High-Rate GPS Velocity and Acceleration Determination in Highly Dynamic Flights

Research output: Chapter in book/report/conference proceedingConference contributionResearchpeer review

Authors

  • C. Bischof
  • S. Schön

Research Organisations

View graph of relations

Details

Original languageEnglish
Title of host publicationProceedings of the 28th International Technical Meeting of the Satellite Division of The Institute of Navigation
Pages3069-3076
Number of pages8
ISBN (electronic)9781510817258
Publication statusPublished - 2015
Event28th International Technical Meeting of the Satellite Division of the Institute of Navigation, ION GNSS 2015 - Tampa, United States
Duration: 14 Sept 201518 Sept 2015

Abstract

GPS receivers typically have update rates of at least 1 Hz at which error characteristics are relatively well known. Therefore, the update rate is usually well below the bandwidth of the phase lock loop, which in theory, when neglecting the impact of atmospheric fluctuations or multipath, results in stochastically independent carrier phase measurements. However, for GPS receivers with update rates up to 100 Hz, the probability of correlations stemming from the receiver is severely increased. Consequently, its impact on high rate position, velocity and acceleration estimates need to be assessed. This contribution investigates the stochastic characteristics of GPS L1 double difference, GPS D1 Doppler and time-differenced GPS D1 Doppler measurements during static and kinematic periods, for measurement update rates from 0.1 Hz to 100 Hz. This information is used to set up a position, velocity, acceleration and time Extended Kalman Filter. Systematic errors during high dynamic stress situations are then characterized based on the comparison of the PVAT EKF solution against an IMU derived solution in a controlled environment of a shaking table. Finally, preliminary acceleration results from a short section of a flight trajectory are shown.

ASJC Scopus subject areas

Cite this

High-Rate GPS Velocity and Acceleration Determination in Highly Dynamic Flights. / Bischof, C.; Schön, S.
Proceedings of the 28th International Technical Meeting of the Satellite Division of The Institute of Navigation. 2015. p. 3069-3076.

Research output: Chapter in book/report/conference proceedingConference contributionResearchpeer review

Bischof, C & Schön, S 2015, High-Rate GPS Velocity and Acceleration Determination in Highly Dynamic Flights. in Proceedings of the 28th International Technical Meeting of the Satellite Division of The Institute of Navigation. pp. 3069-3076, 28th International Technical Meeting of the Satellite Division of the Institute of Navigation, ION GNSS 2015, Tampa, United States, 14 Sept 2015. <https://www.ion.org/sign-in.cfm>
Bischof, C., & Schön, S. (2015). High-Rate GPS Velocity and Acceleration Determination in Highly Dynamic Flights. In Proceedings of the 28th International Technical Meeting of the Satellite Division of The Institute of Navigation (pp. 3069-3076) https://www.ion.org/sign-in.cfm
Bischof C, Schön S. High-Rate GPS Velocity and Acceleration Determination in Highly Dynamic Flights. In Proceedings of the 28th International Technical Meeting of the Satellite Division of The Institute of Navigation. 2015. p. 3069-3076
Bischof, C. ; Schön, S. / High-Rate GPS Velocity and Acceleration Determination in Highly Dynamic Flights. Proceedings of the 28th International Technical Meeting of the Satellite Division of The Institute of Navigation. 2015. pp. 3069-3076
Download
@inproceedings{763503d0187248d9b23f772b10aeff22,
title = "High-Rate GPS Velocity and Acceleration Determination in Highly Dynamic Flights",
abstract = "GPS receivers typically have update rates of at least 1 Hz at which error characteristics are relatively well known. Therefore, the update rate is usually well below the bandwidth of the phase lock loop, which in theory, when neglecting the impact of atmospheric fluctuations or multipath, results in stochastically independent carrier phase measurements. However, for GPS receivers with update rates up to 100 Hz, the probability of correlations stemming from the receiver is severely increased. Consequently, its impact on high rate position, velocity and acceleration estimates need to be assessed. This contribution investigates the stochastic characteristics of GPS L1 double difference, GPS D1 Doppler and time-differenced GPS D1 Doppler measurements during static and kinematic periods, for measurement update rates from 0.1 Hz to 100 Hz. This information is used to set up a position, velocity, acceleration and time Extended Kalman Filter. Systematic errors during high dynamic stress situations are then characterized based on the comparison of the PVAT EKF solution against an IMU derived solution in a controlled environment of a shaking table. Finally, preliminary acceleration results from a short section of a flight trajectory are shown.",
author = "C. Bischof and S. Sch{\"o}n",
year = "2015",
language = "English",
pages = "3069--3076",
booktitle = "Proceedings of the 28th International Technical Meeting of the Satellite Division of The Institute of Navigation",
note = "28th International Technical Meeting of the Satellite Division of the Institute of Navigation, ION GNSS 2015 ; Conference date: 14-09-2015 Through 18-09-2015",

}

Download

TY - GEN

T1 - High-Rate GPS Velocity and Acceleration Determination in Highly Dynamic Flights

AU - Bischof, C.

AU - Schön, S.

PY - 2015

Y1 - 2015

N2 - GPS receivers typically have update rates of at least 1 Hz at which error characteristics are relatively well known. Therefore, the update rate is usually well below the bandwidth of the phase lock loop, which in theory, when neglecting the impact of atmospheric fluctuations or multipath, results in stochastically independent carrier phase measurements. However, for GPS receivers with update rates up to 100 Hz, the probability of correlations stemming from the receiver is severely increased. Consequently, its impact on high rate position, velocity and acceleration estimates need to be assessed. This contribution investigates the stochastic characteristics of GPS L1 double difference, GPS D1 Doppler and time-differenced GPS D1 Doppler measurements during static and kinematic periods, for measurement update rates from 0.1 Hz to 100 Hz. This information is used to set up a position, velocity, acceleration and time Extended Kalman Filter. Systematic errors during high dynamic stress situations are then characterized based on the comparison of the PVAT EKF solution against an IMU derived solution in a controlled environment of a shaking table. Finally, preliminary acceleration results from a short section of a flight trajectory are shown.

AB - GPS receivers typically have update rates of at least 1 Hz at which error characteristics are relatively well known. Therefore, the update rate is usually well below the bandwidth of the phase lock loop, which in theory, when neglecting the impact of atmospheric fluctuations or multipath, results in stochastically independent carrier phase measurements. However, for GPS receivers with update rates up to 100 Hz, the probability of correlations stemming from the receiver is severely increased. Consequently, its impact on high rate position, velocity and acceleration estimates need to be assessed. This contribution investigates the stochastic characteristics of GPS L1 double difference, GPS D1 Doppler and time-differenced GPS D1 Doppler measurements during static and kinematic periods, for measurement update rates from 0.1 Hz to 100 Hz. This information is used to set up a position, velocity, acceleration and time Extended Kalman Filter. Systematic errors during high dynamic stress situations are then characterized based on the comparison of the PVAT EKF solution against an IMU derived solution in a controlled environment of a shaking table. Finally, preliminary acceleration results from a short section of a flight trajectory are shown.

UR - http://www.scopus.com/inward/record.url?scp=84975796923&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:84975796923

SP - 3069

EP - 3076

BT - Proceedings of the 28th International Technical Meeting of the Satellite Division of The Institute of Navigation

T2 - 28th International Technical Meeting of the Satellite Division of the Institute of Navigation, ION GNSS 2015

Y2 - 14 September 2015 through 18 September 2015

ER -