TY - GEN
T1 - A novel constrained quaternion filter
AU - Choukroun, Daniel
AU - Tamir, Uri
N1 - Publisher Copyright:
© 2019 Israel Annual Conference on Aerospace Sciences. All rights reserved.
PY - 2019/1/1
Y1 - 2019/1/1
N2 - This paper presents a novel quaternion filter from vector measurements that belongs to the realm of deterministic constrained least-squares estimation. Hinging on the interpretation of quaternion measurements errors as angular errors in a four-dimensional Euclidean space, a novel cost function is developed and a minimization problem is formulated under the quaternion unit-norm constraint. This approach sheds a new light on the Wahba problem and on the q-method. The optimal estimate can be interpreted as achieving the least angular distance among a collection of planes in ℝ4 that are constructed from the vector observations. The resulting batch algorithm is mathematically equivalent to the q-method. Yet, taking advantage of the gained geometric insight, a recursive algorithm is developed, where the update stage consists of a rotation in the four-dimensional Euclidean space. The rotation angle is empirically designed as a fading memory factor. The quaternion update stage is multiplicative thus preserving the estimated quaternion unit-norm and no iterative search for eigenvalues is required as opposed to the q-method. Simulations illustrate the convergence and accuracy properties of the proposed algorithm.
AB - This paper presents a novel quaternion filter from vector measurements that belongs to the realm of deterministic constrained least-squares estimation. Hinging on the interpretation of quaternion measurements errors as angular errors in a four-dimensional Euclidean space, a novel cost function is developed and a minimization problem is formulated under the quaternion unit-norm constraint. This approach sheds a new light on the Wahba problem and on the q-method. The optimal estimate can be interpreted as achieving the least angular distance among a collection of planes in ℝ4 that are constructed from the vector observations. The resulting batch algorithm is mathematically equivalent to the q-method. Yet, taking advantage of the gained geometric insight, a recursive algorithm is developed, where the update stage consists of a rotation in the four-dimensional Euclidean space. The rotation angle is empirically designed as a fading memory factor. The quaternion update stage is multiplicative thus preserving the estimated quaternion unit-norm and no iterative search for eigenvalues is required as opposed to the q-method. Simulations illustrate the convergence and accuracy properties of the proposed algorithm.
UR - http://www.scopus.com/inward/record.url?scp=85068189571&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:85068189571
T3 - 59th Israel Annual Conference on Aerospace Sciences, IACAS 2019
SP - 202
EP - 218
BT - 59th Israel Annual Conference on Aerospace Sciences, IACAS 2019
PB - Israel Annual Conference on Aerospace Sciences
T2 - 59th Israel Annual Conference on Aerospace Sciences, IACAS 2019
Y2 - 6 March 2019 through 7 March 2019
ER -