Performance of miniaturized atomic clocks in static laboratory and dynamic flight environments

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dc.identifier.uri http://dx.doi.org/10.15488/10695
dc.identifier.uri https://www.repo.uni-hannover.de/handle/123456789/10773
dc.contributor.author Jain, Ankit
dc.contributor.author Krawinkel, Thomas
dc.contributor.author Schön, Steffen
dc.contributor.author Bauch, Andreas
dc.date.accessioned 2021-03-30T11:22:28Z
dc.date.available 2021-03-30T11:22:28Z
dc.date.issued 2021
dc.identifier.citation Jain, A.; Krawinkel, T.; Schön, S.; Bauch, A.: Performance of miniaturized atomic clocks in static laboratory and dynamic flight environments. In: GPS Solutions 25 (2021), Nr. 1, 5. DOI: https://doi.org/10.1007/s10291-020-01036-4
dc.description.abstract Miniaturized atomic clocks with high frequency stability as local oscillators in global navigation satellite system (GNSS) receivers promise to improve real-time kinematic applications. For a number of years, such oscillators are being investigated regarding their overall technical applicability, i.e., transportability, and performance in dynamic environments. The short-term frequency stability of these clocks is usually specified by the manufacturer, being valid for stationary applications. Since the performance of most oscillators is likely degraded in dynamic conditions, various oscillators are tested to find the limits of receiver clock modeling in dynamic cases and consequently derive adequate stochastic models to be used in navigation. We present the performance of three different oscillators (Microsemi MAC SA.35m, Spectratime LCR-900 and Stanford Research Systems SC10) for static and dynamic applications. For the static case, all three oscillators are characterized in terms of their frequency stability at Physikalisch-Technische Bundesanstalt, Germany's national metrology institute. The resulting Allan deviations agree well with the manufacturer's data. Furthermore, a flight experiment was conducted in order to evaluate the performance of the oscillators under dynamic conditions. Here, each oscillator is replacing the internal oscillator of a geodetic-grade GNSS receiver and the stability of the receiver clock biases is determined. The time and frequency offsets of the oscillators are characterized with regard to the flight dynamics recorded by a navigation-grade inertial measurement unit. The results of the experiment show that the frequency stability of each oscillator is degraded by about at least one order of magnitude compared to the static case. Also, the two quartz oscillators show a significant g-sensitivity resulting in frequency shifts of - 1.2 × 10 [hoch -9] and + 1.5 × 10 [hoch -9], respectively, while the rubidium clocks are less sensitive, thus enabling receiver clock modeling and strengthening of the navigation performance even in high dynamics. © 2020, The Author(s). eng
dc.language.iso eng
dc.publisher Berlin [u.a.] : Springer
dc.relation.ispartofseries GPS Solutions 25 (2021), Nr. 1
dc.rights CC BY 4.0 Unported
dc.rights.uri https://creativecommons.org/licenses/by/4.0/
dc.subject Allan variance eng
dc.subject flight navigation eng
dc.subject frequency stability eng
dc.subject GNSS eng
dc.subject miniaturized atomic clocks eng
dc.subject.ddc 550 | Geowissenschaften ger
dc.title Performance of miniaturized atomic clocks in static laboratory and dynamic flight environments
dc.type Article
dc.type Text
dc.relation.essn 1521-1886
dc.relation.issn 1080-5370
dc.relation.doi https://doi.org/10.1007/s10291-020-01036-4
dc.bibliographicCitation.issue 1
dc.bibliographicCitation.volume 25
dc.bibliographicCitation.firstPage 5
dc.description.version publishedVersion
tib.accessRights frei zug�nglich


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