SINS/SNS integration based on loosely coupled scheme using extended Kalman filter
Published: 26.04.2019
Authors: Al Bitar N., Gavrilov A.I.
Published in issue: #4(88)/2019
DOI: 10.18698/2308-6033-2019-4-1870
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control