Initial Test Results from a 3-axis Vibrating Ring Gyroscope

被引:13
|
作者
Gallacher, B. J. [1 ]
Neasham, J. A. [1 ]
Burdess, J. S. [1 ]
Harris, A. J. [1 ]
机构
[1] Newcastle Univ, INSAT, Newcastle Upon Tyne NE1 7RU, Tyne & Wear, England
来源
INTERNATIONAL MEMS CONFERENCE 2006 | 2006年 / 34卷
关键词
D O I
10.1088/1742-6596/34/1/109
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
There are several application areas where the simultaneous measurement of rates of rotation about three mutually orthogonal axes is required. In this paper the principle features of a 3-axis vibrating ring gyroscope are described. The fabrication process for the gyroscope is presented and employs standard MEMS techniques. The modal properties for the ring are measured experimentally using laser vibrometry and electrostatic sensing and compared with the design predictions. In operation as a rate gyroscope it is necessary to excite the primary motion of the gyroscope and control is amplitude. As Q-factors of vibratory gyroscope are typically of the order 10(3)-10(4) slight variations in environmental conditions will perturb the natural frequency of the primary mode significantly. To ensure the primary motion of the gyroscope is maintained with constant amplitude a control scheme employing both frequency tracking and amplitude control is required. An electronic control system using digital signal processing (DSP) has been developed to ensure excitation of the primary motion occurs at resonance with controlled amplitude. The control scheme employs an embedded processor to generate the drive frequency (via a D/A converter) and to monitor the primary vibration (via an A/D converter). Experimental results from the control scheme highlighting its effectiveness over conventional PLL approaches are presented.
引用
收藏
页码:662 / 667
页数:6
相关论文
共 50 条
  • [21] Analysis and experimental test on dynamic characteristic of 3-axis positioner system
    Jiang, Jun-Xia
    Chen, Qi
    Fang, Qiang
    Ke, Ying-Lin
    Jisuanji Jicheng Zhizao Xitong/Computer Integrated Manufacturing Systems, CIMS, 2009, 15 (05): : 1004 - 1009
  • [22] Methods for Reliability Assessment of MEMS Devices - Case Studies of a MEMS Microphone and a 3-Axis MEMS Gyroscope
    Hokka, J.
    Raami, J.
    Hyvonen, H.
    Broas, M.
    Makkonen, J.
    Li, J.
    Mattila, T. T.
    Paulasto-Krockel, M.
    2012 IEEE 62ND ELECTRONIC COMPONENTS AND TECHNOLOGY CONFERENCE (ECTC), 2012, : 62 - 69
  • [23] DESIGN OF A RING-SHAPED 3-AXIS MICRO FORCE/TORQUE SENSOR
    DIDDENS, D
    REYNAERTS, D
    VANBRUSSEL, H
    SENSORS AND ACTUATORS A-PHYSICAL, 1995, 46 (1-3) : 225 - 232
  • [24] Thermo-Mechanical Simulation of Die-Level Packaged 3-axis MEMS Gyroscope Performance
    Parent, A.
    Welham, C. J.
    Piirainen, T.
    Blomqvist, A.
    2017 DGON INERTIAL SENSORS AND SYSTEMS (ISS), 2017,
  • [25] A Robust Feature Extraction Model for Human Activity Characterization Using 3-Axis Accelerometer and Gyroscope Data
    Bhuiyan, Rasel Ahmed
    Ahmed, Nadeem
    Amiruzzaman, Md
    Islam, Md Rashedul
    SENSORS, 2020, 20 (23) : 1 - 17
  • [26] ADVANCEMENT IN THE MEMS GYROSCOPE FROM A VIBRATING TUNING FORK TO A TUNED RING WITH COMB ELECTRODES
    Forke, Roman
    Tsukamoto, Takashiro
    Shaporin, Alexey
    Weidlich, Sebastian
    Buelz, Daniel
    Hahn, Susann
    Tanaka, Shuji
    Hiller, Karla
    2024 IEEE INTERNATIONAL SYMPOSIUM ON INERTIAL SENSORS AND SYSTEMS, INERTIAL, 2024,
  • [27] Three-axis fiber-optic gyroscope: Development and test results
    Meshkovsky I.K.
    Strigalev V.Ye.
    Deineka G.B.
    Peshekhonov V.G.
    Volynsky D.V.
    Untilov A.A.
    Gyroscopy and Navigation, 2011, 2 (4) : 208 - 213
  • [28] GaAs-based tuning fork microresonators: A first step towards a GaAs-based coriolis 3-axis Micro-Vibrating Rate Gyro (GaAs 3-axis μCVG)
    Roland, I.
    Masson, S.
    Ducloux, O.
    Le Traon, O.
    Bosseboeuf, A.
    SENSORS AND ACTUATORS A-PHYSICAL, 2011, 172 (01) : 204 - 211
  • [29] New Scheme for Vibration Test Applying 3-axis Acceleration Sensors Array
    Wang Wei
    Jiao Jianchao
    Tang Liwei
    Yang Tongqiang
    FRONTIERS OF MANUFACTURING AND DESIGN SCIENCE II, PTS 1-6, 2012, 121-126 : 989 - 993
  • [30] 3-Axis magnetic control: flight results of the TANGO satellite in the PRISMA mission
    Chasset, C.
    Noteborn, R.
    Bodin, P.
    Larsson, R.
    Jakobsson, B.
    CEAS SPACE JOURNAL, 2013, 5 (1-2) : 1 - 17