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      The Synthesis Model of Flat-Electrode Hemispherical Resonator Gyro

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          Abstract

          The Hemispherical Resonator Gyro (HRG) is a solid-state and widely used vibrating gyroscope, especially in the field of deep space exploration. The flat-electrode HRG is a new promising type of gyroscope with simpler structure that is easier to be fabricated. In this paper, to cover the shortage of a classical generalized Coriolis Vibration Gyroscope model whose parameters are hard to obtain, the model of flat-electrode HRG is established by the equivalent mechanical model, the motion equations of unideal hemispherical shell resonator are deduced, and the calculation results of parameters in the equations are verified to be reliable and believable by comparing with finite element simulation and the reported experimental data. In order to more truthfully reveal the input and output characteristics of HRG, the excitation and detection models with assemble errors and parameters are established based on the model of flat-electrode capacitor, and they convert both the input and output forms of the HRG model to voltage changes across the electrodes rather than changes in force and capacitance. An identification method of assemble errors and parameters is proposed to evaluate and improve the HRG manufacturing technology and adjust the performance of HRG. The average gap could be identified with the average capacitance of all excitation and detection capacitors; fitting the approximate static capacitor model could identify the inclination angle and direction angle. With the obtained model, a firm and tight connection between the real HRG system and theoretical model is established, which makes it possible to build a fully functional simulation model to study the control and detection methods of standing wave on hemispherical shell resonator.

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          Convergence Properties of the Nelder--Mead Simplex Method in Low Dimensions

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            Vibratory gyro analysis by the method of averaging

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              Force to Rebalance Control of HRG and Suppression of Its Errors on the Basis of FPGA

              A novel design of force to rebalance control for a hemispherical resonator gyro (HRG) based on FPGA is demonstrated in this paper. The proposed design takes advantage of the automatic gain control loop and phase lock loop configuration in the drive mode while making full use of the quadrature control loop and rebalance control loop in controlling the oscillating dynamics in the sense mode. First, the math model of HRG with inhomogeneous damping and frequency split is theoretically analyzed. In addition, the major drift mechanisms in the HRG are described and the methods that can suppress the gyro drift are mentioned. Based on the math model and drift mechanisms suppression method, four control loops are employed to realize the manipulation of the HRG by using a FPGA circuit. The reference-phase loop and amplitude control loop are used to maintain the vibration of primary mode at its natural frequency with constant amplitude. The frequency split is readily eliminated by the quadrature loop with a DC voltage feedback from the quadrature component of the node. The secondary mode response to the angle rate input is nullified by the rebalance control loop. In order to validate the effect of the digital control of HRG, experiments are carried out with a turntable. The experimental results show that the design is suitable for the control of HRG which has good linearity scale factor and bias stability.
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                Author and article information

                Journal
                Sensors (Basel)
                Sensors (Basel)
                sensors
                Sensors (Basel, Switzerland)
                MDPI
                1424-8220
                09 April 2019
                April 2019
                : 19
                : 7
                : 1690
                Affiliations
                Space Control and Inertial Technology Research Center, Harbin Institute of Technology, Harbin 150080, Heilongjiang, China; wzn@ 123456hit.edu.cn (Z.W.); hy_hit@ 123456163.com (Y.H.); qi.ziyang@ 123456protonmail.com (Z.Q.); xuzeyuan@ 123456hit.edu.cn (Z.X.)
                Author notes
                [* ]Correspondence: ygx@ 123456hit.edu.cn ; Tel.: +86-0451-8640-2350
                Author information
                https://orcid.org/0000-0002-0721-9377
                https://orcid.org/0000-0002-1669-6247
                Article
                sensors-19-01690
                10.3390/s19071690
                6479381
                30970645
                8c14aa49-7f5b-4f50-b8e1-342f421ae39a
                © 2019 by the authors.

                Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license ( http://creativecommons.org/licenses/by/4.0/).

                History
                : 13 February 2019
                : 06 April 2019
                Categories
                Article

                Biomedical engineering
                hemispherical resonator gyro,flat electrode,motion equation,excitation and detection model,assemble error and parameter,identification method

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