Method and apparatus for Doppler compensation in a satellite communications system

• US 6,008,758 A
• Filed: 05/26/1998
• Issued: 12/28/1999
• Est. Priority Date: 05/26/1998
• Status: Expired due to Term

• Current Assignee: Rockwell Collins, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Rockwell International Corporation
• Inventors: Campbell, Thomas B.
• Primary Examiner(s): Hellner, Mark
• Application Number:
  US09/084,747
• Time in Patent Office: 581 Days
• Field of Search: 342/352, 342/358, 342/418, 455/12.1
• US Class Current: 342/358
• CPC Class Codes: H04B 7/18508 with satellite system used as relay, i.e. aeronautical mobile satellite service
• CPC Class Codes: H04B 7/208 Frequency-division multiple access [FDMA]

Abstract

A method and apparatus for Doppler compensation in a satellite communications system such as Inmarsat'"'"'s SATCOM network are disclosed. An aircraft terminal provides satellite communications services in one of several user-selectable modes including a circuit-mode services only mode and other modes providing some data packet services. The terminal includes multiple channel units coupled to a processing circuit. The channel units communicate radio signals via data or circuit channels between the aircraft and a satellite. Each channel unit can receive a channel input transmitted at a known frequency, and measure its frequency. Each channel unit can also transmit a channel output at an adjustable frequency. Each channel unit is operated as a circuit channel when circuit-mode services only is selected. Doppler shift is measured using the difference between the measured and known transmitted frequencies of at least one channel input. The measured Doppler shift is used to determine a Doppler correction for each transmission, and the correction is applied to adjust the frequency of each transmitted channel output to maintain the transmissions within an error budget.

Claims

1. An Aircraft Earth Station (AES) terminal for satellite communications capable of use in circuit-mode services only applications, the terminal comprising:

a plurality of channel units, each channel unit configured to receive a circuit channel input having a known transmitted frequency and to transmit a circuit channel output at an adjustable transmit frequency, wherein each channel unit can measure the frequency of its received circuit channel input and can adjust the frequency of its transmitted circuit channel output; and

a processing circuit coupled to the plurality of channel units, the processing circuit configured to measure Doppler shift based upon a difference between the measured frequency and the known transmitted frequency of at least one of the circuit channel inputs, to determine a Doppler correction for each transmitted circuit channel output based on the measured Doppler shift, and to apply the Doppler correction to adjust the frequency of each transmitted circuit channel output to correct for Doppler shift.

2. The terminal of claim 1, wherein each channel unit receives its circuit channel input by searching for, acquiring, and locking onto its circuit channel input.

3. The terminal of claim 2, wherein the processing circuit measures Doppler shift of more than one circuit channel input, and processes the Doppler measurements to generate a single measured Doppler shift which is used to determine the Doppler correction for each transmission.

4. The terminal of claim 3, wherein the Doppler measurements are processed by dropping the highest and lowest measurements and averaging the other measurements.

5. The terminal of claim 1, wherein the Doppler correction for each transmitted circuit channel output is based upon the ratio of the received circuit channel frequency to each transmitted circuit channel frequency.

6. The terminal of claim 5, wherein the Doppler correction is applied to adjust the frequency of each circuit channel output in the opposite direction from the Doppler shift of the received circuit channel input.

7. The terminal of claim 1, wherein the measured Doppler shift is used to determine the Doppler correction for each transmission for only a limited time period.

8. The terminal of claim 7, wherein, after the limited time period expires without a new valid Doppler measurement, one of the channel units is reconfigured to operate as a data channel to receive a P Channel input and to measure Doppler shift via the P Channel input.

9. A SATCOM terminal for providing communications services between an aircraft and a satellite, the SATCOM terminal having a plurality of selectable configuration options, one of the configuration options adapted for providing circuit-mode services only and at least one of the other configuration options adapted for providing at least some data packet services, the terminal comprising:

a plurality of channel units for communicating signals via channels between the aircraft and satellite, each channel unit operable as a data or circuit channel, each channel unit configured to receive a channel input having a known transmitted frequency and to transmit a channel output at an adjustable transmit frequency, wherein each channel unit can measure the frequency of its received channel input and can adjust the frequency of its transmitted channel output; and

a processing circuit coupled to the plurality of channel units, the processing circuit configured, when circuit-mode services only is selected, to operate each of the plurality of channel units as a circuit channel, to measure Doppler shift based upon a difference between the measured frequency and known transmitted frequency of at least one of the channel inputs, to determine a Doppler correction for each transmitted channel output based on the measured Doppler shift, and to apply the Doppler correction to adjust the frequency of each transmitted channel output to correct for Doppler shift.

10. The terminal of claim 9, wherein the channel units communicate telephone calls via C Channels when operating as circuit channels.

11. The terminal of claim 10, wherein the channel units communicate P, R and T Channels when operating as data channels.

12. The terminal of claim 10, wherein the channel units receive telephone calls via C Channels by searching for, acquiring, and locking onto C Channel inputs.

13. The terminal of claim 10, wherein Doppler shift is measured for more than one C Channel input, and the measurements are processed to generate a single measured Doppler shift used to determine each Doppler correction.

14. The terminal of claim 13, wherein the Doppler correction for each transmitted channel output is based upon the ratio of the received channel input frequency to each transmitted channel output frequency.

15. The terminal of claim 14, wherein the Doppler correction is applied to adjust the frequency of each channel output in the opposite direction from the Doppler shift of the received channel input.

16. The terminal of claim 9, wherein the measured Doppler shift is used to determine the Doppler correction for each transmission for only a limited time period.

17. The terminal of claim 16, wherein the limited time period is set as a function of aircraft dynamics.

18. The terminal of claim 17, wherein the limited time period is set as a function of aircraft bank angle.

19. The terminal of claim 16, wherein, after the limited time period expires without a new valid Doppler measurement, one of the channel units is reconfigured to operate as a data channel to receive a P Channel input and to measure Doppler shift via the P Channel input.

20. A method for Doppler shift compensation in a satellite communications terminal for an aircraft during circuit-mode services only communications, the terminal including a plurality of channel units wherein each channel unit provides a circuit channel for supporting a telephone call, the method comprising:

receiving at least one circuit channel input, the at least one circuit channel input having been transmitted by a communications satellite at a known frequency, each circuit channel input having a frequency dependent upon the known transmit frequency and the relative velocity between the aircraft and satellite;

measuring the frequency of the at least one received circuit channel input;

calculating a Doppler error value for the at least one received circuit channel input as a difference between the measured frequency and the known transmit frequency of the at least one received circuit channel input;

determining a Doppler correction value for each circuit channel transmission based upon the Doppler error value; and

applying the Doppler correction value to each transmission of the satellite communications terminal, thereby correcting each transmission for Doppler shift.