Inertial Navigation (original) (raw)

Abstract

Inertial navigation refers to the calculation of position, velocity, and orientation using measurements from inertial measurement units (IMUs) comprising accelerometers and gyroscopes. In particular, inertial navigation systems integrate forward in time the initial state of the systems replacing dynamic models with IMU measurements. This entry reviews the inertial navigation equations in a compact concise manner. Both the attitude and translational integration equations are presented. The work focuses on strapdown inertial measurement units, with particular emphasis on the algorithms used to compensate for the vehicle’s rotation.

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Authors and Affiliations

  1. University of Texas at Austin, Austin, TX, USA
    Renato Zanetti
  2. NASA Johnson Space Center, Houston, TX, USA
    Christopher D’Souza

Authors

  1. Renato Zanetti
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  2. Christopher D’Souza
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Correspondence toRenato Zanetti .

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Editors and Affiliations

  1. Electrical and Computer Engineering, Boston University, Boston, MA, USA
    John Baillieul
  2. Automation and Control Solutions, Honeywell, Golden Valley, MN, USA
    Tariq Samad

Section Editor information

  1. Georgia Institute of Technology, Atlanta, GA, USA
    Panagiotis Tsiotras

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© 2020 Springer-Verlag London Ltd., part of Springer Nature

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Zanetti, R., D’Souza, C. (2020). Inertial Navigation. In: Baillieul, J., Samad, T. (eds) Encyclopedia of Systems and Control. Springer, London. https://doi.org/10.1007/978-1-4471-5102-9\_100036-1

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