Satellite constellation forming system, satellite constellation forming method, ground facility, and business device

Patent metadata

Field	Value
Publication number	US-12344405-B2
Application number	US-202117792406-A
Country	US
Kind code	B2
Filing date	Mar 9, 2021
Priority date	Mar 10, 2020
Publication date	Jul 1, 2025
Grant date	Jul 1, 2025

Abstract

A satellite constellation forming system ( 600 ) forms a satellite constellation which is composed of a satellite group that cooperatively provides a communication service, and has a plurality of orbital planes in each of which a plurality of satellites fly at the same orbital altitude. Each satellite of the satellite group includes inter-satellite communication means and satellite-ground communication means. A satellite constellation forming unit ( 11 ) forms the satellite constellation which has ten or more orbital planes with different normal directions, and in which at least one relative angle in an azimuth direction of adjacent orbital planes of the plurality of orbital planes is arranged to be uneven and satellite-ground communication means of satellites flying in orbital planes spaced unevenly have a communication range that achieves complete ground coverage above the equator.

First claim

The invention claimed is:

1. A satellite constellation forming system to form a satellite constellation which is composed of a satellite group and in which the satellite group cooperatively provides a communication service, the satellite constellation having a plurality of orbital planes in each of which a plurality of satellites fly at a same orbital altitude, wherein each satellite of the satellite group includes an inter-satellite communication device and a satellite-ground communication device, the satellite constellation forming system comprising:
processing circuitry configured to:
form the satellite constellation such that the plurality of orbital planes includes ten or more orbital planes with different normal directions; and
form a passage region for a space object to pass through in the satellite constellation such that:
a first set of adjacent orbital planes of the plurality of orbital planes is set,
a first angle between the first set of adjacent orbital planes in an azimuth direction is set,
a second set of adjacent orbital planes of the plurality of orbital planes is set,
a second angle between the second set of adjacent orbital planes in the azimuth direction is set, and
the first angle is different from the second angle resulting in the first set of adjacent orbital planes being spaced unevenly,

wherein the satellite-ground communication devices of the satellites flying in the orbital planes that are spaced unevenly have a communication range that achieves complete ground coverage above the equator.

2. The satellite constellation forming system according to claim 1 , wherein the processing circuitry is configured to cause the satellite group to simultaneously ascend or descend in orbital altitude so as to move the orbital planes that are spaced unevenly.

3. A satellite constellation forming method of a satellite constellation forming system to form a satellite constellation which is composed of a satellite group and in which the satellite group cooperatively provides a communication service, the satellite constellation having a plurality of orbital planes in each of which a plurality of satellites fly at a same orbital altitude, wherein each satellite of the satellite group includes an inter-satellite communication device and a satellite-ground communication device, the satellite constellation forming method comprising:
forming the satellite constellation such that the plurality of orbital planes includes ten or more orbital planes with different normal directions; and
forming a passage region for a space object to pass through in the satellite constellation such that:
a first set of adjacent orbital planes of the plurality of orbital planes is set,
a first angle between the first set of adjacent orbital planes in an azimuth direction is set,
a second set of adjacent orbital planes of the plurality of orbital planes is set,
a second angle between the second set of adjacent orbital planes in the azimuth direction is set, and
the first angle is different from the second angle resulting in the first set of adjacent orbital planes being spaced unevenly,

wherein the satellite-ground communication devices of the satellites flying in the orbital planes that are spaced unevenly have a communication range that achieves complete ground coverage above the equator.

4. A ground facility included in a satellite constellation forming system to form a satellite constellation which is composed of a satellite group and in which the satellite group cooperatively provides a communication service, the satellite constellation having a plurality of orbital planes in each of which a plurality of satellites fly at a same orbital altitude, wherein each satellite of the satellite group includes an inter-satellite communication device and a satellite-ground communication device, the ground facility comprising:
processing circuitry configured to:
form the satellite constellation such that the plurality of orbital planes includes ten or more orbital planes with different normal directions; and
form a passage region for a space object to pass through in the satellite constellation such that:
a first set of adjacent orbital planes of the plurality of orbital planes is set,
a first angle between the first set of adjacent orbital planes in an azimuth direction is set,
a second set of adjacent orbital planes of the plurality of orbital planes is set,
a second angle between the second set of adjacent orbital planes in the azimuth direction is set, and
the first angle is different from the second angle resulting in the first set of adjacent orbital planes being spaced unevenly,

wherein the satellite-ground communication devices of the satellites flying in the orbital planes that are spaced unevenly have a communication range that achieves complete ground coverage above the equator.

5. A business device of a satellite constellation business operator that manages a satellite constellation, wherein the business device of the satellite constellation business operator executes the satellite constellation forming method according to claim 3 .

6. The satellite constellation forming system according to claim 1 , wherein the processing circuitry is configured to form the passage region such that the first angle is different from the second angle in response to determining that unevenly spaced orbital planes are to be formed.

7. The satellite constellation forming system according to claim 6 , wherein the processing circuitry is configured to determine that the unevenly spaced orbital planes are to be formed when the space object will pass through the orbital altitude of the satellite constellation.

8. The satellite constellation forming system according to claim 1 , wherein the processing circuitry is configured to cause all of the satellites in the first set of adjacent orbital planes to simultaneously change their orbital altitude.

9. The satellite constellation forming system according to claim 1 , wherein the processing circuitry is configured to cause the satellite group to simultaneously ascend in orbital altitude while maintaining a state in which average orbital altitudes of the plurality of orbital planes are raised in a sequential order.

10. The satellite constellation forming method according to claim 3 , wherein the method includes forming the passage region such that the first angle is different from the second angle in response to determining that unevenly spaced orbital planes are to be formed.

11. The satellite constellation forming method according to claim 10 , wherein the method includes determining that the unevenly spaced orbital planes are to be formed when the space object will pass through the orbital altitude of the satellite constellation.

12. The satellite constellation forming method according to claim 3 , further comprising causing all of the satellites in the first set of adjacent orbital planes to simultaneously change their orbital altitude.

13. The satellite constellation forming method according to claim 3 , further comprising causing the satellite group to simultaneously ascend in orbital altitude while maintaining a state in which average orbital altitudes of the plurality of orbital planes are raised in a sequential order.

14. The ground facility according to claim 4 , wherein the processing circuitry is configured to form the passage region such that the first angle is different from the second angle in response to determining that unevenly spaced orbital planes are to be formed.

15. The ground facility according to claim 14 , wherein the processing circuitry is configured to deter

Assignees

• Mitsubishi Electric Corp

Inventors

• Mukae Hisayuki

Classifications

• B64G1/62

  Systems for re-entry into the earth's atmosphere; Retarding or landing devices · CPC title

• B64G1/2429

  Station keeping · CPC title

• B64G1/242

  Orbits and trajectories · CPC title

• H04B7/18513 Primary

  Transmission in a satellite or space-based system · CPC title

• B64G1/244

  Spacecraft control systems · CPC title