Acta Mechanica Sinica

, Volume 34, Issue 2, pp 400–408 | Cite as

Numerical algorithm for rigid body position estimation using the quaternion approach

Research Paper
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Abstract

This paper deals with rigid body attitude estimation on the basis of the data obtained from an inertial measurement unit mounted on the body. The aim of this work is to present the numerical algorithm, which can be easily applied to the wide class of problems concerning rigid body positioning, arising in aerospace and marine engineering, or in increasingly popular robotic systems and unmanned aerial vehicles. Following the considerations of kinematics of rigid bodies, the relations between accelerations of different points of the body are given. A rotation matrix is formed using the quaternion approach to avoid singularities. We present numerical procedures for determination of the absolute accelerations of the center of mass and of an arbitrary point of the body expressed in the inertial reference frame, as well as its attitude. An application of the algorithm to the example of a heavy symmetrical gyroscope is presented, where input data for the numerical procedure are obtained from the solution of differential equations of motion, instead of using sensor measurements.

Keywords

Rigid body Kinematics Inertial measurement unit Euler parameters Quaternion 

Notes

Acknowledgements

The project was supported by the Serbian Ministry of Education, Science and Technological Development (Grant 174016).

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Copyright information

© The Chinese Society of Theoretical and Applied Mechanics; Institute of Mechanics, Chinese Academy of Sciences and Springer-Verlag GmbH Germany 2017

Authors and Affiliations

  1. 1.Department of Mechanics, Faculty of Technical SciencesUniversity of Novi SadNovi SadSerbia

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