Relevant bibliographies by topics / Angular rate

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Angular rate'

Author: Grafiati
Published: 4 June 2021
Last updated: 6 September 2023

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Journal articles on the topic "Angular rate"

1

Kano, Kazuhiko. "Angular Rate Sensor." Journal of the Acoustical Society of America 130, no. 3 (2011): 1775. http://dx.doi.org/10.1121/1.3636045.

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Ogino, Mutsuhito. "Angular rate sensor and mounting structure of angular rate sensor." Journal of the Acoustical Society of America 124, no. 3 (2008): 1393. http://dx.doi.org/10.1121/1.2986184.

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Mochida, Yoichi. "Angular-rate detecting apparatus." Journal of the Acoustical Society of America 121, no. 2 (2007): 685. http://dx.doi.org/10.1121/1.2640142.

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Hall, Gregory W., Jeff R. Crandall, Gregory S. Klopp, and Walter D. Pilkey. "Angular Rate Sensor Joint Kinematics Applications." Shock and Vibration 4, no. 4 (1997): 223–29. http://dx.doi.org/10.1155/1997/243513.

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High speed rotary motion of complex joints were quantified with triaxial angular rate sensors. Angular rate sensors were mounted to rigid links on either side of a joint to measure angular velocities about three orthogonal sensor axes. After collecting the data, the angular velocity vector of each sensor was transformed to local link axes and integrated to obtain the incremental change in angular position for each time step. Using the angular position time histories, a transformation matrix between the reference frame of each link was calculated. Incremental Eulerian rotations from the transformation matrix were calculated using an axis system defined for the joint. Summation of the incremental Eulerian rotations produced the angular position of the joint in terms of the standard axes. This procedure is illustrated by applying it to joint motion of the ankle, the spine, and the neck of crash dummies during impact tests. The methodology exhibited an accuracy of less than 5% error, improved flexibility over photographic techniques, and the ability to examine 3-dimensional motion.
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An, Seungdo, Yongsoo Oh, Sang-on Choi, and Ci-moo Song. "Two-Input Axis Angular Rate Sensor." Japanese Journal of Applied Physics 37, Part 1, No. 12B (December 30, 1998): 7110–15. http://dx.doi.org/10.1143/jjap.37.7110.

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Hudson, Tracy D. "High-performance microfabricated angular rate sensor." Journal of Micro/Nanolithography, MEMS, and MOEMS 4, no. 4 (October 1, 2005): 043006. http://dx.doi.org/10.1117/1.2114787.

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Bordachev, D. A., I. E. Shustov, and B. A. Kazakov. "Double-count angular rate measurement device." Gyroscopy and Navigation 4, no. 4 (October 2013): 229–32. http://dx.doi.org/10.1134/s2075108713040044.

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Liu, Changwu, Haowen Wang, and Chen Jiang. "High-order derivative fusion estimation of rotorcraft angular rate." Aircraft Engineering and Aerospace Technology 93, no. 2 (March 19, 2021): 347–53. http://dx.doi.org/10.1108/aeat-09-2020-0203.

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Purpose The paper aims at developing a novel algorithm to estimate high-order derivatives of rotorcraft angular rates to break the contradiction between bandwidth and filtering performance because high-order derivatives of angular rates are crucial to rotorcraft control. Traditional causal estimation algorithms such as digital differential filtering or various tracking differentiators cannot balance phase-lead angle loss and high-frequency attenuation performance of the estimated differentials under the circumstance of strong vibration from the rotor system and the rather low update rate of angular rates. Design/methodology/approach The algorithm, capable of estimating angular rate derivatives to maximal second order, fuses multiple attitude signal sources through a first-proposed randomized angular motion maneuvering model independent of platform dynamics with observations generated by cascaded tracking differentiators. Findings The maneuvering flight test on 5-kg-level helicopter and the ferry flight test on 230-kg-level helicopter prove such algorithm is feasible to generate higher signal to noise ratio derivative estimation of angular rates than traditional differentiators in regular flight states with enough bandwidth for flight control. Research limitations/implications The decrease of update rate of input attitude signals will weaken the bandwidth performance of the algorithm and higher sampling rate setting is recommended. Practical implications Rotorcraft flight control researchers and engineers would benefit from the estimation method when implementing flight control laws requiring angular rate derivatives. Originality/value A purely kinematic randomized angular motion model for flight vehicle is first established, combining rigid-body Euler kinematics. Such fusion algorithm with observations generated by cascaded tracking differentiators to estimate angular rate derivatives is first proposed, realized and flight tested.
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Seeger, B., L. Klaus, and D. Nordmann. "Dynamic calibration of digital angular rate sensors." ACTA IMEKO 9, no. 5 (December 31, 2020): 394. http://dx.doi.org/10.21014/acta_imeko.v9i5.1008.

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MEMS gyroscopes/angular rate sensors are often equipped with a digital output only. As part of a European research project, the dynamic calibration of sensors with digital output is being investigated. In the following, the operation principle of digital gyroscopes is described, a possible way to derive correct timestamped data from those sensors using a digital acquisition unit is explained and a calibration procedure is presented. The calibration of the analogue input of the digital acquisition unit, which is a prerequisite to derive correct phase responses, is described. Measurements with digital sensors proved the working principles and gave insight into the dynamic behaviour of those gyroscopes.
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Azor, Ruth, Itzhack Y. Bar-Itzhack, and Richard R. Harman. "Satellite Angular Rate Estimation from Vector Measurements." Journal of Guidance, Control, and Dynamics 21, no. 3 (May 1998): 450–57. http://dx.doi.org/10.2514/2.4257.

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Dissertations / Theses on the topic "Angular rate"

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Watson, Vincent C. "Angular rate estimation by multiplicative Kalman filtering techniques." Thesis, Monterey, Calif. : Naval Postgraduate School, 2003. http://handle.dtic.mil/100.2/ADA420668.

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Thesis (M.S. in Astronautical Engineering)--Naval Postgraduate School, December 2003.
"December 2003". Thesis advisor(s): Cristi, Roberto ; Agrawal, Brij. Includes bibliographical references (p. 53). Also available online.
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John, James Daniel, and james d. john@gmail com. "An Adaptively Controlled MEMS Triaxial Angular Rate Sensor." RMIT University. Electrical and Computer Engineering, 2006. http://adt.lib.rmit.edu.au/adt/public/adt-VIT20070112.162019.

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Prohibitive cost and large size of conventional angular rate sensors have limited their use to large scale aeronautical applications. However, the emergence of MEMS technology in the last two decades has enabled angular rate sensors to be fabricated that are orders of magnitude smaller in size and in cost. The reduction in size and cost has subsequently encouraged new applications to emerge, but the accuracy and resolution of MEMS angular rate sensors will have to be greatly improved before they can be successfully utilised for such high end applications as inertial navigation. MEMS angular rate sensors consist of a vibratory structure with two main resonant modes and high Q factors. By means of an external excitation, the device is driven into a constant amplitude sinusoidal vibration in the first mode, normally at resonance. When the device is subject to an angular rate input, Coriolis acceleration causes a transfer of energy between the two modes and results in a sinusoidal motion in the second mode, whose amplitude is a measure of the input angular rate. Ideally the only coupling between the two modes is the Coriolis acceleration, however fabrication imperfections always result in some cross stiffness and cross damping effects between the two modes. Much of the previous research work has focussed on improving the physical structure through advanced fabrication techniques and structural design; however attention has been directed in recent years to the use of control strategies to compensate for these structural imperfections. The performance of the MEMS angular rate sensors is also hindered by the effects of time varying parameter values as well as noise sources such as thermal-mechanical noise and sensing circuitry noise. In this thesis, MEMS angular rate sensing literature is first reviewed to show the evolu- tion of MEMS angular rate sensing from the basic principles of open-loop operation to the use of complex control strategies designed to compensate for any fabrication imperfections and time-varying effects. Building on existing knowledge, a novel adaptively controlled MEMS triaxial angular rate sensor that uses a single vibrating mass is then presented. Ability to sense all three components of the angular rate vector with a single vibrating mass has advantages such as less energy usage, smaller wafer footprint, avoidance of any mechanical interference between multiple resonating masses and removal of the need for precise alignment of three separate devices. The adaptive controller makes real-time estimates of the triaxial angular rates as well as the device cross stiffness and cross damping terms. These estimates are then used to com- pensate for their effects on the vibrating mass, resulting in the mass being controlled to follow a predefined reference model trajectory. The estimates are updated using the error between the reference model trajectory and the mass's real trajectory. The reference model trajectory is designed to provide excitation to the system that is sufficiently rich to enable all parameter estimates to converge to their true values. Avenues for controller simplification and optimisation are investigated through system simulations. The triaxial controller is analysed for stability, averaged convergence rate and resolution. The convergence rate analysis is further utilised to determine the ideal adaptation gains for the system that minimises the unwanted oscillatory behaviour of the parameter estimates. A physical structure for the triaxial device along with the sensing and actuation means is synthesised. The device is realisable using MEMS fabrication techniques due to its planar nature and the use of conventional MEMS sensing and actuation elements. Independent actuation and sensing is achieved using a novel checkerboard electrode arrangement. The physical structure is refined using a design automation process which utilises finite element analysis (FEA) and design optimisation tools that adjust the design variables until suitable design requirements are met. Finally, processing steps are outlined for the fabrication of the device using a modified, commercially available polysilicon MEMS process.
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Osborn, Christopher Scott 1979. "Gyroscope angular rate processing across asynchronous clock domains." Thesis, Massachusetts Institute of Technology, 2002. http://hdl.handle.net/1721.1/87278.

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Thesis (M.Eng.)--Massachusetts Institute of Technology, Dept. of Electrical Engineering and Computer Science, 2002.
Includes bibliographical references (p. 85-86).
by Christopher Scott Osborn.
M.Eng.
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Patil, Nishad. "Design And Analysis Of MEMS Angular Rate Sensors." Thesis, Indian Institute of Science, 2006. http://etd.iisc.ac.in/handle/2005/439.

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Design and analysis of polysilicon and single crystal silicon gyroscopes have been carried out. Variations in suspension design have been explored. Designs that utilize in-plane and out-of-plane sensing are studied. Damping plays an important role in determining the sense response. Reduction in damping directly affects sensor performance. The various damping mechanisms that are prevalent in gyroscopes are studied. Perforations on the proof mass are observed to significantly reduce the damping in the device when operated in air. The effects of perforation geometry and density have been analyzed. The analysis results show that there is a two orders of magnitude reduction in damping of thick gyroscope structures with optimized perforation design. Equivalent circuit lumped parameter models have been developed to analyze gyroscope performance. The simulation results of these models have been compared with results obtained from SABER, a MEMS specific system level design tool from Coventorware. The lumped parameter models are observed to produce faster simulation results with an accuracy comparable to that of Coventorware Three gyroscopes specific to the PolyMUMPS fabrication process have been designed and their performance analyzed. Two of the designs sense motion out-of-plane and the other senses motion in-plane. Results of the simulation show that for a given damping, the gyro design with in-plane modes gives a resolution of 4º/s. The out-of-plane gyroscopes have two variations in suspension. The hammock suspension resolves a rate of 25º/s in a 200 Hz bandwidth while the design with folded beam suspension resolves a rate of 2º/s in a 12 Hz bandwidth. A single crystal silicon in-plane gyroscope has been designed with vertical electrodes to sense Coriolis motion. This design gives an order of magnitude higher Capacitance change for a given rotation in comparison to conventional comb-finger design. The effects of process induced residual stress on the characteristic frequencies of the polysilicon gyroscopes are also studied. The in-plane gyroscope is found to be robust to stress variations. Analysis results indicate that the tuning fork gyroscope with the hammock suspension is the most susceptible to compressive residual stress, with a significant drop in sensitivity at high stress values.
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Patil, Nishad. "Design And Analysis Of MEMS Angular Rate Sensors." Thesis, Indian Institute of Science, 2006. http://hdl.handle.net/2005/291.

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Design and analysis of polysilicon and single crystal silicon gyroscopes have been carried out. Variations in suspension design have been explored. Designs that utilize in-plane and out-of-plane sensing are studied. Damping plays an important role in determining the sense response. Reduction in damping directly affects sensor performance. The various damping mechanisms that are prevalent in gyroscopes are studied. Perforations on the proof mass are observed to significantly reduce the damping in the device when operated in air. The effects of perforation geometry and density have been analyzed. The analysis results show that there is a two orders of magnitude reduction in damping of thick gyroscope structures with optimized perforation design. Equivalent circuit lumped parameter models have been developed to analyze gyroscope performance. The simulation results of these models have been compared with results obtained from SABER, a MEMS specific system level design tool from Coventor-ware. The lumped parameter models are observed to produce faster simulation results with an accuracy comparable to that of Coventorware Three gyroscopes specific to the PolyMUMPS fabrication process have been designed and their performance analyzed. Two of the designs sense motion out-of-plane and the other senses motion in-plane. Results of the simulation show that for a given damping, the gyro design with in-plane modes gives a resolution of 4◦/s. The out-of-plane gyroscopes have two variations in suspension. The hammock suspension resolves a rate of 25◦/s in a 200 Hz bandwidth while the design with folded beam suspension resolves a rate of 2◦/s in a 12 Hz bandwidth. A single crystal silicon in-plane gyroscope has been designed with vertical electrodes to sense Coriolis motion. This design gives an order of magnitude higher capacitance change for a given rotation in comparison to conventional comb-finger design. The effects of process induced residual stress on the characteristic frequencies of the polysilicon gyroscopes are also studied. The in-plane gyroscope is found to be robust to stress variations. Analysis results indicate that the tuning fork gyroscope with the hammock suspension is the most susceptible to compressive residual stress, with a significant drop in sensitivity at high stress values.
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Patil, Nishad. "Design And Analysis Of MEMS Angular Rate Sensors." Thesis, Indian Institute of Science, 2006. https://etd.iisc.ac.in/handle/2005/291.

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Design and analysis of polysilicon and single crystal silicon gyroscopes have been carried out. Variations in suspension design have been explored. Designs that utilize in-plane and out-of-plane sensing are studied. Damping plays an important role in determining the sense response. Reduction in damping directly affects sensor performance. The various damping mechanisms that are prevalent in gyroscopes are studied. Perforations on the proof mass are observed to significantly reduce the damping in the device when operated in air. The effects of perforation geometry and density have been analyzed. The analysis results show that there is a two orders of magnitude reduction in damping of thick gyroscope structures with optimized perforation design. Equivalent circuit lumped parameter models have been developed to analyze gyroscope performance. The simulation results of these models have been compared with results obtained from SABER, a MEMS specific system level design tool from Coventor-ware. The lumped parameter models are observed to produce faster simulation results with an accuracy comparable to that of Coventorware Three gyroscopes specific to the PolyMUMPS fabrication process have been designed and their performance analyzed. Two of the designs sense motion out-of-plane and the other senses motion in-plane. Results of the simulation show that for a given damping, the gyro design with in-plane modes gives a resolution of 4◦/s. The out-of-plane gyroscopes have two variations in suspension. The hammock suspension resolves a rate of 25◦/s in a 200 Hz bandwidth while the design with folded beam suspension resolves a rate of 2◦/s in a 12 Hz bandwidth. A single crystal silicon in-plane gyroscope has been designed with vertical electrodes to sense Coriolis motion. This design gives an order of magnitude higher capacitance change for a given rotation in comparison to conventional comb-finger design. The effects of process induced residual stress on the characteristic frequencies of the polysilicon gyroscopes are also studied. The in-plane gyroscope is found to be robust to stress variations. Analysis results indicate that the tuning fork gyroscope with the hammock suspension is the most susceptible to compressive residual stress, with a significant drop in sensitivity at high stress values.
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Palermo, William J. "Angular rate estimation for multi-body spacecraft attitude control." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2001. http://handle.dtic.mil/100.2/ADA392077.

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Thesis (M.S. in Astronautical Engineering and Aeronautical and Astronautical Engineer) Naval Postgraduate School, June 2001.
Thesis advisor(s): Agrawal, Brij N. "June 2001." Includes bibliographical references (p. 109-110). Also available in print.
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Wilson, Michael J. "Nonlinear projectile attitude estimation with magnetometers and angular rate sensors." Access to citation, abstract and download form provided by ProQuest Information and Learning Company; downloadable PDF file, 37 p, 2006. http://proquest.umi.com/pqdweb?did=1163250861&sid=2&Fmt=2&clientId=8331&RQT=309&VName=PQD.

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Nikpour, Behrouz. "A micromachined silicon vibrating-beam angular rate sensor : a design and implementation study." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 1998. http://www.collectionscanada.ca/obj/s4/f2/dsk1/tape11/PQDD_0005/NQ40318.pdf.

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Ghoussayni, Salim. "Application of angular rate gyroscopes as sensors in electrical orthoses for foot drop correction." Thesis, University of Surrey, 2004. http://epubs.surrey.ac.uk/673/.

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Books on the topic "Angular rate"

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Polites, Michael E. A nonlinear estimator for reconstructing the angular velocity of a spacecraft without rate gyros. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

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D, Lightsey W., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. A nonlinear estimator for reconstructing the angular velocity of a spacecraft without rate gyros. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

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Sweeney, John Peter. Gamma-ray spectroscopy of the light rare earth nuclei 159Er, 160Er and 167Lu at high angula momenta. Manchester: University of Manchester, 1994.

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Angular Rate Estimation by Multiplicative Kalman Filtering Techniques. Storming Media, 2003.

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Angular Rate Estimation for Multi-Body Spacecraft Attitude Control. Storming Media, 2001.

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Real-Time Data Acquisition and Processing of the Magnetic, Angular Rate and Gravity (MARG) Sensor. Storming Media, 2004.

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Theologis, Tim. Common disorders of the lower limb. Oxford University Press, 2011. http://dx.doi.org/10.1093/med/9780199550647.003.013010.

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♦ Most torsional or angular deviations are physiological and resolve with time♦ Ensure the child has normal growth parameters♦ Take care to exclude the rare underlying condition that will require treatment♦ Coronal knee deformities may be due to a systemic or local bone dysplasia.
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Wainwright, Andrew. Developmental deformities of the lower limbs. Oxford University Press, 2011. http://dx.doi.org/10.1093/med/9780199550647.003.013016.

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♦ Some rare angular deformities of the lower limbs must be recognized early♦ Most deteriorate with time and cause significant functional problems♦ With tibial bowing, description of the apex of the bow determines prognosis and management♦ Surgical management of these conditions can be difficult: multiple procedures may be required during the growth period.
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Escudier, Marcel. Basic equations of viscous-fluid flow. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198719878.003.0015.

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In this chapter it is shown that application of the momentum-conservation equation (Newton’s second law of motion) to an infinitesimal cube of fluid leads to Cauchy’s partial differential equations, which govern the flow of any fluid satisfying the continuum hypothesis. Any fluid flow must also satisfy the continuity equation, another partial differential equation, which is derived from the mass-conservation equation. It is shown that distortion of a flowing fluid can be split into elongational distortion and angular distortion or shear strain. For a Newtonian fluid, the normal and shear stresses in Cauchy’s equations are related to the elongational and shear-strain rates through Stokes’ constitutive equations. Substitution of these constitutive equations into Cauchy’s equations leads to the Navier-Stokes equations, which govern steady or unsteady flow of a fluid. A minor modification of the constitutive equations for a Newtonian fluid allows consideration of generalised Newtonian fluids, for which the viscosity depends upon the shear-strain rates. The boundary conditions for the tangential and normal velocity components are discussed briefly.
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Zeitlin, Vladimir. Rotating Shallow-Water Models with Full Coriolis Force. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198804338.003.0016.

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The derivation of the rotating shallow-water model by vertical averaging is carried on in the tangent plane approximation without neglecting the vertical component of the Coriolis force, and contributions of the vertical component of velocity in its horizontal component (‘non-traditional’ terms), leading to one- and two-layer ‘non-traditional’ rotating shallow-water models. A similar approach on the whole sphere encounters difficulties with conservation of angular momentum. Consistent ‘non-traditional’ rotating shallow-water equations in this case are obtained from the variational principle, which is first formulated for full primitive equations. It is shown that columnar motion hypothesis should be replaced by solid-angle motion one on the sphere. Two-layer non-traditional rotating shallow-water equations are used to analyse inertial instability of jets and compare the results with Chapter 10. It is shown that non-traditional terms can increase the growth rates up to 30% in some configurations and can also change the structure of the unstable modes.
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Book chapters on the topic "Angular rate"

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Meroth, Ansgar, and Petre Sora. "Angular Rate Sensors." In Sensor networks in theory and practice, 427–42. Wiesbaden: Springer Fachmedien Wiesbaden, 2023. http://dx.doi.org/10.1007/978-3-658-39576-6_17.

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Merhav, Shmuel. "Coriolis Angular Rate Sensors." In Aerospace Sensor Systems and Applications, 325–48. New York, NY: Springer New York, 1996. http://dx.doi.org/10.1007/978-1-4612-3996-3_7.

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Elwenspoek, Miko, and Remco Wiegerink. "Acceleration and Angular Rate Sensors." In Microtechnology and MEMS, 132–52. Berlin, Heidelberg: Springer Berlin Heidelberg, 2001. http://dx.doi.org/10.1007/978-3-662-04321-9_7.

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Hill, Frank. "The Equatorial Rotation Rate in the Solar Convection Zone." In The Internal Solar Angular Velocity, 45–50. Dordrecht: Springer Netherlands, 1987. http://dx.doi.org/10.1007/978-94-009-3903-5_6.

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Guenther, D. B. "Inertial Oscillations and the Rotation Rate Profile of the Sun." In The Internal Solar Angular Velocity, 107–14. Dordrecht: Springer Netherlands, 1987. http://dx.doi.org/10.1007/978-94-009-3903-5_15.

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Wang, Xing, Linhua Piao, and Quangang Yu. "CJSYS-A01 Piezoelectric Fluidic Angular Rate Sensor." In Advances in Intelligent and Soft Computing, 575–79. Berlin, Heidelberg: Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-25349-2_77.

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Nakano, Takenori. "The Rate of Angular Momentum Loss from Cloud Cores." In Galactic and Intergalactic Magnetic Fields, 281–86. Dordrecht: Springer Netherlands, 1990. http://dx.doi.org/10.1007/978-94-009-0569-6_86.

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Wang, Xing, Linhua Piao, and Quangang Yu. "Software Compensation of the Piezoelectric Fluidic Angular Rate Sensor." In Communications in Computer and Information Science, 253–60. Berlin, Heidelberg: Springer Berlin Heidelberg, 2011. http://dx.doi.org/10.1007/978-3-642-24097-3_39.

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Vardya, M. S. "How Effective is Rotation in Enhancing the Rate of Mass Loss in Early Type Stars?" In Angular Momentum and Mass Loss for Hot Stars, 231–34. Dordrecht: Springer Netherlands, 1990. http://dx.doi.org/10.1007/978-94-009-2105-4_28.

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Zhao, Yue, Ju Liu, Guoxia Sun, Jing Ge, and Wenbo Wan. "Frame Rate Up-Conversion Using Motion Vector Angular for Occlusion Detection." In Lecture Notes in Computer Science, 301–11. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-21963-9_28.

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Conference papers on the topic "Angular rate"

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Ng, Matthew, Xinyu Cai, and Shaohui Foong. "Direct Angular Rate Estimation Without Event Motion-Compensation At High Angular Rates." In 2023 IEEE International Conference on Robotics and Automation (ICRA). IEEE, 2023. http://dx.doi.org/10.1109/icra48891.2023.10160967.

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Johnson, Jack D., Seyed R. Zarabadi, and Douglas R. Sparks. "Surface Micromachined Angular Rate Sensor." In International Congress & Exposition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 1995. http://dx.doi.org/10.4271/950538.

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"Two-Input.axis Angular Rate Sensor." In Microprocesses and Nanotechnology '98. 1998 International Microprocesses and Nanotechnology Conference. IEEE, 1998. http://dx.doi.org/10.1109/imnc.1998.730038.

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Zhang, Fuxue, Ling Wang, and Jiangchuan Wen. "Silicon Micromachined Angular Rate Sensor." In 2007 International Conference on Information Acquisition. IEEE, 2007. http://dx.doi.org/10.1109/icia.2007.4295689.

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Kong, Henry, and Andrew Betts. "Cancellation of Unknown Angular Rate Effects in Linear G Sensitivity Testing for Angular Rate Sensors." In SAE 2000 World Congress. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2000. http://dx.doi.org/10.4271/2000-01-0056.

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Zotov, Sergei A., Igor P. Prikhodko, Alexander A. Trusov, and Andrei M. Shkel. "Frequency modulation based angular rate sensor." In 2011 IEEE 24th International Conference on Micro Electro Mechanical Systems (MEMS). IEEE, 2011. http://dx.doi.org/10.1109/memsys.2011.5734490.

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Sharma, Ajit, Mohammad Faisal Zaman, and Farrokh Ayazi. "A Smart Angular Rate Sensor System." In 2007 IEEE Sensors. IEEE, 2007. http://dx.doi.org/10.1109/icsens.2007.4388602.

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Ichinose, Toshihiko, and Jiro Terada. "Angular Rate Sensor for Automotive Application." In International Congress & Exposition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 1995. http://dx.doi.org/10.4271/950535.

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An, Seungdo, K. Y. Park, Yong-Soo Oh, and Ci M. Song. "Two-input axis angular rate sensor." In 1999 Symposium on Smart Structures and Materials, edited by Vijay K. Varadan. SPIE, 1999. http://dx.doi.org/10.1117/12.354272.

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Geiger, Wolfram, Martin Kieninger, Michael Pascal, Bernd Folkmer, and Walter Lang. "Micromachined angular rate sensor MARS-RR." In Micromachining and Microfabrication, edited by Patrick J. French and Kevin H. Chau. SPIE, 1998. http://dx.doi.org/10.1117/12.323886.

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Reports on the topic "Angular rate"

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Barrie, Alexander C., Bryan S. Taylor, Jared M. Ekholm, Jr Hargus, and William A. Calculating Sputter Rate Angular Dependence Using Optical Profilometry (Preprint). Fort Belvoir, VA: Defense Technical Information Center, July 2007. http://dx.doi.org/10.21236/ada473515.

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Brosseau, Timothy L., and T. G. Brown. Experimental Firing Fixture for Evaluation and Calibration of Angular Rate Sensors During Actual Gun Firings. Fort Belvoir, VA: Defense Technical Information Center, September 2002. http://dx.doi.org/10.21236/ada406775.

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Aubert, B. Measurements of Branching Fractions, Rate Asymmetries, and Angular Distributions in the Rare Decays B -> Kl+l- and B -> K*l+ l-. Office of Scientific and Technical Information (OSTI), April 2006. http://dx.doi.org/10.2172/878714.

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Riley, Mark, and Akis Pipidis. The Mechanical Analogue of the "Backbending" Phenomenon in Nuclear-structure Physics. Florida State University, May 2008. http://dx.doi.org/10.33009/fsu_physics-backbending.

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Abstract:
This short pedagogical movie illustrates an effect in nuclear physics called backbending which was first observed in the study of the rotational behavior of rapidly rotating rare-earth nuclei in Stockholm, Sweden in 1971. The video contains a mechanical analog utilizing rare-earth magnets and rotating gyroscopes on a turntable along with some historic spectra and papers associated with this landmark discovery together with its explanation in terms of the Coriolis induced uncoupling and rotational alignment of a specific pair of particles occupying high-j intruder orbitals. Thus backbending represents a crossing in energy of the groundstate, or vacuum, rotational band by another band which has two unpaired high-j nucleons (two quasi-particles) with their individual angular momenta aligned with the rotation axis of the rapidly rotating nucleus. Backbending was a major surprise which pushed the field of nuclear structure physics forward but which is now sufficiently well understood that it can be used as a precision spectroscopic tool providing useful insight for example, into nuclear pairing correlations and changes in the latter due to blocking effects and quasi-particle seniority, nuclear deformation, the excited configurations of particular rotational structures and the placement of proton and neutron intruder orbitals at the Fermi surface.
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Hollar, Jonathan. Measurements of Rates, Asymmetries, and Angular Distributions in B -> K l+ l- and B -> K* l+ l- Decays. Office of Scientific and Technical Information (OSTI), September 2006. http://dx.doi.org/10.2172/891838.

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