Evaluation of the Experiment Factors Influence in Studying Dynamic Error of the TwoComponent Angular Rate Sensor

Authors: Podchezertsev V.P., Nguyen D.D. Published: 28.12.2022
Published in issue: #4(141)/2022  
DOI: 10.18698/0236-3933-2022-4-92-107

Category: Instrument Engineering, Metrology, Information-Measuring Instruments and Systems | Chapter: Navigation Instruments  
Keywords: angular rate sensor, orientation and navigation system, dynamically tuned gyroscope, dynamic error, angular oscillations bench


Angular rate sensors are widely used in various technology areas, especially in aviation and rocket technologies. Angular rate sensors are installed in aircraft stabilization, orientation and navigation systems to determine the object angular position and control. In addition, they could be introduced in the automatic control systems of a moving object to enter a signal proportional to the angular rate in the control function or to damp the object oscillations occurring under the action of angular or linear overloads. Various design schemes of angular rate sensors are currently known to perform their functionality with required accuracy in the given frequency range. For them, the influence of design parameters and feedback loop on the accuracy of a device under conditions of dynamic operational influences was studied sufficiently. Biaxial angular rate sensor built on the basis of a dynamically tuned gyroscope was considered, and the influence of various design and technological factors on the experimental estimated accuracy of its dynamic error was studied. Main probable factors leading to inaccuracies in determining this error in testing on the angular oscillations bench were considered

Please cite this article in English as:

Podchezertsev V.P., Nguyen D.D. Evaluation of the experiment factors influence in studying dynamic error of the two-component angular rate sensor. Herald of the Bauman Moscow State Technical University, Series Instrument Engineering, 2022, no. 4 (141), pp. 92--107 (in Russ.). DOI: https://doi.org/10.18698/0236-3933-2022-4-92-107


[1] Pelpor D.S., ed. Giroskopicheskie sistemy [Gyroscopic systems]. Moscow, Vysshaya shkola Publ., 1988.

[2] Pelpor D.S., Osokin Yu.A., Rakhteenko E.R. Giroskopicheskie pribory sistem orientatsii i stabilizatsii [Gyroscopic devices of orientation and stabilization systems]. Moscow, Mashinostroenie Publ., 1977.

[3] Volchikhin I.A., Volchikhin A.I., Malyutin D.M., et al. Wave solid-state gyroscopes (analytical review). Izvestiya TulGU. Tekhnicheskie nauki [News of the Tula State University. Technical Sciences], 2017, no. 9-2, pp. 59--78 (in Russ.).

[4] Korolev M.N., Malyutin D.M. Analysis of the technical characteristics of sensitive elements of indicator gyroscopic stabilizers. Izvestiya TulGU. Tekhnicheskie nauki [News of the Tula State University. Technical Sciences], 2019, no. 8, pp. 30--46 (in Russ.).

[5] Sheremetyev A.G. Volokonno-opticheskiy giroskop [Fiber-optic gyroscope]. Moscow, Radio i svyaz Publ., 1987.

[6] Filatov Yu.V. Volokonno-opticheskiy giroskop. St. Petersburg, SPbSETU "LETI" Publ., 2003.

[7] Lukyanov D., Filatov Yu., Golyaev Yu., et al. [Laser gyroscope is 50 years old. Part 2]. Fotonika [Photonics Russia], 2014, no. 2, pp. 20--37 (in Russ.).

[8] Bychkov S.I., Lukyanov D.P., Bakalyar A.I. Lazernyy giroskop [Laser gyroscope]. Moscow, Sovetskoe radio Publ., 1975.

[9] Pelpor D.S., Matveev V.A., Arsenyev V.D. Dinamicheski nastraivaemye giroskopy [Dynamic tuned gyroscopes]. Moscow, Mashinostroenie Publ., 1988.

[10] Matveev V.A., Podchezertsev V.P., Fateev V.V. Giroskopicheskie stabilizatory na dinamicheski nastraivaemykh vibratsionnykh giroskopakh [Gyroscopic stabilizers on dynamically tuned vibration gyroscopes]. Moscow, Bauman MSTU Publ., 2005.

[11] Brozgul L.I. Dinamicheski nastraivaemye giroskopy [Dynamically tuned gyroscopes]. Moscow, Mashinostroenie Publ., 1989.

[12] Odintsov A.A. Dinamicheski nastraivaemye giroskopy [Dynamically tuned gyroscopes]. Kiev, UMK VO Publ., 1992.

[13] Podchezertsev V.P., Nguen D.D. Increasing the dynamic accuracy of a gyroscope with internal elastic gimbal in the angular rate sensor mode. Herald of the Bauman Moscow State Technical University, Series Instrument Engineering, 2021, no. 4 (137), pp. 188--207 (in Russ.). DOI: http://dx.doi.org/10.18698/0236-3933-2021-4-188--207

[14] Podchezertsev V.P., Nguen D.D. Issues of synthesis and practical evaluation of the compensation mode error of a two-component gyroscope. Izvestiya vysshikh uchebnykh zavedeniy. Mashinostroenie [BMSTU Journal of Mechanical Engineering], 2021, no. 9, pp. 108--116 (in Russ.). DOI: http://dx.doi.org/10.18698/0536-1044-2021-9-108-116

[15] Odintsov A.A. Teoriya i raschet giroskopicheskikh priborov [Theory and calculation of gyroscopic devices]. Kiev, Vysshaya shkola Publ., 1985.

[16] Rivkin S.S. Raschet dinamicheskikh pogreshnostey giroskopicheskikh ustroystv na kachayushchemsya osnovanii [Calculation of dynamic errors in gyroscopic devices on a swinging base]. Leningrad, TsNII Rumb Publ., 1991.

[17] Konovalov S.F., Nikitin E.A., Selivanova L.M. Giroskopicheskie sistemy. Proektirovanie giroskopicheskikh system [Gyroscopic systems. Design of gyroscopic systems]. Moscow, Vysshaya shkola Publ., 1980.

[18] Podchezertsev V.P., Tan S., Tsin Ts. Components of model of drift dynamically tuned gyro. Aviakosmicheskoe priborostroenie [Aerospace Instrument-Making], 2015, no. 1, pp. 8--18 (in Russ.).