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      An Accurate Calibration Method Based on Velocity in a Rotational Inertial Navigation System

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          Abstract

          Rotation modulation is an effective method to enhance the accuracy of an inertial navigation system (INS) by modulating the gyroscope drifts and accelerometer bias errors into periodically varying components. The typical RINS drives the inertial measurement unit (IMU) rotation along the vertical axis and the horizontal sensors’ errors are modulated, however, the azimuth angle error is closely related to vertical gyro drift, and the vertical gyro drift also should be modulated effectively. In this paper, a new rotation strategy in a dual-axis rotational INS (RINS) is proposed and the drifts of three gyros could be modulated, respectively. Experimental results from a real dual-axis RINS demonstrate that the maximum azimuth angle error is decreased from 0.04° to less than 0.01° during 1 h. Most importantly, the changing of rotation strategy leads to some additional errors in the velocity which is unacceptable in a high-precision INS. Then the paper studies the basic reason underlying horizontal velocity errors in detail and a relevant new calibration method is designed. Experimental results show that after calibration and compensation, the fluctuation and stages in the velocity curve disappear and velocity precision is improved.

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          Most cited references37

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          Error compensation of an optical gyro INS by multi-axis rotation

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            Calibration of a Novel MEMS Inertial Reference Unit

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              A multi-position self-calibration method for dual-axis rotational inertial navigation system

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                Author and article information

                Contributors
                Role: Academic Editor
                Journal
                Sensors (Basel)
                Sensors (Basel)
                sensors
                Sensors (Basel, Switzerland)
                MDPI
                1424-8220
                28 July 2015
                August 2015
                : 15
                : 8
                : 18443-18458
                Affiliations
                School of Instrument Science and Opto-Electronics Engineering, Beihang University, Beijing 100191, China; E-Mails: victoryqian175@ 123456163.com (Q.Z.); lzj0601@ 123456buaa.edu.cn (Z.L.); pdfeng@ 123456126.com (P.F.)
                Author notes
                [* ]Author to whom correspondence should be addressed; E-Mail: 17wanglei@ 123456buaa.edu.cn ; Tel.: +86-10-8233-8337.
                Article
                sensors-15-18443
                10.3390/s150818443
                4570330
                26225983
                43b84389-2410-4b26-b5e3-c162313b4d6f
                © 2015 by the authors; licensee MDPI, Basel, Switzerland.

                This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution license ( http://creativecommons.org/licenses/by/4.0/).

                History
                : 29 June 2015
                : 24 July 2015
                Categories
                Article

                Biomedical engineering
                rotational inertial navigation system (rins),rotation modulation,rotation strategy,azimuth angle error,velocity errors

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