HUP0101205A2 - Legalább két irányban változást érzékelő giroszkóp - Google Patents

Legalább két irányban változást érzékelő giroszkóp

Info

Publication number
HUP0101205A2
HUP0101205A2 HU0101205A HUP0101205A HUP0101205A2 HU P0101205 A2 HUP0101205 A2 HU P0101205A2 HU 0101205 A HU0101205 A HU 0101205A HU P0101205 A HUP0101205 A HU P0101205A HU P0101205 A2 HUP0101205 A2 HU P0101205A2
Authority
HU
Hungary
Prior art keywords
resonator element
detects
plane
mode
unit
Prior art date
Application number
HU0101205A
Other languages
English (en)
Inventor
Christopher Fell
Colin Henry John Fox
Original Assignee
Bae Systems Plc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Bae Systems Plc filed Critical Bae Systems Plc
Publication of HUP0101205A2 publication Critical patent/HUP0101205A2/hu
Publication of HUP0101205A3 publication Critical patent/HUP0101205A3/hu

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/56Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/56Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces
    • G01C19/567Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces using the phase shift of a vibration node or antinode
    • G01C19/5677Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces using the phase shift of a vibration node or antinode of essentially two-dimensional vibrators, e.g. ring-shaped vibrators

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Gyroscopes (AREA)

Abstract

A találmány tárgya legalább két irányban változást érzékelő giroszkóp.Lényege, hogy tartalmaz közös tengely (A) körül elterülő belső éskülső peremmel határolt, lényegében síkbeli, gyűrű vagy abroncs alakúvibrációs rezonátorelemet, a rezonátorelemet cos n1Q (ahol n1 <2 egészszám) síkbeli vivőmódusban megrezegtető kialakítású vivőmódus-gerjesztő egységet, a rezonátorelemet rugalmasan megtartótartóegységet, amely tartóegység a rezonátorelemet a tartóegységhezképest a vivőmódus-gerjesztő egység hatására rezgésbe jönni engedőnvan kiképezve, továbbá a rezonátorelem síkbeli kitérését érzékelővivőmódus-érzékelő egységet, valamint a rezonátorelemnek a giroszkópx-tengely körüli elfordulására válaszképpen adott cos nQ (ahol nértéke n1+1 vagy n1-1) nemsíkbeli válaszmódusbeli kitérését érzékelőx-irányú válaszmódus-érzékelő egységet és a rezonátorelemnek agiroszkóp y-tengely körüli elfordulására válaszképpen adott sin nQ(ahol n értéke n1+1 vagy n1-1 és megegyezik az x-irányú válaszmódus n1értékével) nemsíkbeli válaszmódusbeli kitérését érzékelő y-irányúválaszmódus-érzékelő egységet. Ó
HU0101205A 1998-03-14 1999-03-10 A gyroscope sensing rotation at last by two axis HUP0101205A3 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB9805388A GB2335273B (en) 1998-03-14 1998-03-14 A two axis gyroscope
PCT/GB1999/000722 WO1999047890A1 (en) 1998-03-14 1999-03-10 A gyroscope

Publications (2)

Publication Number Publication Date
HUP0101205A2 true HUP0101205A2 (hu) 2001-08-28
HUP0101205A3 HUP0101205A3 (en) 2003-04-28

Family

ID=10828507

Family Applications (1)

Application Number Title Priority Date Filing Date
HU0101205A HUP0101205A3 (en) 1998-03-14 1999-03-10 A gyroscope sensing rotation at last by two axis

Country Status (16)

Country Link
US (2) US6343509B1 (hu)
EP (1) EP1062480B1 (hu)
JP (1) JP4375818B2 (hu)
KR (2) KR100539061B1 (hu)
CN (1) CN1148564C (hu)
AU (2) AU743518B2 (hu)
CA (1) CA2323163A1 (hu)
CZ (1) CZ20003337A3 (hu)
DE (1) DE69900751T2 (hu)
DK (1) DK1062480T3 (hu)
ES (1) ES2165730T3 (hu)
GB (1) GB2335273B (hu)
HU (1) HUP0101205A3 (hu)
NO (1) NO20004572D0 (hu)
PL (1) PL342901A1 (hu)
WO (1) WO1999047890A1 (hu)

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GB0122254D0 (en) * 2001-09-14 2001-11-07 Bae Systems Plc Vibratory gyroscopic rate sensor
GB0122253D0 (en) * 2001-09-14 2001-11-07 Bae Systems Plc Vibratory gyroscopic rate sensor
GB0122252D0 (en) * 2001-09-14 2001-11-07 Bae Systems Plc Vibratory gyroscopic rate sensor
GB0122258D0 (en) * 2001-09-14 2001-11-07 Bae Systems Plc Vibratory gyroscopic rate sensor
GB0206510D0 (en) * 2002-03-20 2002-05-01 Qinetiq Ltd Micro-Electromechanical systems
US7040163B2 (en) * 2002-08-12 2006-05-09 The Boeing Company Isolated planar gyroscope with internal radial sensing and actuation
GB0227098D0 (en) * 2002-11-20 2002-12-24 Bae Systems Plc Method of calibrating bias drift with temperature for a vibrating structure gyroscope
US20050092084A1 (en) * 2003-03-28 2005-05-05 Fell Christopher P. Rate sensing device
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US8079259B2 (en) * 2005-06-27 2011-12-20 Milli Sensor Systems & Actuators MEMS gyroscope with output oscillation about the normal to the plane
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US7543496B2 (en) * 2006-03-27 2009-06-09 Georgia Tech Research Corporation Capacitive bulk acoustic wave disk gyroscopes
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US7958781B2 (en) * 2006-12-15 2011-06-14 Atlantic Inertial Systems Limited Vibrating structure gyroscope
US7493814B2 (en) * 2006-12-22 2009-02-24 The Boeing Company Vibratory gyroscope with parasitic mode damping
US7836765B2 (en) * 2007-07-31 2010-11-23 The Boeing Company Disc resonator integral inertial measurement unit
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EP2239541B1 (en) * 2008-01-29 2013-10-23 Sumitomo Precision Products Co., Ltd. Vibrating gyroscope using piezoelectric film
JP5524045B2 (ja) * 2008-03-25 2014-06-18 住友精密工業株式会社 圧電体膜を用いた振動ジャイロ
JP5524044B2 (ja) * 2008-03-25 2014-06-18 住友精密工業株式会社 圧電体膜を用いた振動ジャイロ
JP5523755B2 (ja) * 2009-02-11 2014-06-18 住友精密工業株式会社 圧電体膜を用いた振動ジャイロ及びその製造方法
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JP2011027561A (ja) * 2009-07-27 2011-02-10 Sumitomo Precision Prod Co Ltd 圧電体膜を用いた振動ジャイロ
US20120125100A1 (en) * 2009-07-27 2012-05-24 Sumitomo Precision Products Co, Ltd. Vibrating gyroscope including piezoelectric film
JP2011027560A (ja) * 2009-07-27 2011-02-10 Sumitomo Precision Prod Co Ltd 圧電体膜を用いた振動ジャイロ
JP2011027562A (ja) * 2009-07-27 2011-02-10 Sumitomo Precision Prod Co Ltd 圧電体膜を用いた振動ジャイロ
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FR2958030B1 (fr) * 2010-03-23 2012-04-20 Sagem Defense Securite Procede et dispositif de mesure angulaire avec compensation de non linearites
US8616056B2 (en) * 2010-11-05 2013-12-31 Analog Devices, Inc. BAW gyroscope with bottom electrode
US8919199B2 (en) 2010-12-01 2014-12-30 Analog Devices, Inc. Apparatus and method for anchoring electrodes in MEMS devices
US9091544B2 (en) * 2010-11-05 2015-07-28 Analog Devices, Inc. XY-axis shell-type gyroscopes with reduced cross-talk sensitivity and/or mode matching
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CN102706337B (zh) * 2012-05-07 2015-08-19 上海交通大学 压电圆盘微机械陀螺
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CN104165624B (zh) * 2014-07-25 2017-01-11 中国人民解放军国防科学技术大学 一种基于侧壁压电驱动的环形振动陀螺及其驱动和检测方法
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Also Published As

Publication number Publication date
CN1292866A (zh) 2001-04-25
AU2739499A (en) 1999-10-11
NO20004572L (no) 2000-09-13
EP1062480B1 (en) 2002-01-02
GB2335273A (en) 1999-09-15
KR100539061B1 (ko) 2005-12-26
GB2335273B (en) 2002-02-27
KR20010041859A (ko) 2001-05-25
NO20004572D0 (no) 2000-09-13
DE69900751T2 (de) 2002-09-26
PL342901A1 (en) 2001-07-16
JP4375818B2 (ja) 2009-12-02
KR20010034602A (ko) 2001-04-25
GB9805388D0 (en) 1998-05-06
US6401534B1 (en) 2002-06-11
AU2739299A (en) 1999-10-11
DE69900751D1 (de) 2002-02-28
DK1062480T3 (da) 2002-04-22
JP2002509615A (ja) 2002-03-26
WO1999047890A1 (en) 1999-09-23
HUP0101205A3 (en) 2003-04-28
CN1148564C (zh) 2004-05-05
ES2165730T3 (es) 2002-03-16
US6343509B1 (en) 2002-02-05
CZ20003337A3 (cs) 2002-01-16
GB2335273A9 (en) 1999-11-16
EP1062480A1 (en) 2000-12-27
AU740992B2 (en) 2001-11-22
KR100511845B1 (ko) 2005-09-02
CA2323163A1 (en) 1999-09-23
AU743518B2 (en) 2002-01-24

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