Abstract:
This paper addresses the problem of estimating the angular velocity given noisy attitude measurements for attitude control in small satellites. Based on contraction analy...Show MoreMetadata
Abstract:
This paper addresses the problem of estimating the angular velocity given noisy attitude measurements for attitude control in small satellites. Based on contraction analysis, a set of global exponentially convergent observers, namely, reduced-order, complete-order, and synchronized observers is designed. Simulations and experimental results are presented to illustrate their performance.
Published in: IEEE Transactions on Aerospace and Electronic Systems ( Volume: 54, Issue: 6, December 2018)