Methods for effecting seamless handover and enhancing capacity in elliptical orbit satellite communications systems

• US 20070135040A1
• Filed: 06/07/2006
• Published: 06/14/2007
• Est. Priority Date: 12/12/2005
• Status: Abandoned Application

• Current Assignee: John Draim
• Original Assignee: John Draim
• Inventors: Draim, John
• Application Number:
  US11/448,183
• Publication Number:
  US 20070135040A1
• Time in Patent Office: Days
• US Class Current: 455/12.100
• CPC Class Codes: H04B 7/18541 for handover of resources

Abstract

Seamless handover of a communications signal from a first satellite to a second satellite is provided when the satellites are at orbital positions which coincide. Timing marks are inserted simultaneously in signals transmitted through the satellites, and signals received from the satellites compared to determine the difference in path length. Handover occurs when the path length difference is zero and the two signals are perfectly synchronized. Interference between the signals transmitted through the two satellites is avoided by using different transmission modes, such as different carrier frequencies, orthogonal senses of polarization, or digital signals with uncorrelated spreading codes. Using these different transmission modes in the right- and left-leaning orbits of a Cobra Teardrop system also permits overlaying multiple teardrop patterns, at longitudinal spacings comparable to the Basic Cobra system, as well as closer in-track spacing of satellites. The result is over an order of magnitude increase in global system capacity.

Claims

1. A method for effecting a seamless handover of a communications signal from a first satellite to a second satellite when the first and second satellites are at orbital positions which coincide, the method comprising:

determining a time at which a first signal path length from a transmitting earth station to a receiving earth station through the first satellite is equal to a second signal path length from the transmitting earth station to the receiving earth station through the second satellite; and

effecting the communications signal handover from the first satellite to the second satellite at the time so determined.

2. The method of claim 1, wherein said determining a time at which the first and second signal path lengths are equal comprises:

inserting a timing mark simultaneously in a first signal transmitted through the first satellite and in a second signal transmitted through the second satellite;

receiving the first signal from the first satellite in a first mode; and

receiving the second signal from the second satellite in a second mode, such that the second signal does not interfere with the first signal.

3. The method of claim 2, wherein the first mode is transmission at a first carrier frequency and the second mode is transmission at a second carrier frequency which differs from the first carrier frequency.

4. The method of claim 2, wherein the first mode is transmission in a first polarization sense and the second mode is transmission in a second polarization sense which is orthogonal to the first polarization sense.

5. The method of claim 4, wherein one of the first and second polarization sense is right-hand circular polarization and the other polarization sense is left-hand circular polarization.

6. The method of claim 2, wherein the first mode is spread spectrum digital transmission using a first spreading code and the second mode is spread spectrum digital transmission using a second spreading code which is uncorrelated with the first spreading code.

7. The method of claim 2, wherein said determining a time at which the first and second signal path lengths are equal further comprises:

measuring a time difference between receipt of the time mark inserted in the first signal and receipt of the time mark inserted in the second signal; and

determining the first and second signal path lengths to be equal when the time difference is zero.

8. The method of claim 2, wherein said determining a time at which the first and second signal path lengths are equal further comprises:

measuring a time difference between receipt of the time mark inserted in the first signal and receipt of the time mark inserted in the second signal;

determining a rate of change of the time difference based on the measurement of the time difference and at least one previous measurement of the time difference;

dividing the measured time difference by the rate of change of the time difference to predict when the first and second signal path lengths will be equal

9. The method of claim 1, wherein both the first satellite and the second satellite are in elliptical orbits.

10. The method of claim 9, wherein one of the first satellite and the second satellite is in a left-leaning Cobra Teardrop orbit and the other is in a right-leaning Cobra Teardrop orbit.

11. The method of claim 9, wherein the first satellite in descending in altitude and the second satellite is ascending in altitude.

12. The method of claim 9, wherein the first satellite is turned off after handover of the communications signal and the second satellite is turned on before handover of the communications signal.

13. A method for effecting handover of a communications signal from a first satellite which is in a first elliptical orbit and descending in altitude, to a second satellite which is in a second elliptical orbit and ascending in altitude, when the first and second satellites are at orbital positions which coincide, the method comprising:

determining a time at which the first satellite and the second satellite are at the same altitude; and

simultaneously turning the first satellite off and turning the second satellite on at the time so determined.

14. The method of claim 13, wherein one of the first satellite and the second satellite is in a left-leaning Cobra Teardrop orbit and the other is in a right-leaning Cobra Teardrop orbit.

15. A method of enhancing the communications capacity of a Cobra Teardrop satellite constellation having a first plurality of satellites in a left-leaning ground track and a right-leaning ground track which form a first set of teardrop patterns, and a second plurality of satellites in a left-leaning ground track and a right-leaning ground track which form a second set of teardrop patterns, the method comprising:

communicating with the satellites in the left-leaning ground tracks using signals in a first mode;

communicating with the satellites in the right-leaning ground tracks using signals in a second mode, such that the signals in the second mode do not interfere with the signals in the first mode; and

arranging the orbits of the first and second pluralities of satellites such that the first and second sets of teardrop patterns are displaced from each other in longitude but are overlapping.

16. The method of claim 15, wherein the first mode is transmission at a first carrier frequency and the second mode is transmission at a second carrier frequency which differs from the first carrier frequency.

17. The method of claim 15, wherein the first mode is transmission in a first polarization sense and the second mode is transmission in a second polarization sense which is orthogonal to the first polarization sense.

18. The method of claim 17, wherein one of the first and second polarization sense is right-hand circular polarization and the other polarization sense is left-hand circular polarization.

19. The method of claim 15, wherein the first mode is spread spectrum digital transmission using a first spreading code and the second mode is spread spectrum digital transmission using a second spreading code which is uncorrelated with the first spreading code.