HEAD MOUNTED DISPLAY (HMD) DEVICE CALIBRATION BASED ON HINGE MOTION

    公开(公告)号:US20250008076A1

    公开(公告)日:2025-01-02

    申请号:US18344549

    申请日:2023-06-29

    Abstract: Systems and techniques are described herein for using head mounted display (HMD) hinge motion to calibrate the head mounted device. For example, an device (or component of the device) can obtain, via one or more sensors, sensor measurements during rotation of a display of the HMD between a first end of a range of motion of a hinge of the display about an axis and a second end of the range of motion of the hinge about the axis; determine parameters of the HMD based on the sensor measurements and the rotation of the display between the first end of the range of motion of the hinge and the second end of the range of motion of the hinge about the axis; and determine pose information for the HMD based on the determined parameters.

    METHOD AND APPARATUS FOR IN MOTION INITIALIZATION OF GLOBAL NAVIGATION SATELLITE SYSTEM - INERTIAL NAVIGATION SYSTEM

    公开(公告)号:US20220011447A1

    公开(公告)日:2022-01-13

    申请号:US16927337

    申请日:2020-07-13

    Abstract: A mobile device in a moving vehicle initializes a Global Navigation Satellite System (GNSS)-Inertial Navigation System (INS) system while the vehicle is in-motion with the orientation of the mobile device with respect to a global reference frame. The mobile device uses gyroscope measurements made while the vehicle is turning to determine a gravity vector. The gravity vector and accelerometer measurements may be used to determine a forward vector for the mobile device. A north vector is determined using the GNSS measurements. After the GNSS-INS system is calibrated, the mobile device may be positioned with respect to the vehicle. The orientation of the mobile device, prior to repositioning, may be compared to a current orientation, determined while the vehicle is in motion, in order to determine whether the GNSS-INS system should be re-initialized.

    CORRECTION OF MOTION SENSOR AND GLOBAL NAVIGATION SATELLITE SYSTEM DATA OF A MOBILE DEVICE IN A VEHICLE

    公开(公告)号:US20220326015A1

    公开(公告)日:2022-10-13

    申请号:US17852179

    申请日:2022-06-28

    Abstract: Aspects of the disclosure relate to initializing an inertial navigation system (INS) of a mobile device. Accelerometer bias of a plurality of accelerometers of the mobile device, and gyroscope bias of a plurality of gyroscopes of the mobile device, are determined. A first spatial relationship between a first frame of reference of the mobile device and a second frame of reference of a vehicle transporting the mobile device is determined. A second spatial relationship between the first frame of reference and a third frame of reference of a surface beneath the vehicle is determined. Each of the frames of reference are determined based on output of at least two of the GNSS receiver, the plurality of accelerometers, or the plurality of gyroscopes. The INS is provided with the accelerometer bias, the gyroscope bias, the first spatial relationship, and the second spatial relationship to initialize the INS.

    CORRECTION OF MOTION SENSOR AND GLOBAL NAVIGATION SATELLITE SYSTEM DATA OF A MOBILE DEVICE IN A VEHICLE

    公开(公告)号:US20210207961A1

    公开(公告)日:2021-07-08

    申请号:US16735356

    申请日:2020-01-06

    Abstract: Aspects of the disclosure relate to initializing an inertial navigation system (INS) of a mobile device. Accelerometer bias of a plurality of accelerometers of the mobile device, and gyroscope bias of a plurality of gyroscopes of the mobile device, are determined. A first spatial relationship between a first frame of reference of the mobile device and a second frame of reference of a vehicle transporting the mobile device is determined. A second spatial relationship between the first frame of reference and a third frame of reference of a surface beneath the vehicle is determined. Each of the frames of reference are determined based on output of at least two of the GNSS receiver, the plurality of accelerometers, or the plurality of gyroscopes. The INS is provided with the accelerometer bias, the gyroscope bias, the first spatial relationship, and the second spatial relationship to initialize the INS.

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