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Izvestiya SFedU
Engineering sciences
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ISSN 1999-9429 print
ISSN 2311-3103 online
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  • OPTIMIZATION-BASED CALIBRATION OF MEMS NAVIGATION SYSTEM

    D.E. Chickrin , S.V. Golousov
    2021-08-11
    Abstract ▼

    Technologies of autonomous wheeled robotic systems are becoming more and more in demand
    lately. A separate type of application of such technology is an autonomous unmanned
    ground vehicle. Unlike other types of transport (air, water), ground vehicles need to periodically
    operate in full autonomy - when external communication with the infrastructure and other agents
    of the transport network is inaccessible. In such circumstances, the issue of autonomous navigation
    comes out on top, and increased requirements are imposed on positioning accuracy, especially
    in an anthropogenic environment, for example, when driving in an urban environment, along
    narrow mountain roads, and tunnels. One of the components of autonomous navigation is often an
    inertial assembly consisting of several accelerometers, gyroscopes, and magnetometers. To obtain
    a high-precision navigation solution based on an inertial assembly, it is required to properly calibrate
    it. A separate issue is automation and its cost for further scaling necessary for mass production.
    The article presents the theory and methodology for automated calibration of an inertial
    navigation system based on MEMS sensors by solving an optimization problem. The proposed
    technique does not require high-precision calibration equipment. The aim of the presented work is
    to develop methods and theory for the calibration of inertial navigation units. The article formulates
    general measurement models of sensors included in the inertial assembly, and proposes
    methods for calibrating the parameters of accelerometers and gyroscopes fixed relative to each
    other. The method of automation of the calibration process is presented, which does not require
    high-precision equipment. The results of the application of the developed methods for the calibration
    of a real inertial assembly are presented. A stand for automated calibration is presented.

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