Advanced timing and time transfer for satellite constellations using crosslink ranging and an accurate time source
First Claim
1. A method for timing for a satellite constellation, the method comprising:
- transmitting, by at least one first satellite, at least one crosslink ranging signal to at least one second satellite, wherein at least one of the at least one first satellite and the at least one second satellite is a timing satellite with a synchronization time;
receiving, by the at least one second satellite, the at least one crosslink ranging signal;
calculating at least one ranging measurement from the at least one first satellite to the at least one second satellite by using an amount of time elapsed from the transmitting of the at least one crosslink ranging signal to the receiving of the at least one crosslink ranging signal; and
calculating an estimate of time and frequency for the at least one first satellite and the at least one second satellite relative to each other and to the synchronization time to synchronize the time and the frequency for at least one of the at least one first satellite and the at least one second satellite by using at least one of the at least one ranging measurement and the synchronization time from the at least one timing satellite; and
calculating an estimate of orbital positioning for at least one of the at least one first satellite and the at least one second satellite by using at least one of the at least one ranging measurement, the synchronization time, positioning data from the at least one timing satellite, and at least one positioning ranging measurement.
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Accused Products
Abstract
A system, method, and apparatus for advanced timing and time transfer for satellite constellations using crosslink ranging and an accurate time source are disclosed herein. In particular, the present disclosure relates generally to systems for providing improved positioning, navigation, and/or timing information for oscillator calibration and more specifically, to use at least one satellite with accessibility to an accurate time source to calibrate the local oscillator on a crosslink paired satellite. In at least, one embodiment, time synchronization on a subset of satellites with crosslinking capabilities is used to distribute time through a network of crosslinked satellites.
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Citations
27 Claims
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1. A method for timing for a satellite constellation, the method comprising:
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transmitting, by at least one first satellite, at least one crosslink ranging signal to at least one second satellite, wherein at least one of the at least one first satellite and the at least one second satellite is a timing satellite with a synchronization time; receiving, by the at least one second satellite, the at least one crosslink ranging signal; calculating at least one ranging measurement from the at least one first satellite to the at least one second satellite by using an amount of time elapsed from the transmitting of the at least one crosslink ranging signal to the receiving of the at least one crosslink ranging signal; and calculating an estimate of time and frequency for the at least one first satellite and the at least one second satellite relative to each other and to the synchronization time to synchronize the time and the frequency for at least one of the at least one first satellite and the at least one second satellite by using at least one of the at least one ranging measurement and the synchronization time from the at least one timing satellite; and calculating an estimate of orbital positioning for at least one of the at least one first satellite and the at least one second satellite by using at least one of the at least one ranging measurement, the synchronization time, positioning data from the at least one timing satellite, and at least one positioning ranging measurement. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12)
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13. A method for timing for a satellite constellation, the method comprising:
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transmitting, by at least one first satellite, at least one first crosslink ranging signal to at least one second satellite, wherein at least one of the at least one first satellite and the at least one second satellite is a timing satellite with a synchronization time; receiving, by the at least one second satellite, the at least one first crosslink ranging signal; transmitting, by the at least one second satellite, at least one second crosslink ranging signal to the at least one first satellite; receiving, by the at least one first satellite, the at least one second crosslink ranging signal; calculating at least one first ranging measurement from the at least one first satellite to the at least one second satellite by using an amount of time elapsed from the transmitting of the at least one first crosslink ranging signal to the receiving of the at least one first crosslink ranging signal; calculating at least one second ranging measurement from the at least one second satellite to the at least one first satellite by using an amount of time elapsed from the transmitting of the at least one second crosslink ranging signal to the receiving of the at least one second crosslink ranging signal calculating an estimate of time and frequency for the at least one first satellite and the at least one second satellite relative to each other and to the synchronization time to synchronize the time and the frequency for at least one of the at least one first satellite and the at least one second satellite by using at least one of the at least one first ranging measurement, the at least one second ranging measurement, and the synchronization time from the at least one timing satellite; and calculating an estimate of orbital positioning for at least one of the at least one first satellite and the at least one second satellite by using at least one of the at least one first ranging measurement, the at least one second ranging measurement, the synchronization time, positioning data from the at least one timing satellite, and at least one positioning ranging measurement.
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14. A system for timing for a satellite constellation, the system comprising:
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at least one first satellite configured to transmit at least one crosslink ranging signal to at least one second satellite; the at least one second satellite configured to receive the at least one crosslink ranging signal, wherein at least one of the at least one first satellite and the at least one second satellite is a timing satellite with a synchronization time; at least one processor configured to calculate at least one ranging measurement from the at least one first satellite to the at least one second satellite by using an amount of time elapsed from the transmitting of the at least one crosslink ranging signal to the receiving of the at least one crosslink ranging signal; the at least one processor further configured to calculate an estimate of time and frequency for the at least one first satellite and the at least one second satellite relative to each other and to the synchronization time to synchronize the time and the frequency for at least one of the at least one first satellite and the at least one second satellite by using at least one of the at least one ranging measurement and the synchronization time from the at least one timing satellite; and the at least one processor is further configured to calculate an estimate of orbital positioning for at least one of the at least one first satellite and the at least one second satellite by using at least one of the at least one ranging measurement, the synchronization time, positioning data from the at least one timing satellite, and at least one positioning ranging measurement. - View Dependent Claims (15, 16, 17, 18, 19, 20, 21, 22, 23, 24, 25, 26)
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27. A system for timing for a satellite constellation, the system comprising:
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at least one first satellite configured to transmit at least one first crosslink ranging signal to at least one second satellite, and to receive at least one second crosslink ranging signal; the at least one second satellite configured to receive the at least one first crosslink ranging signal, and to transmit the at least one second crosslink ranging signal, wherein at least one of the at least one first satellite and the at least one second satellite is a timing satellite with a synchronization time; at least one processor configured to calculate at least one first ranging measurement from the at least one first satellite to the at least one second satellite by using an amount of time elapsed from the transmitting of the at least one first crosslink ranging signal to the receiving of the at least one first crosslink ranging signal; the at least one processor further configured to calculate at least one second ranging measurement from the at least one second satellite to the at least one first satellite by using an amount of time elapsed from the transmitting of the at least one second crosslink ranging signal to the receiving of the at least one second crosslink ranging signal the at least one processor further configured to calculate an estimate of time and frequency for the at least one first satellite and the at least one second satellite relative to each other and to the synchronization time to synchronize the time and the frequency for at least one of the at least one first satellite and the at least one second satellite by using at least one of the at least one first ranging measurement, the at least one second ranging measurement, and the synchronization time from the at least one timing satellite; and the at least one processor further configured to calculate an estimate of orbital positioning for at least one of the at least one first satellite and the at least one second satellite by using at least one of the at least one first ranging measurement, the at least one second ranging measurement, the synchronization time, positioning data from the at least one timing satellite, and at least one positioning ranging measurement.
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Specification