HIGH-CONTRAST ATOMIC INERTIAL INTERFEROMETRY WITH FREQUENCY COMB OR COMB-LIKE LIGHT SOURCE

    公开(公告)号:US20240328786A1

    公开(公告)日:2024-10-03

    申请号:US18191541

    申请日:2023-03-28

    Inventor: Robert Compton

    Abstract: An atomic inertial interferometer comprises a laser that emits a CW beam; a modulator that modulates the CW beam; a filter and delay mechanism that receives the modulated beam, and includes a first pathway and a second pathway longer than the first pathway; a comb generator that receives the modulated beam, and produces a frequency comb; and a comb drive coupled to the comb generator to generate a multiple of a comb repetition rate, the comb drive including a HF source coupled to a bandpass filter. A vacuum cell holds a sample of cold atoms. The frequency comb counter-propagates with respect to the modulated beam to provide velocity slicing of the cold atoms such that a given temperature distribution of the cold atoms is sliced into a plurality of narrow temperature distributions that are probed individually and in parallel, to extract an interference signal from the narrow temperature distributions.

    MITIGATING SYSTEMATIC ERROR IN GYROCOMPASSING

    公开(公告)号:US20240133713A1

    公开(公告)日:2024-04-25

    申请号:US18484878

    申请日:2023-10-11

    Inventor: Jaakko RUOHIO

    CPC classification number: G01C25/00 G01C19/58

    Abstract: A MEMS gyrocompass and method are provided to mitigate systematic error in determination of a north angle. The MEMS gyrocompass includes one or more MEMS gyroscopes having a sense axis within a reference plane. Samples from an output of the MEMS gyroscope are obtained in at least two angles of rotation about an axis perpendicular to the reference plane. First fit coefficients are determined by fitting samples with first fitting functions determined as function of time. Second fit coefficients are determined by fitting components of earth rotation rate projected on the reference plane based on samples obtained by all the MEMS gyroscopes, which fitting is performed with a second fitting function determined as a function of rotation angle of the MEMS gyroscope with respect to a reference angle. The north angle is determined as an angle between the reference angle and true north based on the second fit coefficients.

    Systems and methods for eliminating multi-path errors from atomic inertial sensors

    公开(公告)号:US09887019B2

    公开(公告)日:2018-02-06

    申请号:US15016180

    申请日:2016-02-04

    CPC classification number: G21K1/006 G01C19/58 G01P15/08

    Abstract: Systems and methods for eliminating multi-path errors from atomic inertial sensors are provided. In certain embodiments, a system for performing atom interferometry includes a vacuum cell containing multiple atoms and a first plurality of lasers configured to trap the atoms within the vacuum cell. The system further includes a second plurality of lasers configured to impart momentum to the atoms and direct the atoms down multiple paths, wherein a primary path in the multiple paths has a first and second component that converge at a converging point, wherein a diverging part of the primary path in which the first and second components are diverging is asymmetrical with respect to a converging part of the primary path in which the first and second components are converging, such that only the first and second components converge at the converging point wherein other paths do not converge at the converging point.

    ATOM INTERFEROMETER WITH ADAPTIVE LAUNCH DIRECTION AND/OR POSITION
    9.
    发明申请
    ATOM INTERFEROMETER WITH ADAPTIVE LAUNCH DIRECTION AND/OR POSITION 有权
    具有自适应发射方向和/或位置的ATOM干涉仪

    公开(公告)号:US20170032863A1

    公开(公告)日:2017-02-02

    申请号:US15294510

    申请日:2016-10-14

    Abstract: Embodiments described herein provide for a method of launching atoms in an atom interferometer. The method includes determining a direction of the total effective acceleration force on the atoms, controlling a direction of launch of the atoms for measurement in the atom interferometer based on the direction of the total effective acceleration force, and obtaining measurements from the atoms.

    Abstract translation: 本文描述的实施例提供了在原子干涉仪中发射原子的方法。 该方法包括确定原子上总有效加速力的方向,基于总有效加速力的方向控制原子干涉仪中用于测量的原子的发射方向,并从原子获得测量值。

    RING ARCHITECTURE FOR SEQUENTIAL OPERATION OF AN ATOMIC GYROSCOPE
    10.
    发明申请
    RING ARCHITECTURE FOR SEQUENTIAL OPERATION OF AN ATOMIC GYROSCOPE 有权
    用于原子晶体的顺序操作的环形结构

    公开(公告)号:US20160298967A1

    公开(公告)日:2016-10-13

    申请号:US14214767

    申请日:2014-03-15

    Abstract: Compact inertial measurement systems and methods based on atom interferometry. Certain examples provide a combination atomic accelerometer-gyroscope configured to recapture and cycle atom samples through atom interferometers arranged to allow the next measurement to use the atoms from the previous measurement. Examples of the apparatus provide inertial measurements indicative of rotation for different inertial axes by applying atom interferometry to a plurality of atom samples launched in opposite directions to allow for measurement of both acceleration and rotation rates. In some examples, the inertial measurement apparatus provide a combined atomic gyroscope and an atomic accelerometer in a compact six Degrees of Freedom (6 DOF) IMU.

    Abstract translation: 基于原子干涉测量的紧凑型惯性测量系统和方法。 某些示例提供了一种组合原子加速度计 - 陀螺仪,其被配置为通过布置成允许下次测量使用来自先前测量的原子的原子干涉仪来重新捕获和循环原子样品。 该装置的实例通过将原子干涉测量法应用于沿相反方向发射的多个原子样品,提供表示不同惯性轴的旋转的惯性测量,以允许测量加速度和旋转速率。 在一些示例中,惯性测量装置提供了一种紧凑的六自由度(6自由度)IMU中的组合原子陀螺仪和原子加速度计。

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