Space traffic management system, space traffic management device, ground facility and operation method for avoiding collision during orbital descent
A satellite constellation forming system ( 100 ) forms a satellite constellation ( 20 ). The satellite constellation ( 20 ) is composed of a satellite group ( 300 ). In the satellite constellation ( 20 ), the satellite group ( 300 ) provides a service cooperatively. The satellite constellation ( 20 ) has a plurality of orbital planes in which a plurality of satellites ( 30 ) fly at the same orbital altitude in each orbital plane ( 21 ). A satellite constellation forming unit ( 110 ) forms the satellite constellation ( 20 ) in which orbital altitudes of the plurality of orbital planes ( 21 ) are mutually different.
1 . A space traffic management system comprising:
space traffic management devices respectively provided in enterprise devices of a plurality of operators that manage at least an orbital plane and an orbital altitude of a plurality of space objects that form a satellite constellation by communicating with the plurality of space objects via respective communication devices, the space traffic management devices being connected with each other via communication lines,
wherein the enterprise devices are computers that collect information regarding the plurality of space objects and include at least one of a mega-constellation enterprise device, a low earth orbit (LEO) constellation enterprise device, a satellite enterprise device, an orbit transfer enterprise device, a debris removal enterprise device, a rocket launch enterprise device, and a space situational awareness (SSA) enterprise device,
wherein the plurality of space objects are satellites of a mega-constellation at orbital altitudes above 1000 km and are initially maintained at a same orbital plane and at different orbital altitudes or different orbital planes and different orbital altitudes, to avoid collision with one another,
wherein during a process of deorbiting and entering the atmosphere of one of the plurality of space objects during free fall descent, at least one of the space traffic management devices performs an operation for avoiding collision of the one of the plurality of space objects with other of the plurality of space objects by controlling a debris removal satellite to capture and unite the one of the plurality of space objects before the one of the plurality of space objects intrudes into any one of
an area in sun-synchronous orbit of about local sun time (LST) 10:30 at orbital altitudes 500 km to 1000 km,
an area in sun-synchronous orbit of about LST 13:30 at orbital altitudes 500 km to 1000 km,
an area in sun-synchronous orbit of about LST 06:00 at orbital altitudes 500 km to 1000 km, and
an area in sun-synchronous orbit of LST 18:00 at orbital altitudes 500 km to 1000 km, and
wherein the process of deorbiting and entering the atmosphere includes, by the debris removal satellite, capturing and uniting with the one of the plurality of space objects and entering the atmosphere by avoiding the congested areas by changing the inclination of the orbital plane of the one of the plurality of space objects to be different from that of the congested areas or shifting a passage timing by applying acceleration in an out-of-plane direction of the orbital plane by injection from a propulsor in a direction approximately perpendicular to a satellite traveling direction so that the inclination of the orbital plane becomes different from that of the other of the plurality of space objects, based on SSA data processed by the SSA enterprise device, and further comprising prioritizing deorbit operations for space objects at higher orbital altitudes to minimize collision risks in the congested areas based on the SSA data.
2 . The space traffic management system of claim 1 , wherein the one space object is a satellite, and
wherein the capturing of the one space object further includes providing access to the satellite or coupling to the satellite.
3 . The space traffic management system of claim 1 , wherein the space traffic management devices are installed on a public SSA server.
4 . The space traffic management system of claim 1 , wherein the SSA enterprise device is configured to predict potential intrusion of the one of the plurality of space objects into the any one of the areas in sun-synchronous orbit based on SSA data and to initiate the operation for avoiding collision by controlling the debris removal satellite.
5 . The space traffic management system of claim 1 , wherein the debris removal satellite is configured to securely capture and unite with the one of the plurality of space objects to prevent intrusion into the any one of the areas in sun-synchronous orbit.
6 . An operation method for avoiding collision during orbital descent of a space traffic management system in which space traffic management devices respectively provided in enterprise devices of a plurality of operators that manage at least an orbital plane and an orbital altitude of a plurality of space objects that form a satellite constellation by communicating with the plurality of space objects via respective communication devices, the space traffic management device being connected with each other via communication lines, wherein the enterprise devices are computers that collect information regarding the plurality of space objects and include at least one of a mega-constellation enterprise device, a low earth orbit (LEO) constellation enterprise device, a satellite enterprise device, an orbit transfer enterprise device, a debris removal enterprise device, a rocket launch enterprise device, and a space situational awareness (SSA) enterprise device, the operation method for avoiding collision during orbital descent comprising:
initially maintaining the plurality of space objects, which are satellites of a mega-constellation at orbital altitudes above 1000 km, at a same orbital plane and at different orbital altitudes or different orbital planes and different orbital altitudes, to avoid collision with one another,
performing, by at least one of the space traffic management devices, a process of deorbiting and entering the atmosphere of one of the plurality of space objects during free fall descent including an operation for avoiding collision of the one of the plurality of space objects with other of the plurality of space objects by controlling a debris removal satellite to capture and unite the one of the plurality of space objects before the one of the plurality of space objects intrudes into any one of
an area in sun-synchronous orbit of about local sun time (LST) 10:30 at orbital altitudes 500 km to 1000 km,
an area in sun-synchronous orbit of about LST 13:30 at orbital altitudes 500 km to 1000 km,
an area in sun-synchronous orbit of about LST 06:00 at orbital altitudes 500 km to 1000 km,
an area in sun-synchronous orbit of LST 18:00 at orbital altitudes 500 km to 1000 km,
wherein the process of deorbiting and entering the atmosphere includes, by the debris removal satellite, capturing and uniting with the one of the plurality of space objects and entering the atmosphere by avoiding the congested areas by changing the inclination of the orbital plane of the one of the plurality of space objects to be different from that of the congested areas or shifting a passage timing by applying acceleration in an out-of-plane direction of the orbital plane by injection from a propulsor in a direction approximately perpendicular to a satellite traveling direction so that the inclination of the orbital plane becomes different from that of the other of the plurality of space objects, based on SSA data processed by the SSA enterprise device, and further comprising prioritizing deorbit operations for space objects at higher orbital altitudes to minimize collision risks in the congested areas based on the SSA data.
7 . The operation method for avoiding collision of claim 6 , wherein the one space object is a satellite, and
wherein the capturing of the one space object further includes providing access to the satellite or coupling to the satellite.
8 . The operation method for avoiding collision of claim 6 , wherein the space traffic management devices are installed on a public SSA server.
9 . The operation method for avoiding collision of claim 6 , wherein the at least one of the space traffic management devices transmits SSA data to the debris removal satellite to adjust a trajectory of the debris removal satellite and prevent intrusion of the one of the plurality of space objects into the any one of the areas in sun-synchronous orbit.
10 . A space traffic management device that manages at least an orbital plane and an orbital altitude of a plurality of space objects that form a satellite constellation by communicating with the plurality of space objects,
wherein the plurality of space objects are satellites of a mega-constellation at orbital altitudes above 1000 km and are initially maintained at a same orbital plane and at different orbital altitudes or different orbital planes and different orbital altitudes, to avoid collision with one another, and
wherein during a process of deorbiting and entering the atmosphere of one of the plurality of space objects during free fall descent, the space traffic management device performs an operation by using a congested area identification information for avoiding collision of the one of the plurality of space objects with other of the plurality of space objects by controlling a debris removal satellite to capture and unite the one of the plurality of space objects before the one of the plurality of space objects intrudes into the congested area that is identified by the congested area identification information,
wherein the process of deorbiting and entering the atmosphere includes, by the debris removal satellite, capturing and uniting with the one of the plurality of space objects and entering the atmosphere by avoiding the congested areas by changing the inclination of the orbital plane of the one of the plurality of space objects to be different from that of the congested areas or shifting a passage timing by applying acceleration in an out-of-plane direction of the orbital plane by injection from a propulsor in a direction approximately perpendicular to a satellite traveling direction so that the inclination of the orbital plane becomes different from that of the other of the plurality of space objects, based on space situational awareness (SSA) data processed by a SSA enterprise device, and further comprising prioritizing deorbit operations for space objects at higher orbital altitudes to minimize collision risks in the congested areas based on the SSA data.
11 . The space traffic management device of claim 10 , wherein the congested area identification information indicates that the congested area is any one of
an area in sun-synchronous orbit of about local sun time (LST) 10:30 at orbital altitudes 500 km to 1000 km,
an area in sun-synchronous orbit of about LST 13:30 at orbital altitudes 500 km to 1000 km,
an area in sun-synchronous orbit of about LST 06:00 at orbital altitudes 500 km to 1000 km, and
an area in sun-synchronous orbit of LST 18:00 at orbital altitudes 500 km to 1000 km.
12 . The space traffic management device of claim 10 , wherein the debris removal satellite includes a grappling mechanism and the propulsor, the grappling mechanism being configured to capture the one of the plurality of space objects, and the propulsor being configured to adjust a trajectory of the debris removal satellite to avoid intrusion into the congested area based on SSA data.
13 . The space traffic management device of claim 10 , wherein the space traffic management device is configured to process SSA data to generate a collision-free deorbit path for the one of the plurality of space objects and communicate the collision-free deorbit path to the debris removal satellite to avoid intrusion into the congested area.
14 . A ground facility that transmits commands to adjust the altitude of each satellite so as to maintain the relative phases of a plurality of satellites in each orbital plane of a plurality of orbital planes,
wherein the plurality of space objects are satellites of a mega-constellation at orbital altitudes above 1000 km and are initially maintained at a same orbital plane and at different orbital altitudes or different orbital planes and different orbital altitudes, to avoid collision with one another,
wherein during a process of deorbiting and entering the atmosphere of one of the plurality of space objects during free fall descent, the ground facility transmits a capture command and an orbit control command to a debris removal satellite by using a congested area identification information for avoiding collision of the one of the plurality of space objects with other of the plurality of space objects by controlling the debris removal satellite to capture and unite the one of the plurality of space objects before the one of the plurality of space objects intrudes into the congested area that is identified by the congested area identification information, and
wherein the process of deorbiting and entering the atmosphere includes, by the debris removal satellite, capturing and uniting with the one of the plurality of space objects and entering the atmosphere by avoiding the congested areas by changing the inclination of the orbital plane of the one of the plurality of space objects to be different from that of the congested areas or shifting a passage timing by applying acceleration in an out-of-plane direction of the orbital plane by injection from a propulsor in a direction approximately perpendicular to a satellite traveling direction so that the inclination of the orbital plane becomes different from that of the other of the plurality of space objects, based on space situational awareness (SSA) data processed by a SSA enterprise device, and further comprising prioritizing deorbit operations for space objects at higher orbital altitudes to minimize collision risks in the congested areas based on the SSA data.