BASIC PROBLEMS OF DESIGN OF REDUNDANT NONCOLLINEAR CONFIGURATIONS WITH INERTIAL SENSORS

Authors

  • O. A. Sushchenko National Aviation University, Kyiv
  • V. O. Golitsyn National Aviation University, Kyiv

DOI:

https://doi.org/10.18372/1990-5548.58.13512

Keywords:

Inertial sensor, information processing, noncollinear configuration, rate gyroscope, redundancy

Abstract

The paper deals with basics tasks of the design of redundant noncollinear inertial measuring units based on the  technology of micrielectromechanical systems. Analysis of noncollinear configurations of inertial sensors is represented. The approach to the creation of the mathematical model of the inertial sensor is given. The basic problems of redundant information processing are discussed. The problem of optimal orientation of inertial sensors sensitivity axes in noncollinear configurations is studied. The approaches to conversion of redundant measuring information into projections of moving vehicles kinematical parameters are represented. The possibility to use the criterion of maximum a posteriori probability and least-squares method is considered. The ways to solve the above-mentioned problems are proposed. The obtained results can be useful for the  design of inertial measuring units of the wide class

Author Biographies

O. A. Sushchenko, National Aviation University, Kyiv

Aerospace Control Systems Department, Education & Research Institute of Air Navigation, Electronics and Telecommunications

Doctor of Engineering. Professor

V. O. Golitsyn, National Aviation University, Kyiv

Aerospace Control Systems Department, Education & Research Institute of Air Navigation, Electronics and Telecommunications

Post-graduate student

References

A. D. Epifanov, Redundant Systems of Aircraft Control. Moscow: Mashinostroenie, 1978, 178 p. (in Russian).

A. A. Volintsev, B.A. Kazakov, and I. E. Shutov, “Gyroscopic instrument of angular rate measurement. Experience of research of failures in operation”. Proceedings of MSTU named after N.E. Bauman, no. 5, 2015, pp. 136–151. (in Russian).

A. P. Parshin and Y. A. Nemshilov, “Development of measurement UAV attitude control unit with nonorthogonal arrangement of sensing elements,” Modern techniques and technologies, issue 3, 2016, URL: http://technology.snauka.ru/2016/03/9697.

X. Dai, L. Zhao, and Z. Shi, “Fault Tolerant Control in Redundant Inertial Navigation System,” Mathematical Problems in Engineering, vol. 2013, Article ID 782617, 11pp.

R. H. Rogne, T. H. Bryne, T. I. Fossen, and T. A. Johansen, “Redundant MEMS-Based Inertial Navigation Using Nonlinear Observers,” Journal of Dynamic Systems, Measurement, and Control, vol. 140, issue 7, pp. 071001–072009, 2018.

J. W. Song and C. G. Park, “Optimal Configuration of Redundant Inertial Sensors Considering Lever Arm Effect,” IEEE Sensors Journal, vol. 16, issue 9, pp. 3171–3180, 2016.

M. Jafari, “Optimal redundant sensor configuration for accuracy increasing in space inertial navigation system,” Aerospace Science and Technology, vol. 47, pp. 467–472, 2015.

M. Jafari and J. Roshanian, “Optimal Redundant Sensor Configuration for Accuracy and Reliability Increasing in Space Inertial Navigation Systems,” Journal of Navigation, vol. 66, Issue 02, pp. 199–208, 2012.

O. A. Sushchenko, Y. N. Bezkorovainyi, and N. D. Novytska, “Nonorthogonal redundant configurations of inertial sensors,” Proceedings of 2017 IEEE 4th International Conference Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD), October 17-19, Ukraine, pp. 73–78.

O. A., Sushchenko, Y. N. Bezkorovainyi, and N. D. Novytska, “Theoretical and Experimental Assessments of Accuracy of Nonorthogonal MEMS Sensor Aarrays,” Eastern European Journal of Enterprise Technologies, no. 3, pp. 78–87.

Silicon Sensing CRG20 model: Acess mode: http://wikis.controltheorypro.com/Silicon_Sensing_CRG20_Model

O.A. Sushchenko and Y.V. Beliavtsev, “Modelling of inertial sensors in UAV systems,” Proceedings of 2017 IEEE 4th International Conference on Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD), Kyiv, Ukraine, October 17-19, 2017, pp. 130–133.

V. M. Ageev and N. V. Pavlova, Aircraft instrumentation complexes and their design. Moscow: Mashinostroenie, 1990, 432 p. (in Russian).

A.D. Epifanov, Reliability of control systems, Moscow: Mashinostroenie, 1975, 180 p. (in Russian)

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Issue

Vol. 4 No. 58 (2018)

Section

COMPUTER-AIDED DESIGN SYSTEMS

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