Non-geosynchronous orbit satellite constellations
A method for designing Non-Geosynchronous Orbit (NGSO) satellite constellations and NGSO satellite constellations thereof are presented. An NGSO satellite constellation may be designed to allow an earth station to perform handover between two satellites of the NGSO satellite constellation while the two satellites appear to be at about a same location in the sky relative to the earth station. In such constellation, an earth station may perform such handover between the two satellites in a Make-Before-Break fashion while the earth station may be configured to use a single, slow-tracking antenna, such as a mechanically tracking dish antenna.
1. A satellite communication earth station comprising a single antenna, the satellite communication earth station configured to track satellites of a satellite constellation using the single antenna, wherein tracking the satellites of the satellite constellation comprises:
tracking a first satellite associated with a first orbit along a first section of the first orbit;
determining that the first satellite is at about a first handover point associated with the first orbit and with a second orbit;
switching communication from the first satellite to a second satellite associated with the second orbit, wherein:
the second satellite and the first satellite are at about the first handover point associated with the first orbit and the second orbit at about a same time, and
the switching communication from the first satellite to the second satellite is in accordance with a make-before-break technique;
tracking the second satellite along a second section of the second orbit, wherein the first section and the second section are part of a first tracking pattern;
performing one or more tracking cycles along the first tracking pattern;
determining a need to switch the tracking of the satellites to a second tracking pattern located to the east of the first tracking pattern, wherein the first tracking pattern and the second tracking pattern have a common handover point; and
switching the tracking of the satellites from the first tracking pattern to the second tracking pattern by tracking a satellite in accordance to the first tracking pattern past the common handover point into the second tracking pattern, without switching communication at about the common handover point.
2. The satellite communication earth station of claim 1 , wherein tracking the satellites of the satellite constellation further comprises:
determining that the second satellite is at about a second handover point associated with the second orbit and with a third orbit;
switching communication from the second satellite to a third satellite associated with the third orbit;
tracking the third satellite along a third section of the third orbit;
determining that the third satellite is at about a third handover point associated with the third orbit and with a fourth orbit;
switching communication from the third satellite to a fourth satellite associated with the fourth orbit;
tracking the fourth satellite along a fourth section of the fourth orbit;
determining that the fourth satellite is at about a fourth handover point associated with the fourth orbit and with the first orbit; and
switching communication from the fourth satellite to another satellite associated with the first orbit, the another satellite is different from the first satellite.
3. The satellite communication earth station of claim 2 , wherein the third section and the fourth section are part of the first tracking pattern.
4. The satellite communication earth station of claim 1 , wherein tracking the satellites of the satellite constellation further comprises:
determining that the second satellite is at about a second handover point associated with the second orbit and with a third orbit;
switching communication from the second satellite to a third satellite associated with the third orbit;
tracking the third satellite along a section of the third orbit;
determining that the third satellite is at about a third handover point associated with the third orbit and with the first orbit; and
switching communication from the third satellite to another satellite associated with the first orbit, the another satellite is different from the first satellite.
5. The satellite communication earth station of claim 1 , where the make-before-break technique comprises establishing a second return link over the second satellite prior to terminating a first return link over the first satellite.
6. The satellite communication earth station of claim 3 , wherein a tracking direction of the first tracking pattern is opposite to a tracking direction of the second tracking pattern.
7. A method of tracking satellites of a satellite constellation using a single antenna of a satellite communication earth station, the method comprising:
tracking, by the satellite communication earth station, a first satellite associated with a first orbit along a first section of the first orbit;
determining, by the satellite communication earth station, that the first satellite is at about a first handover point associated with the first orbit and with a second orbit;
switching, by the satellite communication earth station, communication from the first satellite to a second satellite associated with the second orbit, wherein:
the second satellite and the first satellite are at about the first handover point associated with the first orbit and the second orbit at about a same time, and
the switching communication from the first satellite to the second satellite is in accordance with a make-before-break technique;
tracking, by the satellite communication earth station, the second satellite along a second section of the second orbit, wherein the first section and the second section are part of a first tracking pattern;
performing one or more tracking cycles along the first tracking pattern;
determining a need to switch the tracking of the satellites to a second tracking pattern located to the east of the first tracking pattern, wherein the first tracking pattern and the second tracking pattern have a common handover point; and
switching the tracking of the satellites from the first tracking pattern to the second tracking pattern by tracking a satellite in accordance to the first tracking pattern past the common handover point into the second tracking pattern, without switching communication at about the common handover point.
8. The method of claim 7 , further comprising:
determining that the second satellite is at about a second handover point associated with the second orbit and with a third orbit;
switching communication from the second satellite to a third satellite associated with the third orbit;
tracking the third satellite along a third section of the third orbit;
determining that the third satellite is at about a third handover point associated with the third orbit and with a fourth orbit;
switching communication from the third satellite to a fourth satellite associated with the fourth orbit;
tracking the fourth satellite along a fourth section of the fourth orbit;
determining that the fourth satellite is at about a fourth handover point associated with the fourth orbit and with the first orbit; and
switching communication from the fourth satellite to another satellite associated with the first orbit, the another satellite is different from the first satellite.
9. The method of claim 8 , wherein the third section and the fourth section are part of the first tracking pattern.
10. The method of claim 7 , further comprising:
determining that the second satellite is at about a second handover point associated with the second orbit and with a third orbit;
switching communication from the second satellite to a third satellite associated with the third orbit;
tracking the third satellite along a section of the third orbit;
determining that the third satellite is at about a third handover point associated with the third orbit and with the first orbit; and
switching communication from the third satellite to another satellite associated with the first orbit, the another satellite is different from the first satellite.
11. The method of claim 7 , where the make-before-break technique comprises establishing a second return link over the second satellite prior to terminating a first return link over the first satellite.
12. The method of claim 9 , wherein a tracking direction of the first tracking pattern is opposite to a tracking direction of the second tracking pattern.
13. A system comprising:
a satellite constellation comprising one or more satellites;
a satellite communication earth station comprising a single antenna, wherein the satellite communication earth station is configured to:
track a first satellite, of the one or more satellites, wherein the first satellite is associated with a first orbit along a first section of the first orbit;
determine that the first satellite is at about a first handover point associated with the first orbit and with a second orbit;
switch communication from the first satellite to a second satellite, of the one or more satellites, wherein the second satellite is associated with the second orbit, wherein:
the second satellite and the first satellite are at about the first handover point associated with the first orbit and the second orbit at about a same time, and
the switching communication from the first satellite to the second satellite is in accordance with a make-before-break technique;
track the second satellite along a second section of the second orbit, wherein the first section and the second section are part of a first tracking pattern;
perform one or more tracking cycles along the first tracking pattern;
determine a need to switch the tracking of the satellites to a second tracking pattern located to the east of the first tracking pattern, wherein the first tracking pattern and the second tracking pattern have a common handover point; and
switch the tracking of the satellites from the first tracking pattern to the second tracking pattern by tracking a satellite in accordance to the first tracking pattern past the common handover point into the second tracking pattern, without switching communication at about the common handover point.
14. The system of claim 13 , wherein the satellite communication earth station is configured to:
determine that the second satellite is at about a second handover point associated with the second orbit and with a third orbit;
switch communication from the second satellite to a third satellite associated with the third orbit;
track the third satellite along a third section of the third orbit;
determine that the third satellite is at about a third handover point associated with the third orbit and with a fourth orbit;
switch communication from the third satellite to a fourth satellite associated with the fourth orbit;
track the fourth satellite along a fourth section of the fourth orbit;
determine that the fourth satellite is at about a fourth handover point associated with the fourth orbit and with the first orbit; and
switch communication from the fourth satellite to another satellite associated with the first orbit, the another satellite is different from the first satellite.
15. The system of claim 14 , wherein the third section and the fourth section are part of the first tracking pattern.
16. The system of claim 13 , wherein the satellite communication earth station is configured to:
determine that the second satellite is at about a second handover point associated with the second orbit and with a third orbit;
switch communication from the second satellite to a third satellite associated with the third orbit;
track the third satellite along a section of the third orbit;
determine that the third satellite is at about a third handover point associated with the third orbit and with the first orbit; and
switch communication from the third satellite to another satellite associated with the first orbit, the another satellite is different from the first satellite.
17. The system of claim 13 , where the make-before-break technique comprises establishing a second return link over the second satellite prior to terminating a first return link over the first satellite.
18. The system of claim 15 , wherein a tracking direction of the first tracking pattern is opposite to a tracking direction of the second tracking pattern.