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Averaging quaternions

  • SUNY Buffalo
  • NASA Goddard Space Flight Center
  • Aeronautical Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

4 Scopus citations

Abstract

This paper presents an algorithm to average a set of quaternion observations. The average quaternion is determined by minimizing the weighted sum of the squared Probenius norms of the corresponding attitude matrix differences, subject to the unit-norm constraint in the determined solution. Two cases are presented: one that incorporates scalar weights and one that incorporates general weights on the quaternions. For both cases, the optimal quaternion is found from an eigenvalue/eigenvector decomposition of a matrix formed by the weights and quaternion observations. The relationship between the solution for the average quaternion and familiar q-method for attitude estimation is discussed. Also, the uniqueness of the solution is shown and the relationship of the matrix weighted case to maximum likelihood estimation is given.

Original languageEnglish
Title of host publicationAmerican Astronautical Society - Space Flight Mechanics 2007 - Advances in the Astronautical Sciences, Proceedings of the AAS/AIAA Space Flight Mechanics Meeting
Pages1675-1682
Number of pages8
StatePublished - 2007
Event17th Annual Space Flight Mechanics Meeting - Sedona, AZ, United States
Duration: Jan 28 2007 → Feb 1 2007

Publication series

NameAdvances in the Astronautical Sciences
Volume127 PART 2
ISSN (Print)0065-3438

Conference

Conference17th Annual Space Flight Mechanics Meeting
Country/TerritoryUnited States
CitySedona, AZ
Period01/28/07 → 02/1/07

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