A New Silicon Tuning Fork Gyroscope for Aerospace Applications

被引:0
|
作者
Chaumet, B. [1 ]
Leverrier, B.
Rougeot, C.
Bouyat, S. [1 ]
机构
[1] THALES Avion, F-86101 Chatellerault, France
关键词
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
For several years THALES Aerospace has been developing a silicon micro-machined tuning fork gyroscope for military and civil applications. The targeted performance is: bias and scale factor errors of 10 degrees/h and 500ppm for a range of 1000 degrees/s. The technology is based on Deep Reactive Ion Etching (DRIE) on a SOI wafer. Associated with an in-plane design for the drive and sense modes, this technology leads to a high geometric precision and allows the realization of the sense and the drive mechanical resonators, and trimming elements within a single active layer. Good bias stability is achieved by cancelling the quadrature bias with electrostatic trimming. The signal processing of the gyro is primarily digital and consists of two main closed loops, for controlling the drive and sense modes, and an auxiliary loop for cancelling the quadrature bias. The typical results obtained on a demonstrator of a third generation device are the following: random walk=0.01 degrees/root h, bias instability<0.1 degrees/h, noise of 0.005 degrees/s over 0-50Hz, with a 1000 degrees/s range (adjustable by the electronics), bias and scale factor errors of 8 degrees/h and 28 ppm in the temperature range -25 degrees C, 70 degrees C, linearity error<0.1 degrees/s over 1000 degrees/s. A high g shock test of 20000g has been carried out on a hardened prototype without any observable performance degradation.
引用
收藏
页数:13
相关论文
共 50 条
  • [41] A Tuning Fork Gyroscope with a Polygon-Shaped Vibration Beam
    Xu, Qiang
    Hou, Zhanqiang
    Kuang, Yunbin
    Miao, Tongqiao
    Ou, Fenlan
    Zhuo, Ming
    Xiao, Dingbang
    Wu, Xuezhong
    MICROMACHINES, 2019, 10 (12)
  • [42] Construction of a new-type tuning fork vibratory gyroscope using a single resonance mode
    Sugawara, Sumio
    Tomikawa, Yoshiro
    Japanese Journal of Applied Physics, Part 1: Regular Papers & Short Notes & Review Papers, 2000, 39 (7 A): : 4249 - 4252
  • [43] Construction of a new-type tuning fork vibratory gyroscope using a single resonance mode
    Sugawara, S
    Tomikawa, Y
    JAPANESE JOURNAL OF APPLIED PHYSICS PART 1-REGULAR PAPERS SHORT NOTES & REVIEW PAPERS, 2000, 39 (7A): : 4249 - 4252
  • [44] Tuning fork silicon angular rate sensor with enhanced performance for automotive applications
    Sassen, S
    Voss, R
    Schalk, J
    Stenzel, E
    Gleissner, T
    Gruenberger, R
    Neubauer, F
    Ficker, W
    Kupke, W
    Bauer, K
    Rose, M
    SENSORS AND ACTUATORS A-PHYSICAL, 2000, 83 (1-3) : 80 - 84
  • [45] Design and analysis of MEMS tuning fork gyroscope with dual mode ordering
    Jia, Lu
    Han, Guowei
    Wei, Zhenyu
    Si, Chaowei
    Ning, Jin
    Yang, Fuhua
    Han, Weihua
    MICROWAVE AND OPTICAL TECHNOLOGY LETTERS, 2024, 66 (01)
  • [46] A high-Q in-plane SOI tuning fork gyroscope
    Sharma, A
    Zaman, FM
    Amini, BV
    Ayazi, F
    PROCEEDINGS OF THE IEEE SENSORS 2004, VOLS 1-3, 2004, : 467 - 470
  • [47] Finite element simulation of the vibratory characteristics for quartz tuning fork gyroscope
    Wang, Ying
    Sun, Yu-Nan
    Qin, Bing-Kun
    Journal of Beijing Institute of Technology (English Edition), 2002, 11 (02): : 155 - 158
  • [48] Structure design of a novel micromachinined tuning fork gyroscope with high robustness
    Chen, W. P.
    Yang, Y. B.
    Yu, Y.
    MICRO-NANO TECHNOLOGY XIII, 2012, 503 : 108 - +
  • [49] Design and simulation of a tuning fork micromachined gyroscope with slide film damping
    CHE Lufeng XIONG Bin JIAO Jiwei WANG Yuelin State Key Laboratory of Transducer Technology Shanghai Institute of Microsystem and Information Technology Chinese Academy of Sciences Shanghai China
    光学精密工程, 2005, (05) : 519 - 524
  • [50] Analysis of acceleration sensitivity in frequency decoupled MEMS tuning fork gyroscope
    Singh, Thakur Praveen
    Sugano, Koji
    Tsuchiya, Toshiyuki
    Tabata, Osamu
    EUROSENSORS XXV, 2011, 25