Details
| Originalsprache | Englisch |
|---|---|
| Titel des Sammelwerks | 2023 DGON Inertial Sensors and Systems (ISS) |
| Herausgeber/-innen | Peter Hecker |
| ISBN (elektronisch) | 979-8-3503-4724-1 |
| Publikationsstatus | Veröffentlicht - 2023 |
Publikationsreihe
| Name | International Symposium on Inertial Sensors and Systems |
|---|---|
| ISSN (Print) | 2377-3464 |
| ISSN (elektronisch) | 2377-3480 |
Abstract
We present the development of an atom chip system along with associated peripherals for a six-axis quantum inertial navigation sensor based on atom interferometry. Based on quantum mechanical measurement concepts, these sensors are expected to have high sensitivity and superior long-term stability compared to conventional inertial sensors. Furthermore, they enable offset-free absolute measurement. However, the low measurement rate proves to be a disadvantage. Compared to classical inertial sensors, quantum inertial navigation sensors thus exhibit complementary features, so that a combination of these two methods appears promising. The use of inertial measurement systems on board of aircraft or satellites is usually accompanied by limitations in size, payload and power consumption. To meet these requirements, we address both the atom chip system itself and the necessary environment in the form of pumps and vacuum enclosures which are crucial parts of the sensor head.
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2023 DGON Inertial Sensors and Systems (ISS). Hrsg. / Peter Hecker. 2023. (International Symposium on Inertial Sensors and Systems).
Publikation: Beitrag in Buch/Bericht/Sammelwerk/Konferenzband › Aufsatz in Konferenzband › Forschung › Peer-Review
}
TY - GEN
T1 - Miniaturized quantum systems for inertial measurement units
AU - Kassner, A.
AU - Diekmann, L.
AU - Künzler, C.
AU - Petring, J.
AU - Droese, N.
AU - Dencker, F.
AU - Heine, H.
AU - Abend, S.
AU - Gersemann, M.
AU - Rasel, E. M.
AU - Herr, W.
AU - Schubert, C.
AU - Wurz, M. C.
N1 - This work was supported by the German Aerospace Center (DLR) with funds provides by the Federal Ministry for Economic Affairs and Climate Action (BMWK) due to an enactment of the German Bundestag under Grant No. DLR 50NA2106 (QGyroPlus). Furthermore, we would like to thank Simone Callegari and the Physikalisch-Technische Bundesanstalt for carrying out the outgassing measurements.
PY - 2023
Y1 - 2023
N2 - We present the development of an atom chip system along with associated peripherals for a six-axis quantum inertial navigation sensor based on atom interferometry. Based on quantum mechanical measurement concepts, these sensors are expected to have high sensitivity and superior long-term stability compared to conventional inertial sensors. Furthermore, they enable offset-free absolute measurement. However, the low measurement rate proves to be a disadvantage. Compared to classical inertial sensors, quantum inertial navigation sensors thus exhibit complementary features, so that a combination of these two methods appears promising. The use of inertial measurement systems on board of aircraft or satellites is usually accompanied by limitations in size, payload and power consumption. To meet these requirements, we address both the atom chip system itself and the necessary environment in the form of pumps and vacuum enclosures which are crucial parts of the sensor head.
AB - We present the development of an atom chip system along with associated peripherals for a six-axis quantum inertial navigation sensor based on atom interferometry. Based on quantum mechanical measurement concepts, these sensors are expected to have high sensitivity and superior long-term stability compared to conventional inertial sensors. Furthermore, they enable offset-free absolute measurement. However, the low measurement rate proves to be a disadvantage. Compared to classical inertial sensors, quantum inertial navigation sensors thus exhibit complementary features, so that a combination of these two methods appears promising. The use of inertial measurement systems on board of aircraft or satellites is usually accompanied by limitations in size, payload and power consumption. To meet these requirements, we address both the atom chip system itself and the necessary environment in the form of pumps and vacuum enclosures which are crucial parts of the sensor head.
UR - http://www.scopus.com/inward/record.url?scp=85182748208&partnerID=8YFLogxK
U2 - 10.1109/iss58390.2023.10361909
DO - 10.1109/iss58390.2023.10361909
M3 - Conference contribution
SN - 979-8-3503-4725-8
T3 - International Symposium on Inertial Sensors and Systems
BT - 2023 DGON Inertial Sensors and Systems (ISS)
A2 - Hecker, Peter
ER -