Analysis of Errors of Piezoelectric Sensors used in Weapon Stabilizers

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Effectiveness of operation of a weapon stabilization system is largely dependent on the choice of a sensor, i.e. an accelerometer. The paper identifies and examines fundamental errors of piezoelectric accelerometers and offers measures for their reduction. Errors of a weapon stabilizer piezoelectric sensor have been calculated. The instrumental measurement error does not exceed 0.1 × 10−5 m/s2. The errors caused by the method of attachment to the base, different noise sources and zero point drift can be mitigated by the design features of piezoelectric sensors used in weapon stabilizers.


  • [1] Lai, A., James, D.A., Hayes, J.P., Harvey, E.C. (2004). Semi-automatic calibration technique using six inertial frames of reference. Proc. of SPIE × The International Society for Optical Engineering, 5274, 531−542.

  • [2] Lakehal, A., Ghemari, Z. (2016). Suggestion for a new design of the piezoresistive accelerometer. Ferroelectrics, 493(1), 93−102.

  • [3] Korobiichuk, I., Bezvesilna, O., Tkachuk, A., Nowicki, M., Szewczyk, R., Shadura, V. (2015). Aviation gravimetric system. International Journal of Scientific & Engineering Research, 6(7), 1122−1127.

  • [4] Liu, Y., Ji, T., et al. (2016). Calibration and compensation for accelerometer based on Kalman filter and a six-position method. Yadian Yu Shengguang/Piezoelectrics and Acoustooptics, 38(1), 94−98, 110.

  • [5] Gao, J.M., Zhang, K.B., et al. (2015). Temperature characteristics and error compensation for quartz flexible accelerometer. International Journal of Automation and Computing, 12(5), 540−550.

  • [6] Korobiichuk, I. (2016). Mathematical model of precision sensor for an automatic weapons stabilizer system. Measurement,

  • [7] Korobiichuk, I., Bezvesilna, O., et al. (2016). Design of piezoelectric gravimeter for automated aviation gravimetric system. Journal of Automation, Mobile Robotics & Intelligent Systems (JAMRIS), 10(1).

  • [8] Korobiichuk, I., Bezvesilna, O., et al. (2016). Piezoelectric gravimeter of the aviation gravimetric system. Advances in Intelligent Systems and Computing 440. Szewczyk, R., Zieliński, C., Kaliczyńska, M. (eds.), Challenges in Automation, Robotics and Measurement Techniques. Proc. of AUTOMATION-2016, Warsaw, Poland, 753−763.

  • [9] Korobiichuk, I., Bezvesilna, O., et al. (2015). Stabilization system of aviation gravimeter. International Journal of Scientific & Engineering Research, 6(8), 956−959.

  • [10] Fan, C., Hu, X., et al. (2014). Observability analysis of a MEMS INS/GPS integration system with gyroscope G-sensitivity errors. Sensors, 14(9), 16003−16016.

  • [11] Quinchia, A.G., Falco, G., Falletti, E., Dovis, F., Ferrer, C. (2013). A comparison between different error modeling of MEMS applied to GPS/INS integrated systems. Sensors, 13(8), 9549−9588.

  • [12] Karachun, V., Mel’nick, V., Korobiichuk, I., Nowicki, M., Szewczyk, R., Kobzar, S. (2016). The Additional Error of Inertial Sensor Induced by Hypersonic Flight Condition. Sensors, 16(3).

  • [13] Lobanov, V.S., Tarasenko, N.V., et al. (2007). Fiber-optic gyros & quartz accelerometers for motion control. IEEE Aerospace and Electronic Systems Magazine. 22(4), 23−29.

  • [14] Guo, Y., Kakimoto, K.I., Ohsato, H. (2005). (Na0.5K0.5)NbO3-LiTaO3 lead-free piezoelectric ceramics. Materials Letters, 59(2−3), 241−244.

  • [15] Tables of fundamental properties of piezoceramic materials manufactured by Ferropiezoelectric Material Division, devices and tools of Research Institute of Physics SFU [electronic resource]. – Access mode,

  • [16] Arlou, Y.Y., Tsyanenka, D.A., Sinkevich, E.V. (2015). Wideband computationally-effective worst-case model of twisted pair radiation. Proc. of the International Conference Days on Diffraction, 14−19.

  • [17] Meggiolaro, M.A., Castro, J.T.P.D., Góes, R.C.D.O. (2016). Elastoplastic nominal stress effects in the estimation of the notch-tip behavior in tension. Theoretical and Applied Fracture Mechanics.

  • [18] Korobiichuk, I., Koval, A., Nowicki, M., Szewczyk, R. Investigation of the Effect of Gravity Anomalies on the Precession Motion of Single Gyroscope Gravimeter. Solid State Phenomena, 251, 139−145.

Metrology and Measurement Systems

The Journal of Committee on Metrology and Scientific Instrumentation of Polish Academy of Sciences

Journal Information

IMPACT FACTOR 2016: 1.598

CiteScore 2016: 1.58

SCImago Journal Rank (SJR) 2016: 0.460
Source Normalized Impact per Paper (SNIP) 2016: 1.228


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