Satellite constellation forming system, satellite constellation forming method, computer readable medium, and ground device

1. A satellite constellation forming system to form a satellite constellation having a plurality of orbital planes in each of which a plurality of satellites fly as an orbit satellite group, the plurality of orbital planes having mutually different normal directions, each of the plurality of satellites in the orbit satellite group including a propulsion device to change velocity of each of the plurality of satellites in the orbit satellite group, the satellite constellation forming system comprising

processing circuitry to cause propulsion devices of the plurality of satellites in the orbit satellite group to operate in synchronization, for each orbital plane of the plurality of orbital planes,

wherein the processing circuitry causes each satellite in an orbit satellite group in a first orbital plane of the plurality of orbital planes to perform an acceleration and deceleration process of repeating operation of accelerating for a first time period and then decelerating for the first time period, and causes each satellite in an orbit satellite group in an orbital plane adjacent to the first orbital plane to start the acceleration and deceleration process after a delay of a second time period from a time point when the acceleration and deceleration process is started in the first orbital plane, repeatedly for each of the plurality of orbital planes.

2. The satellite constellation forming system according to claim 1 ,

wherein the processing circuitry sets the first time period and the second time period so that an altitude profile of orbital altitudes, in which relative altitude differences between adjacent orbital planes in the plurality of orbital planes are arranged sequentially, is sinusoidal.

3. The satellite constellation forming system according to claim 1 ,

wherein the processing circuitry calculates, as the second time period, a value resulting from dividing the first time period that is doubled by the number of orbital planes of the plurality of orbital planes.

4. A satellite constellation forming method of a satellite constellation forming system to form a satellite constellation having a plurality of orbital planes in each of which a plurality of satellites fly as an orbit satellite group, the plurality of orbital planes having mutually different normal directions, each of the plurality of satellites in the orbit satellite group including a propulsion device to change velocity of each of the plurality of satellites in the orbit satellite group, the satellite constellation forming method comprising:

causing propulsion devices of the plurality of satellites in the orbit satellite group to operate in synchronization, for each orbital plane of the plurality of orbital planes; and

causing each satellite in an orbit satellite group in a first orbital plane of the plurality of orbital planes to perform an acceleration and deceleration process of repeating operation of accelerating for a first time period and then decelerating for the first time period, and causing each satellite in an orbit satellite group in an orbital plane adjacent to the first orbital plane to start the acceleration and deceleration process after a delay of a second time period from a time point when the acceleration and deceleration process is started in the first orbital plane, repeatedly for each of the plurality of orbital planes.

5. A non-transitory computer readable medium storing a satellite constellation forming program for a satellite constellation forming system to form a satellite constellation having a plurality of orbital planes in each of which a plurality of satellites fly as an orbit satellite group, the plurality of orbital planes having mutually different normal directions, each of the plurality of satellites in the orbit satellite group including a propulsion device to change velocity of each of the plurality of satellites in the orbit satellite group, the satellite constellation forming program causing a computer to execute:

a process of causing propulsion devices of the plurality of satellites in the orbit satellite group to operate in synchronization, for each orbital plane of the plurality of orbital planes; and

a process of causing each satellite in an orbit satellite group in a first orbital plane of the plurality of orbital planes to perform an acceleration and deceleration process of repeating operation of accelerating for a first time period and then decelerating for the first time period, and causing each satellite in an orbit satellite group in an orbital plane adjacent to the first orbital plane to start the acceleration and deceleration process after a delay of a second time period from a time point when the acceleration and deceleration process is started in the first orbital plane, repeatedly for each of the plurality of orbital planes.

6. The non-transitory computer readable medium storing the satellite constellation forming program according to claim 5 , further causing the computer to execute

a process of setting the first time period and the second time period so that an altitude profile of orbital altitudes, in which relative altitude differences between adjacent orbital planes in the plurality of orbital planes are arranged sequentially, is sinusoidal.

7. The non-transitory computer readable medium storing the satellite constellation forming program according to claim 5 , further causing the computer to execute

a process of calculating, as the second time period, a value resulting from dividing the first time period that is doubled by the number of orbital planes of the plurality of orbital planes.

8. A ground device of a satellite constellation forming system to form a satellite constellation having a plurality of orbital planes in each of which a plurality of satellites fly as an orbit satellite group, the plurality of orbital planes having mutually different normal directions, each of the plurality of satellites in the orbit satellite group including a propulsion device to change velocity of each of the plurality of satellites in the orbit satellite group, the ground device comprising:

a communication device to transmit and receive signals for tracking and controlling each satellite in the orbit satellite group in each orbital plane of the plurality of orbital planes of the satellite constellation; and

processing circuitry to generate an orbit control command to cause propulsion devices of the plurality of satellites in the orbit satellite group to operate in synchronization, for each orbital plane of the plurality of orbital planes, and to cause each satellite in an orbit satellite group in a first orbital plane of the plurality of orbital planes to perform an acceleration and deceleration process of repeating operation of accelerating for a first time period and then decelerating for the first time period, and cause each satellite in an orbit satellite group in an orbital plane adjacent to the first orbital plane to start the acceleration and deceleration process after a delay of a second time period from a time point when the acceleration and deceleration process is started in the first orbital plane, repeatedly for each of the plurality of orbital planes,

wherein the communication device transmits the orbit control command to each satellite in the orbit satellite group in each orbital plane of the plurality of orbital planes.

9. The ground device according to claim 8 ,

wherein the processing circuitry sets the first time period and the second time period so that an altitude profile of orbital altitudes, in which relative altitude differences between adjacent orbital planes in the plurality of orbital planes are arranged sequentially, is sinusoidal.

10. The ground device according to claim 8 ,

wherein the processing circuitry calculates, as the second time period, a value resulting from dividing the first time period that is doubled by the number of orbital planes of the plurality of orbital planes.

11. The satellite constellation forming system according to claim 2 ,

wherein the processing circuitry calculates, as the second time period, a value resulting from dividing the first time period that is doubled by the number of orbital planes of the plurality of orbital planes.

12. The non-transitory computer readable medium storing the satellite constellation forming program according to claim 6 , further causing the computer to execute

a process of calculating, as the second time period, a value resulting from dividing the first time period that is doubled by the number of orbital planes of the plurality of orbital planes.

13. The ground device according to claim 9 ,

wherein the processing circuitry calculates, as the second time period, a value resulting from dividing the first time period that is doubled by the number of orbital planes of the plurality of orbital planes.