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Optics & Optoelectronic Technology

Development of Cold Atom Interferometic Gyroscope

Deng Jian-hu

Published Jan 1, 2014• 1 citation
OpenAlex

Abstract

A comprehensive comparison of atom gyroscope and traditional gyroscope is presented based on the characteristics of high-precision measurement of cold atom.Then a summary of up-to-date progress achieved in the field of atom inertial navigation is presented.Finally,A discussion of the application of atom gyroscope in high-precision inertial navigation is concluede.

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Research Status and Prospects of Cold Atom Interferometry Gyroscope in Inertial Navigation Fields

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With the progress of laser cooling and other atom optics technologies, the cold atom interferometry gyroscope based on cold atom wave is developing rapidly, and it promises to be a novel gyroscope technology in inertial navigation areas. The research status of cold atom interferometry gyroscope and the principle of atom interferometry are introduced, and a comparative analysis of the characteristics among the three distinct types of cold atom interferometry gyroscopes in Stanford University, Observatoire de Paris and Hanover University is carried out. The improving schemes and developing prospects of cold atom interferometry gyroscope are discussed by focusing on its current limitations, aiming at its wider application in inertial navigation fields.

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•Jan 1, 2020•8 citations

Realization of cold atom gyroscope in space

Jinting Li, Xi Chen, Danfang Zhang +21 more

High-precision gyroscopes in space are essential for fundamental physics research and navigation. Due to its potential high precision, the cold atom gyroscope is expected to be the next generation of gyroscopes in space. Here, we report the first realization of a cold atom gyroscope, which was demonstrated by the atom interferometer installed in the China Space Station (CSS) as a payload. By compensating for CSS's high dynamic rotation rate using a built-in piezoelectric mirror, spatial interference fringes in the interferometer are successfully obtained. Then, the optimized ratio of the Raman laser's angles is derived, the coefficients of the piezoelectric mirror are self-calibrated in orbit, and various systemic effects are corrected. We achieve a rotation measurement resolution of 50*10^-6 rad/s for a single shot and 17*10^-6 rad/s for an average number of 32. The measured rotation is (-1142+/-29)*10^-6 rad/s and is compatible with that recorded by the classical gyroscope of the CSS. This study paves the way for developing high-precision cold atom gyroscopes in space.

arXiv:2405.20659•May 31, 2024•1 citation
A comprehensive comparison of atom gyroscope and traditional gyroscope is presented based on the characteristics of high-precision measurement of cold atom.Then a summary of up-to-date progress achieved in the field of atom inertial navigation is presented.Finally,A discussion of the application of atom gyroscope in high-precision inertial navigation is concluede.
With the progress of laser cooling and other atom optics technologies, the cold atom interferometry gyroscope based on cold atom wave is developing rapidly, and it promises to be a novel gyroscope technology in inertial navigation areas. The research status of cold atom interferometry gyroscope and the principle of atom interferometry are introduced, and a comparative analysis of the characteristics among the three distinct types of cold atom interferometry gyroscopes in Stanford University, Observatoire de Paris and Hanover University is carried out. The improving schemes and developing prospects of cold atom interferometry gyroscope are discussed by focusing on its current limitations, aiming at its wider application in inertial navigation fields.
With the rapid development of modern physics, atomic gyroscopes have been demonstrated in recent years. There are two types of atomic gyroscope. The Atomic Interferometer Gyroscope (AIG), which utilizes the atomic interferometer to sense rotation, is an ultra-high precision gyroscope; and the Atomic Spin Gyroscope (ASG), which utilizes atomic spin to sense rotation, features high precision, compact size and the possibility to make a chip-scale one. Recent developments in the atomic gyroscope field have created new ways to obtain high precision gyroscopes which were previously unavailable with mechanical or optical gyroscopes, but there are still lots of problems that need to be overcome to meet the requirements of inertial navigation systems. This paper reviews the basic principles of AIG and ASG, introduces the recent progress in this area, focusing on discussing their technical difficulties for inertial navigation applications, and suggests methods for developing high performance atomic gyroscopes in the near future.
As the core sensors of inertial navigation, the accuracy of gyroscope and accelerometer directly determines the performance of inertial navigation system. With the appearance of cold atom interference technology, it has a wide application prospect in the field of inertial measurement, and cold atom gravimeter and cold atom gyroscope have appeared in succession. This paper mainly introduces the basic principle of cold atom interference technology, and briefly describes the development status of cold atom gyroscope and accelerometer. The existing problems in the current research is summarized, and its future application in navigation are prospected.
In this paper,we described the progress of cold atom gyroscope.We launched the atoms along the same trajectory accurately and the opposite direction by controlling the frequency of directed digital system circuit.Using stimulated Raman beams,we operated the cold atoms and realized the atom interferometer fringes.With this configuration,it will greatly eliminate the common mode noise caused by uncertainty factor,such as the phase of the Raman laser beams,the gravity acceleration.It will significantly improve the precision in our experiment.The atom gyroscope will give a new way for the inertial navigation technology in the future.
This report assesses the potential of gyroscopes and accelerometers based on cold atom interferometry (CAI) for space and defence applications, by analysing their strengths and weaknesses in comparison with devices based on other working principles. Indeed, it is widely recognized that quantum sensors based on atomic interferometry provide absolute measurements with the potential for high sensitivity and long-term stability. This last property is particularly valuable for accelerometers and gyroscopes to be used for inertial navigation, since it guarantees precise positioning without the need for frequent recalibrations, a shortcoming which affects several devices presently in use. \nHigh-performance inertial sensors play an important role both in space applications, where gyroscopes are widely used e.g. to orientate a satellite and its on-board communications and sensing equipment, and in defence, where gyroscopes and accelerometers constitute the core of the inertial measurement units to be used for autonomous navigation, e.g. in GNSS-denied conditions. The EU has a well-established role in space with the Copernicus and Galileo programmes, and a fledging but increasing involvement in the defence industry. An independent assessment of a quantum technology such as cold atom interferometry which may in time acquire a significant role in these fields is a precondition to advance well-grounded suggestions for EU policy initiatives.
High-precision gyroscopes in space are essential for fundamental physics research and navigation. Due to its potential high precision, the cold atom gyroscope is expected to be the next generation of gyroscopes in space. Here, we report the first realization of a cold atom gyroscope, which was demonstrated by the atom interferometer installed in the China Space Station (CSS) as a payload. By compensating for CSS's high dynamic rotation rate using a built-in piezoelectric mirror, spatial interference fringes in the interferometer are successfully obtained. Then, the optimized ratio of the Raman laser's angles is derived, the coefficients of the piezoelectric mirror are self-calibrated in orbit, and various systemic effects are corrected. We achieve a rotation measurement resolution of 50*10^-6 rad/s for a single shot and 17*10^-6 rad/s for an average number of 32. The measured rotation is (-1142+/-29)*10^-6 rad/s and is compatible with that recorded by the classical gyroscope of the CSS. This study paves the way for developing high-precision cold atom gyroscopes in space.