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The effect of detuning of the partial frequency of MEMS gyros sensing elements on the amplitude-frequency response

  • Aircraft Instruments and Instrumentation Computer Complexes
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Abstract

The effect of detuning the partial frequencies of MEMS gyroscopes on its amplitudefrequency response is investigated. The formulated mathematical model allows defining requirements for the tolerances on gyros parameters, which determine the values of gyros partial frequencies, at the design stage of the sensor.

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References

  1. Afanas’ev, V.A., Degryarev, G.L., and Meshchanov, A.S., Rocket Berthing to an Asteroid: Design Problems, Izv.Vuz. Av. Tekhnika, 2013, vol. 56, no. 2, pp. 72–77 [Russian Aeronautics (Engl. Transl.), vol. 56, no. 2, pp. 199–207].

    Google Scholar 

  2. Kasumov, E.V., Modeling of Helicopter Behavior Dynamics under the Controlling Action of the Stabilization and Control System, Izv.Vuz. Av. Tekhnika, 2013, vol. 56, no. 3, pp. 11–14 [Russian Aeronautics (Engl. Transl.), vol. 56, no. 3, pp. 224–228].

    Google Scholar 

  3. Peshekhonov, V.G., Gyroscopic Navigation Systems: Current Status and Prospects, Gyroscopy and Navigation, 2011, no. 3, pp. 111–118.

    Article  Google Scholar 

  4. Raspopov, V.Ya., Mikromekhanicheskie pribory (Micromechanical Devices), Tula: TulGU, 2002.

    Google Scholar 

  5. Dzhashitov, V.E. and Pankratov, V.M., Datchiki, pribory i sistemy aviakosmicheskogo i morskogo priborostroeniya v usloviyakh teplovykh vozdeistvii (Airspace and Marine Sensors, Devices, and Systems under Thermal Actions), Peshekhonov, V.G., Ed., St. Petersburg: Elektropribor, 2005.

    Google Scholar 

  6. Dzhashitov V.E. and Pankratov V.M., The Superminiature Micromechanical Sensor of the Inertial Information in Conditions of Variables and Constant Mechanical Effects, Nano- i Mikrosistemnaya Tekhnika. 2011, no. 6. pp. 39–43.

    Google Scholar 

  7. Dzhashitov, V.E., Pankratov, V.M., and Golikov, A.V., Obshchaya i prikladnaya teoriya giroskopov s primeneniem komp’yuternykh tekhnologii (General and Applied Theory of Gyros with Applications of Computer Technology), Peshekhonov, V.G., Ed., St. Petersburg: Elektropribor, 2010.

    Google Scholar 

  8. Mandel’shtam, L.I., Polnoe sobranie trudov (Complete Collection of Works), vol. 4, Lectures on Oscillations, Moscow: Izd. AN SSSR, 1955.

    Google Scholar 

  9. Babakov, N.A., Teorija avtomaticheskogo upravlnija (Theory of Automatic Control, part 1, Theory of Linear System of Automatic Control), Moscow: Vyshaya Shkola, 1986.

    Google Scholar 

  10. SageMath, URL: http://www.sagemath.org.

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Authors and Affiliations

  1. Institute of Precision Mechanics and Control, ul. Rabochaya 24, Saratov, 410028, Russia

    V. M. Pankratov & M. A. Barulina

  2. Saratov State Technical University, Polytechnicheskaya ul. 77, Saratov, 410054, Russia

    A. V. Krys’ko

Authors
  1. V. M. Pankratov
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  2. M. A. Barulina
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  3. A. V. Krys’ko
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Corresponding author

Correspondence to V. M. Pankratov.

Additional information

Original Russian Text © V.M. Pankratov, M.A. Barulina, A.V. Krys’ko, 2017, published in Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2017, No. 2, pp. 99–105.

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Pankratov, V.M., Barulina, M.A. & Krys’ko, A.V. The effect of detuning of the partial frequency of MEMS gyros sensing elements on the amplitude-frequency response. Russ. Aeronaut. 60, 270–277 (2017). https://doi.org/10.3103/S1068799817020179

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  • DOI: https://doi.org/10.3103/S1068799817020179

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