System and method for communicating via a satellite in an inclined geosynchronous orbit

• US 10,587,332 B2
• Filed: 01/27/2014
• Issued: 03/10/2020
• Est. Priority Date: 01/27/2014
• Status: Active Grant

• Current Assignee: Peter Lemme
• Original Assignee: Peter Lemme
• Inventors: Lemme, Peter
• Primary Examiner(s): Nguyen, Chuong P
• Application Number:
  US14/164,379
• Publication Number:
  US 20150215029A1
• Time in Patent Office: 2,234 Days
• Field of Search: 342359, 3423574, 342368, 342 37
• CPC Class Codes: H01Q 21/00 Antenna arrays or systems arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system H01Q3/00
• CPC Class Codes: H01Q 3/02 using mechanical movement of antenna or antenna system as a whole
• CPC Class Codes: H01Q 3/34 by electrical means active lenses or reflecting arrays H01Q3/46
• CPC Class Codes: H04B 7/18513 Transmission in a satellite or space-based system
• CPC Class Codes: H04B 7/18528 Satellite systems for providing two-way communications service to a network of fixed stations, i.e. fixed satellite service or very small aperture terminal [VSAT] system
• CPC Class Codes: H04B 7/195 Non-synchronous stations

Abstract

A hub terminal and remote client communicate via a target satellite in an inclined geosynchronous orbit. As the target satellite ascends or descends away from the geostationary arc, the signal strength of the uplink channel is increased without increasing the level of interference with adjacent geostationary satellites. The increased angular separation from adjacent satellites also decreases downlink interference. The resulting increase in signal to interference ratio permits adjustment of the modulation and coding parameters to increase spectral efficiency. The antenna gain pattern is modeled based on antenna characteristics and the model may be supplemented with measurements of a signal relayed by adjacent satellites. The method permits intermittent communication from locations where the geostationary arc is blocked or using disadvantaged antennas that would be impractical for use with geostationary satellites. In some circumstances, it is desirable to deliberately mis-steer the antenna slightly away from the target satellite.

Claims

1. A method of communicating via a satellite, the method comprising:

locating a target satellite in an inclined geosynchronous orbit;

pointing an antenna at an aiming point offset from a geostationary arc, the antenna having a radiation pattern;

estimating a maximum boresite Equivalent Isotropic Radiated Power (EIRP) Spectral Density (SD) that complies with a predetermined maximum off-axis EIRP SD mask along the geostationary arc based on the antenna radiation pattern and the aiming point;

encoding information into a radio frequency signal based on an information rate, coding parameters, and modulation parameters; and

transmitting the radio frequency signal to the target satellite at a transmitted boresite EIRP SD based on the maximum boresite EIRP SD.

2. The method of claim 1 further comprising:

adjusting the aiming point as a declination of the target satellite changes;

revising the maximum boresite EIRP SD as the aiming point changes; and

adjusting the transmitted boresite EIRP SD based on the revised maximum boresite EIRP SD mask.

3. The method of claim 1 further comprising adjusting the information rate as a declination of the target satellite changes.

4. The method of claim 1 further comprising adjusting the coding parameters as a declination of the target satellite changes.

5. The method of claim 1 further comprising adjusting the modulation parameters as a declination of the target satellite changes.

6. The method of claim 1 further comprising:

adjusting the aiming point as a declination of the target satellite changes;

revising the maximum boresite EIRP SD as the aiming point changes;

adjusting the transmitted boresite EIRP SD based on the revised maximum boresite EIRP SD; and

adjusting the information rate, coding parameters, or modulation parameters as the declination of the target satellite changes.

7. The method of claim 1 further comprising measuring a signal transmitted by a geosynchronous satellite other than the target satellite.

8. The method of claim 1 wherein the antenna radiation pattern is non-circular and estimating the maximum boresite EIRP SD is based on a current skew angle.

9. The method of claim 1 wherein a declination of the aiming point is greater in absolute value than a declination of the target satellite.

10. A communications transmitter comprising:

a directional antenna having a radiation pattern;

an antenna pointing control configured to point the antenna at an aiming point offset from a geostationary arc; and

a modulator configured to convert information into a radio frequency signal at an information rate using encoding parameters;

an amplifier configured to amplify the radio frequency signal such that the signal is transmitted from the antenna with a transmitted boresite EIRP SD; and

a processor programmed to determine a maximum boresite EIRP SD that complies with a predetermined maximum off-axis EIRP SD mask along the geostationary arc based on the antenna radiation pattern and the aiming point and to control the amplifier based on the maximum boresite EIRP SD.

11. The transmitter of claim 10 wherein the processor is further programmed to:

locate a target satellite in an inclined geosynchronous orbit;

adjust the aiming point as a declination of the target satellite changes; and

adjust the transmitted boresite EIRP SD as the aiming point changes.

12. The transmitter of claim 11 wherein the processor is further programmed to adjust the information rate as the transmitted boresite EIRP SD changes.

13. The transmitter of claim 11 wherein the processor is further programmed to adjust the encoding parameters as the transmitted boresite EIRP SD changes.

14. The transmitter of claim 11 wherein a declination of the aiming point is greater in absolute value than a declination of the target satellite.

15. The transmitter of claim 10 wherein:

the antenna radiation pattern is non-circular; and

the processor is further programmed to adjust the transmitted boresite EIRP SD as a skew angle changes.

16. A communications receiver comprising:

a directional antenna configured to receive a radio frequency signal from a target satellite in an inclined geosynchronous orbit;

a demodulator configured to convert the radio frequency signal into information at a spectral efficiency; and

a processor programmed to vary demodulator settings to increase the spectral efficiency as a declination of the target satellite increases.

17. The receiver of claim 16 wherein the spectral efficiency is increased by increasing an information rate.

18. The receiver of claim 16 wherein the spectral efficiency is increased by decreasing a bandwidth.

19. The receiver of claim 16 further comprising an antenna pointing control configured to aim the antenna at the target satellite.

20. The receiver of claim 16 further comprising an antenna pointing control configured to aim the antenna at an aiming point having a declination greater in absolute value than the declination of the target satellite.