Deep Learning Based Dynamics Identification and Linearization of Orbital Problems using Koopman Theory

arXiv:2403.08965v1 Announce Type: cross
Abstract: The study of the Two-Body and Circular Restricted Three-Body Problems in the field of aerospace engineering and sciences is deeply important because they help describe the motion of both celestial and artificial satellites. With the growing demand for satellites and satellite formation flying, fast and efficient control of these systems is becoming ever more important. Global linearization of these systems allows engineers to employ methods of control in order to achieve these desired results. We …

abstract aerospace artificial arxiv astro-ph.ep celestial cs.lg deep learning demand dynamics engineering identification linearization math.mp math-ph physics.space-ph satellite satellites study theory type