Novel Attitude Estimation Of Strapdown Inertial Navigation Systems With Singular Value Decomposition Technique

  • Sivasubramaniam Nambi Naidu Guru Kashi University, Talwandi Sabo, Bathinda - 151001, India https://orcid.org/0000-0001-9313-622X
  • Ramesh Kumar Gupta Guru Kashi University, Talwandi Sabo, Bathinda - 151001, India
Keywords: Attitude estimation, Singular value decomposition, Transfer alignment, Moving launch platform, Critical error probability

Abstract

Davenport’s q method & the Singular Value Decomposition (SVD) method are the two vigorous estimators that reduces Wahba’s loss function. In these, the q method is slightly quicker due to its computation of optimum quaternion as an eigenvector of a symmetric 4x4 matrix through the prevalent eigenvalue. The ESOQ and ESOQ2 (EStimators of the Optimal Quaternion) and the QUEST (QUaternion ESTimator) algorithms are less determined as the extreme eigenvalue’s distinguishing polynomial equation is solved by them. These estimators are apt to track the undulations of the sea with equivalent precision and accurateness. The SVD method is chosen and shown to be the most robust of all the hostile methods for the orientation of SDINS (Strap-Down Inertial Navigation Systems) using rate matching observations at sea in this paper. SVD is known most robust decomposition of all the decompositions of a matrix. SVD based attitude estimation being a batch technique would suffer from much less computational issues.

Published
2022-05-11
How to Cite
Naidu, S., & Gupta, R. (2022). Novel Attitude Estimation Of Strapdown Inertial Navigation Systems With Singular Value Decomposition Technique. Defence Science Journal, 72(2), 281-289. https://doi.org/10.14429/dsj.72.17637
Section
Missile Systems