Lagrange reversion theorem

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A vibrating structure gyroscope, standardised by IEEE as Coriolis vibratory gyroscope (CVG),[1] is a wide group of gyroscope using solid-state resonators of different shapes that functions much like the halteres of an insect.

The underlying physical principle is that a vibrating object tends to continue vibrating in the same plane as its support rotates. In the engineering literature, this type of device is also known as a Coriolis vibratory gyro because as the plane of oscillation is rotated, the response detected by the transducer results from the Coriolis term in its equations of motion ("Coriolis force").

Vibrating structure gyroscopes are simpler and cheaper than conventional rotating gyroscopes of similar accuracy. Miniature devices using this principle are a relatively inexpensive type of attitude indicator.

Theory of operation

Consider two proof masses vibrating in plane (as in the MEMS gyro) at frequency . Recall that the Coriolis effect induces an acceleration on the proof masses equal to , where is a velocity and is an angular rate of rotation. The in-plane velocity of the proof masses is given by: , if the in-plane position is given by . The out-of-plane motion , induced by rotation, is given by:


is a mass of the proof mass,
is a spring constant in the out of plane direction,
is a magnitude of a rotation vector in the plane of and perpendicular to the driven proof mass motion.

In application to axi-symmetric thin-walled structures like beams and shells, Coriolis forces cause a precession of vibration patterns around the axis of rotation. For such shells, it causes a slow precession of a standing wave around this axis, with an angular rate that differs from input one. This is the wave inertia effect, discovered in 1890 by British scientist George Hartley Bryan (1864–1928).[2]

If we consider a polarization of a shear (transverse) elastic wave propagating along an acoustic axis in a solid—a polarization rotation effect from rotation of the body as a whole (the polarization inertia effect) can be observed too. (It was noted by Ukrainian scientist Sergii A. Sarapuloff in the early 1980s,[3] It also produces a corresponding modification of Green-Christoffel's tensors in Acoustics[4][5]).



Piezoelectric gyroscopes

A piezoelectric material can be induced to vibrate, and lateral motion due to centrifugal force can be measured to produce a signal related to the rate of rotation.[6]

Wine-glass resonator

Also called a Hemispherical Resonator Gyroscope or HRG, a wine-glass resonator makes using a thin solid-state hemisphere, anchored by a thick stem, and driven to a flexural resonance of this shell, the nodal points of which are measured to detect rotation. There are two basic variants of such a system: one based on a rate regime of operation (so-called, "force-to-rebalance mode") and another variant based on an integrating regime of operation (so-called, "whole-angle mode"). Usually, the latter one is used in combination with a controlled parametric excitation. It is possible to use the both regimes with same hardware, which is a feature unique to these gyroscopes. For a single-piece design (i.e., the hemispherical cup and stem(s) form a monolithic part) made from high-purity quartz glass, it is possible to reach Q-factor over 30-50 millions in vacuum, so, the corresponding random walks are extremely low. The Q is limited by coating (extremely thin film of gold or platinum) and by fixture losses.[7] Such resonators have to be fine-tuned by ion-beam micro-erosion of the glass or by laser ablation. Engineers and researchers in several countries have been working on further improvements of these sophisticated state-of-art technologies.[8]

Cylindrical resonator gyroscope (CRG)

This type of gyroscope was developed by GE Marconi and GE Ferranti in 80s using alloys with attached piezoelectri elements and single-piece piezoceramic design, then, in 90s, CRGs with magneto-electric excitation and readout were produced by Inertial Engineering, Inc. (CA, USA), and piezo-ceramic variants by Watson Industries, and a recently patented variant by Innalabs uses cylindrical design resonator made from Elinvar-type alloy with piezoceramic elements for excitation and pickoff at its perforated bottom. This breakthrough technologies allowed substantially increase product life of the gyroscopes (MTBF > 500,000 hours) and their shock resistance (>300g) that looks enough for "tactical" (mid-accuracy) applications. The resonator is operated on its second order resonant modes. The Q-factor is usually about 20,000 that pre-determine its noises and angle random walks. Standing waves are therefore elliptical shape oscillations with four antinodes and four nodes located circumferentially along the rim, angle between two adjacent antinode – node being 45 deg. One of the elliptical resonant modes is excited to a prescribed amplitude. When the device rotates about its sensitive axis (along its inner stem), the resulting Coriolis forces acting on the resonator’s vibrating mass elements excite the second resonant mode. Angle between major axis of the two modes is 45 deg. A closed-loop drives the second resonant mode to zero and the force required to null this mode is proportional to the input rotation rate. Corresponding control loop system is called force-rebalanced mode. Piezo-electric elements on the resonator produce forces and sense induced motions. This electromechanical system provides the low output noise and large dynamic range that demanding applications require, but suffers from intense acoustic noises and high overloads.

Tuning fork gyroscope

This type of gyroscope uses a pair of test masses driven to resonance. Their displacement from the plane of oscillation is measured to produce a signal related to the system's rate of rotation.

F.W. Meredith registered a patent for such a device in 1942 while working at the Royal Aircraft Establishment. Further development was carried out at the RAE in the late 1950s by G.H. Hunt and A.E.W. Hobbs, who demonstrated drift of less than 1 °/h (3.6×10−4 °/s).[9]

Modern variants of tactical gyros use doubled tuning forks such as those produced by Systron Donner (CA, USA) and SAGEM Défence Securité / Safran Group (France).[10]

Vibrating wheel gyroscope

A wheel is driven to rotate a fraction of a full turn about its axis. The tilt of the wheel is measured to produce a signal related to the rate of rotation.[11]

MEMS gyroscopes

Inexpensive vibrating structure gyroscopes manufactured with MEMS technology have become widely available. These are packaged similarly to other integrated circuits and may provide either analog or digital outputs. In many cases, a single part includes gyroscopic sensors for multiple axes. Some parts incorporate multiple gyroscopes and accelerometers (or multiple axis gyroscopes and accelerometers, to achieve output that has six full degrees of freedom. These units are called Inertial measurement units, or IMUs. Panasonic, Robert Bosch GmbH, InvenSense, Seiko Epson, Sensonor, STMicroelectronics, and Analog Devices are major manufacturers.

Internally, MEMS gyroscopes use lithographically constructed versions of one or more of the mechanisms outlined above (tuning forks, vibrating wheels, or resonant solids of various designs, i.e., similar to TFG, CRG, or HRG mentioned above).[12]


Spacecraft orientation

The oscillation can also be induced and controlled in the vibrating structure gyroscope for the positioning of spacecraft such as Cassini-Huygens. These small Hemispherical Resonator Gyroscopes made of quartz glass operate in vacuum. There are also prototypes of elastically decoupled Cylindrical Resonator Gyroscopes (CRG)[13][14] made from high-purity single-crystalline sapphire. The high-purity leuko-sapphire have Q-factor in order of value higher than quartz glass used for HRG, but this material is hard and has anisotropy. They provide accurate 3 axis positioning of the spacecraft and are highly reliable over the years as they have no moving parts.


Automotive yaw sensors can be built around vibrating structure gyroscopes. These are used to detect error states in yaw compared to a predicted response when connected as an input to electronic stability control systems in conjunction with a steering wheel sensor.[15] Advanced systems could conceivably offer rollover detection based on a second VSG but it is cheaper to add longitudinal and vertical accelerometers to the existing lateral one to this end.


The Nintendo Game Boy Advance game WarioWare: Twisted! uses a piezoelectric gyroscope to detect rotational movement. The Sony SIXAXIS PS3 controller uses a single MEMS gyroscope to measure the sixth axis (yaw). The Nintendo Wii MotionPlus accessory uses multi-axis MEMS gyroscopes provided by InvenSense to augment the motion sensing capabilities of the Wii Remote.[16] The iPhone, iPad, iPod Touch, Nintendo 3DS, Nexus S and HTC Titan also feature gyroscopes.


Many Image stabilization systems on video and still cameras employ vibrating structure gyroscopes.


Vibrating structure gyroscopes are commonly used in radio-controlled helicopters to help control the helicopter's tail rotor and in radio-controlled airplanes to help keep the attitude steady during flight. They are also used in multirotor flight controllers, since multirotors aren't aerodynamically stable and cannot stay airborne without electronic stabilization.

Industrial robotics

Epson Robots uses a Quartz MEMS Gyroscope, called QMEMS, to detect and control vibrations on their robots. This helps the robots position the robot end effector with high precision in high speed and fast-deceleration motion.[17]


The Segway Human Transporter uses a vibrating structure gyroscope made by Silicon Sensing Systems to stabilize the operator platform.[18]


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External links

  • Proceedings of Anniversary Workshop on Solid-State Gyroscopy (19–21 May 2008. Yalta, Ukraine). - Kyiv-Kharkiv. ATS of Ukraine. 2009. - ISBN 978-976-0-25248-6 Template:Please check ISBN. See also the next meetings at: International Workshops on Solid-State Gyroscopy [1].
  • Silicon Sensing - Case Study: Segway HT
  • Apostolyuk V. Theory and Design of Micromechanical Vibratory Gyroscopes
  • Prandi L., Antonello R., Oboe R., and Biganzoli F. Automatic Mode-Matching in MEMS Vibrating Gyroscopes Using Extremum Seeking Control //IEEE Transactions on Industrial Electronics. 2009. Vol.56. - P.3880-3891.. [2]
  • Prandi L., Antonello R., Oboe R., Caminada C., and Biganzoli F. Open-Loop Compensation of the Quadrature Error in MEMS Vibrating Gyroscopes //Proceedings of 35th Annual Conference of the IEEE Industrial Electronics Society - IECON-2009. 2009. [3]
  1. IEEE Std 1431–2004 Coriolis Vibratory Gyroscopes.
  2. Bryan G.H. On the Beats in the Vibrations of a Revolving Cylinder or Bell //Proc. of Cambridge Phil. Soc. 1890, Nov. 24. Vol.VII. Pt.III. - P.101-111.
  3. Sarapuloff S.A. General Solution of Problem of Elasticity Theory of a Rotated Medium //Mechanics of Gyroscopic Systems. Issue 8. – Kyiv. 1989. – P.57-61. (In Russian.)
  4. Sarapuloff S.A., and Ulitko I.A. Rotation Influence upon Bulk Waves in an Elastic Medium and their Usage in Solid-State Gyroscopy // VIII International Conference on Integrated Navigation Systems. – St. Petersburg. St.-Petersburg. The State Research Center of Russia - Central Scientific & Research Institute "ElektroPribor". RF. 2001. – P.127-129.
  5. Sarapuloff S.A. Polarization Precession Effects for Shear Elastic Waves in Rotated Solids //Proceedings of the 23rd KSNVE (Korean Society for Noise & Vibration Engineering) Annual Spring Conference. Yeosu-city, 24–26 April 2013. – P.842-848.
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  7. Sarapuloff S.A., Rhee H.-N., and Park S.-J. Avoidance of Internal Resonances in Hemispherical Resonator Assembly from Fused Quartz Connected by Indium Solder //Proceedings of the 23rd KSNVE (Korean Society for Noise & Vibration Engineering) Annual Spring Conference. Yeosu-city, 24–26 April 2013. – P.835-841.
  8. Sarapuloff S.A. 15 Years of Solid-State Gyrodynamics Development in the USSR and Ukraine: Results and Perspectives of Applied Theory //Proc. of the National Technical Meeting of Institute of Navigation (Santa Monica, Calif., USA. January 14–16, 1997). – P.151-164.
  9. Collinson, R.P.G. Introduction to Avionics, Second edition, Kluwer Academic Publishers: Netherlands, 2003, p.235
  10. QuapasonTM
  11. Template:Cite web
  12. Bernstein, Jonathan. "An Overview of MEMS Inertial Sensing Technology", Sensors Weekly, February 1, 2003.
  13. Sarapuloff S.A. High-Q Sapphire Resonator of Solid-State Gyroscope CRG-1 – In book: 100 Selected Technologies of Academy of Technological Sciences of Ukraine (ATS of Ukraine). Catalogue. – Published by STCU (Science & Technological Council for Ukraine). Kyiv.
  14. Sarapuloff S. A., Lytvynov L.A., et al. Particularities of Designs and Fabrication Technology of High-Q Sapphire Resonators of CRG-1 Type Solid-State Gyroscopes //XIVth International Conference on Integrated Navigation Systems (28–30 May 2007. St.-Petersburg, RF.). – St.-Petersburg. The State Research Center of Russia - Central Scientific & Research Institute "ElektroPribor". RF. 2007. – P.47-48.
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