Method of measuring of angular orientation parameters in micromechanical inertial-satellite navigation systems

Method of measuring of angular orientation parameters in micromechanical inertial-satellite navigation systems

M. K. Filyashkin

 

Abstract

Are given the method of determination of angular parameters, which is used in micromechanicalinertial-satellite systems, constructed by the method of compensation or based on the reduced Kalmanfilter. Measurement errors of roll and pitch angles are investigated by the proposed method with aircraftperforming various maneuvers and with changing the acceleration and attitude

Keywords

Аccelerometer; acceleration; angular velocity sensor; angular orientation; compensation scheme

References

Filyashkin, М. К.; Mar’yasova, Т. І. “Suboptimal filtering algorithms in schemes for combining inertial-satellite systems by the method of compensation”. Electronics and control systems.

Kyiv. NAU. 2011. no. 4(28). pp. 100–106. (in Ukrainian).

Zakharin, F. М.; Sineglazov, V. М.; Filyashkin, М. K. Algorithmic software of inertialsatellite navigation systems: monograph. Kyiv. Edition NAU. 2011. 320 p. (in Ukrainian).

Mukhina, M. P.; Stoyan T. M. “Analysis of magnetometer components errors for correlation-extreme navigation.” Electronics and Control Systems, no. 2(34), 2012. pp. 142–148.