Improved Inertial Navigation With Cold Atom Interferometry

verfasst von: B. Tennstedt, N. Weddig, S. Schön
Abstract: Abstract: This article discusses chances and challenges of using cold atom interferometers in inertial navigation. The error characteristics of the novel sensor are presented, as well as one option for an online estimation of the different readout errors. An extended Kalman filter framework is derived and analysed which uses the readout of the atom interferometer as observation in order to correct several systematic errors of a conventional IMU, allowing for an improved strapdown calculation in an arbitrary target system. The performance gain is discussed analytically based on the steady state variances of the filter, as well as on the example of a simulated scenario for Earth orbit satellites. The correction of the conventional IMU errors is further demonstrated in an experiment under laboratory conditions with a higher class sensor emulating an atom interferometer. While the application of the novel technology as a gyroscope is still limited, as pointed out in the paper, the presented framework yields options for a full six degree of freedom operation of the atom interferometer.
Organisationseinheit(en): Institut für Erdmessung
QuantumFrontiers
Typ: Artikel
Journal: Gyroscopy and Navigation
Band: 12
Seiten: 294-307
Anzahl der Seiten: 14
ISSN: 2075-1087
Publikationsdatum: 12.2021
Publikationsstatus: Veröffentlicht
Peer-reviewed: Ja
ASJC Scopus Sachgebiete: Steuerungs- und Systemtechnik, Informatik (insg.), Elektrotechnik und Elektronik
Elektronische Version(en): https://doi.org/10.1134/S207510872104009X (Zugang: Geschlossen)

BibTeX

@article{b2fe7fc44a2c438299184c6b614b6975,
title = "Improved Inertial Navigation With Cold Atom Interferometry",
abstract = "Abstract: This article discusses chances and challenges of using cold atom interferometers in inertial navigation. The error characteristics of the novel sensor are presented, as well as one option for an online estimation of the different readout errors. An extended Kalman filter framework is derived and analysed which uses the readout of the atom interferometer as observation in order to correct several systematic errors of a conventional IMU, allowing for an improved strapdown calculation in an arbitrary target system. The performance gain is discussed analytically based on the steady state variances of the filter, as well as on the example of a simulated scenario for Earth orbit satellites. The correction of the conventional IMU errors is further demonstrated in an experiment under laboratory conditions with a higher class sensor emulating an atom interferometer. While the application of the novel technology as a gyroscope is still limited, as pointed out in the paper, the presented framework yields options for a full six degree of freedom operation of the atom interferometer.",
keywords = "cold atom interferometry, extended Kalman filter, hybridization, inertial navigation",
author = "B. Tennstedt and N. Weddig and S. Sch{\"o}n",
note = "Funding Information: This work was sponsored by BMWi, project 50RK1957. The authors would like to thank [] for providing the interferometer data for the experimental study in Section 5.1, as well as EXC-2123 QuantumFrontiers – 390837967 for providing a platform of exchange. ",
year = "2021",
month = dec,
doi = "10.1134/S207510872104009X",
language = "English",
volume = "12",
pages = "294--307",
journal = "Gyroscopy and Navigation",
issn = "2075-1087",
publisher = "Pleiades Publishing",
number = "4",
}