• Assistant Examiner(s): PHAN, DAO LINDA
• Application Number:
  US08/730,208
• Time in Patent Office: 1,253 Days
• Field of Search: 342/352, 342/357.1, 342/357.01, 342/453, 701/213, 701/223
• US Class Current: 342/357.21
• CPC Class Codes: G01S 19/02 Details of the space or ground control segments
• CPC Class Codes: G01S 19/071 DGPS corrections
• CPC Class Codes: G01S 19/072 Ionosphere corrections
• CPC Class Codes: G01S 19/235 Calibration of receiver components
• CPC Class Codes: G01S 19/40 Correcting position, velocity or attitude
• CPC Class Codes: G01S 19/41 Differential correction, e.g. DGPS [differential GPS]
• CPC Class Codes: G01S 5/0009 Transmission of position information to remote stations involving assistance data G01S5/0236
• CPC Class Codes: G01S 5/009 Transmission of differential positioning data to mobile

Abstract

A satellite radiodetermination system comprises global navigation service (GNSS) satellites 2 such as GPS satellites, which generate GNSS ranging signals R_n, geostationary satellites 6 which retransmit ranging signals R_g generated at a navigation land earth station (NLES) 8, including augmentation data A, and medium earth orbit (MEO) satellites 10 which generate ranging signals R_m including regional augmentation data RA transmitted from a satellite access node (SAN) 14. The regional augmentation data RA is supplied by regional augmentation systems 21a, 21b.

A navigation receiver 11 receives the ranging signals R_g, R_m, R_n and calculates ionospheric delay values for those ranging signals which are provided on dual frequencies. Using these ionospheric delay values, and optionally the regional augmentation data RA and the augmentation data A, the navigation receiver estimates ionospheric delay values for those ranging signals which are provided on single frequencies. The navigation receiver uses the ranging signals, corrected for ionospheric delay and errors indicated by the augmentation data A and regional augmentation data RA, to calculate position and time accurately.

Claims

1. Satellite radiodetermination apparatus, comprising:

a radio receiver for receiving a multiple frequency ranging signal from a first satellite and a further ranging signal from a second satellite, the radio receiver including;

deriving means for deriving first ionospheric delay data from said multiple frequency ranging signal; and

estimating means for estimating second ionospheric delay data for the further ranging signal on the basis of said first ionospheric delay data.

2. Apparatus as claimed in claim 1, further comprising data receiving means for receiving ionospheric data, said estimating means being operable to estimate the second ionospheric delay data additionally on the basis of said ionospheric data.

3. Apparatus as claimed in claim 2, wherein said data receiving means is arranged to receive said ionospheric data from a satellite.

4. Apparatus as claimed in claim 2 or 3, wherein said ionospheric data represents a plurality of ionospheric delay values corresponding to a plurality of spatially separated points.

5. Apparatus as claimed in claim 1, wherein said estimating means includes modelling means for generating a model of spatial variation of ionospheric delay on the basis of said first ionospheric delay data, said estimating means being operable to estimate said second ionospheric delay data on the basis of said model.

6. Apparatus as claimed in claim 5, wherein said modelling means is operable to generate said model on the basis of said ionospheric data.

7. Apparatus as claimed in claim 5, wherein said model comprises a function which is variable in accordance with one or more parameters, said modelling means being arranged to calculate said one or more parameters such that said function is fitted to said first ionospheric delay data.

8. Apparatus as claimed in claim 7, wherein said modelling means is arranged to calculate said one or more parameters such that said function is additionally fitted to said ionospheric data.

9. A method of satellite radiodetermination, comprising receiving at a receiver a multiple frequency ranging signal from a first satellite;

receiving at the receiver a further ranging signal from a second satellite, deriving at the receive first ionospheric delay data from said multiple frequency ranging signal; and

estimating at the receiver second ionospheric delay data for the further ranging signal on the basis of said first ionospheric delay data.