Details
| Original language | English |
|---|---|
| Title of host publication | 27th International Technical Meeting of the Satellite Division of the Institute of Navigation, ION GNSS 2014 |
| Pages | 2431-2439 |
| Number of pages | 9 |
| ISBN (electronic) | 9781634399913 |
| Publication status | Published - 2014 |
| Event | 27th International Technical Meeting of the Satellite Division of the Institute of Navigation, ION GNSS 2014 - Tampa, United States Duration: 8 Sept 2014 → 12 Sept 2014 |
Abstract
Kinematic GNSS (Global Navigation Satellite Systems) single point positioning (SPP) requires epoch-wise estimation of a receiver synchronization error w.r.t. GNSS system time because of the low long-term stability and the generally poor accuracy of the receiver's internal quartz oscillator. Modeling this error source by a linear polynomial instead of epoch-wise estimation improves the precision of the up-coordinate and makes the adjustment more robust. In this paper we briefly discuss the performance of three different miniaturized atomic frequency standards that were characterized in terms of their frequency stabilities at Physikalisch-Technische Bundesanstalt, Germany. We found significant differences to the manufacturer's data in terms of Allan deviations. In order to analyze the clock performance when connected to GNSS receivers, a kinematic experiment was carried out with a motor vehicle. Applying miniaturized atomic clocks and properly modeling their behavior in kinematic SPP improves the precision of the up-coordinates by up to 58% and the up-velocities by up to 66%, respectively, compared to epoch-wise receiver clock error estimation. Due to remaining systematic effects the accuracy improvements in the coordinate estimates are distinctly smaller. Furthermore, the impact of receiver clock modeling on reliability measures in SPP was investigated. We found improvements in internal reliability of up to 16%-depending on the satellite considered-which makes the positioning solution more robust against gross observation errors.
ASJC Scopus subject areas
- Engineering(all)
- Electrical and Electronic Engineering
- Engineering(all)
- Aerospace Engineering
- Computer Science(all)
- Computer Science Applications
- Computer Science(all)
- Software
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27th International Technical Meeting of the Satellite Division of the Institute of Navigation, ION GNSS 2014. 2014. p. 2431-2439.
Research output: Chapter in book/report/conference proceeding › Conference contribution › Research › peer review
}
TY - GEN
T1 - Applying Miniaturized Atomic Clocks for Improved Kinematic GNSS Single Point Positioning
AU - Krawinkel, T.
AU - Schön, S.
PY - 2014
Y1 - 2014
N2 - Kinematic GNSS (Global Navigation Satellite Systems) single point positioning (SPP) requires epoch-wise estimation of a receiver synchronization error w.r.t. GNSS system time because of the low long-term stability and the generally poor accuracy of the receiver's internal quartz oscillator. Modeling this error source by a linear polynomial instead of epoch-wise estimation improves the precision of the up-coordinate and makes the adjustment more robust. In this paper we briefly discuss the performance of three different miniaturized atomic frequency standards that were characterized in terms of their frequency stabilities at Physikalisch-Technische Bundesanstalt, Germany. We found significant differences to the manufacturer's data in terms of Allan deviations. In order to analyze the clock performance when connected to GNSS receivers, a kinematic experiment was carried out with a motor vehicle. Applying miniaturized atomic clocks and properly modeling their behavior in kinematic SPP improves the precision of the up-coordinates by up to 58% and the up-velocities by up to 66%, respectively, compared to epoch-wise receiver clock error estimation. Due to remaining systematic effects the accuracy improvements in the coordinate estimates are distinctly smaller. Furthermore, the impact of receiver clock modeling on reliability measures in SPP was investigated. We found improvements in internal reliability of up to 16%-depending on the satellite considered-which makes the positioning solution more robust against gross observation errors.
AB - Kinematic GNSS (Global Navigation Satellite Systems) single point positioning (SPP) requires epoch-wise estimation of a receiver synchronization error w.r.t. GNSS system time because of the low long-term stability and the generally poor accuracy of the receiver's internal quartz oscillator. Modeling this error source by a linear polynomial instead of epoch-wise estimation improves the precision of the up-coordinate and makes the adjustment more robust. In this paper we briefly discuss the performance of three different miniaturized atomic frequency standards that were characterized in terms of their frequency stabilities at Physikalisch-Technische Bundesanstalt, Germany. We found significant differences to the manufacturer's data in terms of Allan deviations. In order to analyze the clock performance when connected to GNSS receivers, a kinematic experiment was carried out with a motor vehicle. Applying miniaturized atomic clocks and properly modeling their behavior in kinematic SPP improves the precision of the up-coordinates by up to 58% and the up-velocities by up to 66%, respectively, compared to epoch-wise receiver clock error estimation. Due to remaining systematic effects the accuracy improvements in the coordinate estimates are distinctly smaller. Furthermore, the impact of receiver clock modeling on reliability measures in SPP was investigated. We found improvements in internal reliability of up to 16%-depending on the satellite considered-which makes the positioning solution more robust against gross observation errors.
UR - http://www.scopus.com/inward/record.url?scp=84939250530&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:84939250530
SP - 2431
EP - 2439
BT - 27th International Technical Meeting of the Satellite Division of the Institute of Navigation, ION GNSS 2014
T2 - 27th International Technical Meeting of the Satellite Division of the Institute of Navigation, ION GNSS 2014
Y2 - 8 September 2014 through 12 September 2014
ER -