Towards a GNSS-assisted autonomous heterogeneous clock system for very small satellites in the Earth-Moon system

There is an increasing interest in science and exploration missions in the Earth-Moon system. These missions call for simple, efficient and accurate timing onboard of these spacecraft. A heterogeneous onboard timing system is proposed, presented and characterized, which comprises an Oven-Controlled Crystal Oscillator (OCXO) and one or several Chip Scale Atomic Clocks (CSACs), providing nano-second timing accuracy on time scales of seconds to hours. To extend the stability of this system to days, weeks and months, it is assisted by a Global Navigation Satellite Systems (GNSS) timing receiver, which is operated in snapshot mode and activated only for very short time durations of a few seconds on a daily or weekly basis, based on the mission needs. This innovative GNSS assistance replaces the ground-based synchronisation and offers an autonomous operations of the onboard timing system. In this way, a highly accurate yet very low Size, Weight and Power (SWaP) system can be realized, which can be used on very small satellites down to nano-satellites. The onboard architecture of this system is presented and characterised in terms of its achievable Allan deviations as well as its SWaP. It is found that the average power consumption can be as low as 2.2 W, based on a daily GNSS synchronisation schedule, significantly reducing the power requirements over current state-of-the-art solutions. An even less complex variant of this innovative system can be employed for any deep space or planetary mission, replacing the onboard GNSS timing receiver by a traditional time synchronisation mechanism using a terrestrial ground station, or, in the further future, using a pulsar. • Two-component heterogenous clock system of OCXO – CSAC proposed for very small satellites in Earth-Moon System • Provides stable performance above 10 -12 for time scales of 1-10,000 seconds with power consumption of 2.2 W • Innovative extension to three-component clock system by GNSS receiver in snapshot mode • Three-component clock system essentially does not increase power consumption and maintains autonomy of system

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Publication Details

Journal
Acta Astronautica
Published
2025-05-05
DOI
https://doi.org/10.1016/j.actaastro.2025.04.043
Primary Topic
Advanced Frequency and Time Standards
Type
article
Field-Weighted Citation Impact
0.00

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article

Towards a GNSS-assisted autonomous heterogeneous clock system for very small satellites in the Earth-Moon system

S. E. Palo, Eberhard Gill
1 links
Acta Astronautica
Advanced Frequency and Time Standards
article

Towards a GNSS-assisted autonomous heterogeneous clock system for very small satellites in the Earth-Moon system

S. E. Palo, Eberhard Gill
article en

Abstract

There is an increasing interest in science and exploration missions in the Earth-Moon system. These missions call for simple, efficient and accurate timing onboard of these spacecraft. A heterogeneous onboard timing system is proposed, presented and characterized, which comprises an Oven-Controlled Crystal Oscillator (OCXO) and one or several Chip Scale Atomic Clocks (CSACs), providing nano-second timing accuracy on time scales of seconds to hours. To extend the stability of this system to days, weeks and months, it is assisted by a Global Navigation Satellite Systems (GNSS) timing receiver, which is operated in snapshot mode and activated only for very short time durations of a few seconds on a daily or weekly basis, based on the mission needs. This innovative GNSS assistance replaces the ground-based synchronisation and offers an autonomous operations of the onboard timing system. In this way, a highly accurate yet very low Size, Weight and Power (SWaP) system can be realized, which can be used on very small satellites down to nano-satellites. The onboard architecture of this system is presented and characterised in terms of its achievable Allan deviations as well as its SWaP. It is found that the average power consumption can be as low as 2.2 W, based on a daily GNSS synchronisation schedule, significantly reducing the power requirements over current state-of-the-art solutions. An even less complex variant of this innovative system can be employed for any deep space or planetary mission, replacing the onboard GNSS timing receiver by a traditional time synchronisation mechanism using a terrestrial ground station, or, in the further future, using a pulsar. • Two-component heterogenous clock system of OCXO – CSAC proposed for very small satellites in Earth-Moon System • Provides stable performance above 10 -12 for time scales of 1-10,000 seconds with power consumption of 2.2 W • Innovative extension to three-component clock system by GNSS receiver in snapshot mode • Three-component clock system essentially does not increase power consumption and maintains autonomy of system

Acta AstronauticaVol. 234
University of Colorado Boulder (US), Delft University of Technology (NL)
Technische Universiteit Delft
Openalex Percentile: Top 93%
Advanced Frequency and Time Standards
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