System for maintaining satellites in orbital configuration to mitigate interference with geosynchronous satellites
Many satellites comprising a constellation are arranged in non-geosynchronous orbits (NGSO) forming a regular lattice arrangement in terms of right ascension ascending node (RAAN) and mean anomaly (M), with the orbital parameters specified by the position in the lattice. A set of satellites form a traffic lane having a nonzero RAAN/M slope. Lattice arrangements may be determined based on operational parameters such as antenna pattern beamwidth. The regular lattice may be configured such that adjacent satellites in each lane provide coverage for areas that are subject to interference exclusion limitations. For example, to prevent interference between an NGSO satellite and the geosynchronous satellite's service, the NGSO satellite is prohibited from transmitting towards a ground terminal that may be looking towards the geosynchronous satellite. The regular lattice may also be configured such that lanes in the regular lattice provide coverage for at least a portion of exclusion areas in adjacent lanes.
1 . A method of controlling satellites, the method comprising:
determining a first set of orbital parameters comprising:
a first traffic lane associated with a first plurality of satellites, wherein each satellite of the first plurality of satellites is associated with:
a respective one of a first plurality of right ascension of the ascending node (RAAN) values, and
a respective one of a first plurality of mean anomaly (M) values, and
a second traffic lane associated with a second plurality of satellites, wherein each satellite of the second plurality of satellites is associated with:
a respective one of a second plurality of RAAN values, and
a respective one of a second plurality of M values,
wherein:
the first plurality of RAAN values and the first plurality of M values, and
the second plurality of RAAN values and the second plurality of M values form a regular lattice with respect to RAAN and M;
determining the regular lattice with respect to RAAN and M such that:
a first distance within the regular lattice between adjacent satellites in a same traffic lane is a first value,
a second distance within the regular lattice between adjacent satellites in the first traffic lane and the second traffic lane is a second value, and
the first value is less than the second value;
placing the first plurality of satellites into orbits corresponding to the first traffic lane;
determining, from respective ones of the first plurality of satellites, first position data;
determining a first set of maneuvering instructions based at least in part on the first position data and the first set of orbital parameters associated with the first traffic lane; and
based at least in part on the first set of maneuvering instructions, maneuvering the respective ones of the first plurality of satellites to within (i) a first threshold value of the associated RAAN value, and (ii) a second threshold value of the associated M value.
2 . The method of claim 1 , further comprising:
determining that a first ground track associated with the first traffic lane is adjacent, with respect to Earth, to a second ground track associated with the second traffic lane;
determining that the first traffic lane is associated with a first direction of motion with respect to Earth; and
determining that the second traffic lane is associated with a second direction of motion with respect to Earth that is opposite the first direction of motion.
3 . The method of claim 1 , further comprising:
determining that the first traffic lane has a first slope, with respect to the regular lattice with respect to RAAN and M, that is not equal to zero.
4 . The method of claim 1 , further comprising:
determining a satellite transmit beamwidth associated with operation of respective ones of the first plurality of satellites; and
determining a width of the first traffic lane and the second traffic lane, wherein the width is based at least in part on the satellite transmit beamwidth and overlap between transmissions from adjacent satellites in the first plurality of satellites that mitigate geosynchronous exclusion areas.
5 . The method of claim 1 , further comprising:
determining a satellite transmit beamwidth associated with operation of respective ones of the first plurality of satellites; and
determining one or more of the first plurality of RAAN values, the first plurality of M values, the second plurality of RAAN values, or the second plurality of M values such that coverage from satellites within the first traffic lane minimize geosynchronous exclusion areas.
6 . The method of claim 1 , further comprising:
determining a satellite transmit beamwidth associated with operation of respective ones of the first plurality of satellites; and
determining one or more of the first plurality of RAAN values, the first plurality of M values, the second plurality of RAAN values, or the second plurality of M values such that coverage from satellites within the first traffic lane and the second traffic lane minimize geosynchronous exclusion areas.
7 . The method of claim 1 , further comprising:
determining that the first set of orbital parameters are associated with a first altitude; and
determining that the first traffic lane and the second traffic lane as designated with respect to RAAN and M do not intersect, and wherein:
the first traffic lane is associated with a first ground track,
the second traffic lane is associated with a second ground track, and
the first ground track intersects with the second ground track.
8 . The method of claim 1 , wherein:
the first set of orbital parameters are determined based on capabilities of maneuvering systems associated with the first plurality of satellites and the second plurality of satellites.
9 . A system comprising:
a constellation comprising:
a first plurality of satellites,
a second plurality of satellites; and
wherein each satellite of the constellation comprises a maneuvering system; and
a first set of one or more processors executing instructions to:
determine a first set of orbital parameters comprising:
a first traffic lane associated with the first plurality of satellites, wherein each satellite of the first plurality of satellites is associated with:
a respective one of a first plurality of right ascension of the ascending node (RAAN) values, and
a respective one of a first plurality of mean anomaly (M) values, and
a second traffic lane associated with the second plurality of satellites, wherein each satellite of the second plurality of satellites is associated with:
a respective one of a second plurality of RAAN values, and
a respective one of a second plurality of M values,
wherein:
the first plurality of RAAN values and the first plurality of M values, and
the second plurality of RAAN values and the second plurality of M values form a regular lattice with respect to RAAN and M; and
wherein the first traffic lane has a first slope, with respect to the regular lattice with respect to RAAN and M, that is not equal to zero; and
operate the maneuvering systems of satellites in the first plurality of satellites based on the first set of orbital parameters.
10 . The system of claim 9 , wherein, with respect to the regular lattice with respect to RAAN and M:
a first distance within the regular lattice between adjacent satellites in a same traffic lane is a first value,
a second distance within the regular lattice between adjacent satellites in the first traffic lane and the second traffic lane is a second value, and
the first value is less than the second value.
11 . The system of claim 9 , wherein;
the first traffic lane is associated with a first ground track having a first direction of motion, and
the second traffic lane is associated with a second ground track having a second direction of motion that is opposite the first direction of motion.
12 . The system of claim 9 , the first set of one or more processors executing instructions to:
determine a satellite transmit beamwidth associated with operation of respective ones of the first plurality of satellites; and
determine one or more of the first plurality of RAAN values, the first plurality of M values, the second plurality of RAAN values, or the second plurality of M values such that coverage from satellites within the first traffic lane minimize geosynchronous exclusion areas.
13 . The system of claim 9 , the first set of one or more processors executing instructions to:
determine a satellite transmit beamwidth associated with operation of respective ones of the first plurality of satellites; and
determine one or more of the first plurality of RAAN values, the first plurality of M values, the second plurality of RAAN values, or the second plurality of M values such that coverage from satellites within the first traffic lane and the second traffic lane minimize geosynchronous exclusion areas.
14 . The system of claim 9 , wherein:
the first set of orbital parameters are based on capabilities of the maneuvering systems associated with the first plurality of satellites and the second plurality of satellites.
15 . The system of claim 9 , the first set of one or more processors executing instructions to:
determine, from respective ones of the first plurality of satellites, first position data;
determine a first set of maneuvering instructions based at least in part on the first position data and the first set of orbital parameters associated with the first traffic lane; and
wherein operation of the maneuvering systems of the satellites in the first plurality of satellites is based on the first set of maneuvering instructions.
16 . A method performed by a first satellite in a constellation of satellites, the method comprising:
determining first position data based on one or more sensors of the first satellite;
retrieving a first set of orbital parameters comprising:
a first traffic lane associated with a first plurality of satellites, wherein each satellite of the first plurality of satellites is associated with:
a respective one of a first plurality of right ascension of the ascending node (RAAN) values, and
a respective one of a first plurality of mean anomaly (M) values, and
a second traffic lane associated with a second plurality of satellites, wherein each satellite of the second plurality of satellites is associated with:
a respective one of a second plurality of RAAN values, and
a respective one of a second plurality of M values,
wherein:
the first plurality of RAAN values and the first plurality of M values, and
the second plurality of RAAN values and the second plurality of M values form a regular lattice with respect to RAAN and M;
determining that the first set of orbital parameters are associated with a first altitude;
determining that the first traffic lane and the second traffic lane as designated with respect to RAAN and M do not intersect, wherein:
the first traffic lane is associated with a first ground track,
the second traffic lane is associated with a second ground track, and
the first ground track intersects with the second ground track;
determining, based on the first position data and the first set of orbital parameters, a first set of maneuvering instructions; and
maneuvering, based on the first set of maneuvering instructions, the first satellite to within a first threshold value of the associated RAAN value, and a second threshold value of the associated M value.
17 . The method of claim 16 , further comprising:
determining the regular lattice with respect to RAAN and M such that:
a first distance within the regular lattice between adjacent satellites in a same traffic lane is a first value,
a second distance within the regular lattice between adjacent satellites in the first traffic lane and the second traffic lane is a second value, and
the first value is less than the second value.
18 . The method of claim 16 , further comprising:
determining that the first traffic lane has a first slope, with respect to the regular lattice with respect to RAAN and M, that is not equal to zero.
19 . The method of claim 16 , further comprising:
determining a satellite transmit beamwidth associated with operation of respective ones of the first plurality of satellites; and
determining one or more of the first plurality of RAAN values, the first plurality of M values, the second plurality of RAAN values, or the second plurality of M values such that geosynchronous exclusion areas are minimized.
20 . The method of claim 16 , further comprising:
determining the first set of orbital parameters based on capabilities of maneuvering systems associated with the first plurality of satellites and the second plurality of satellites.