Abstract
AbstractWe test an approximation mechanism, recently proposed, on some relevant optimal control problems for satellites. Our emphasis is placed in the treatment of the full non-linear model with no linearization whatsoever. In addition to testing its performance for several typical manoeuvres, we also carried out some comparison with linearized models.
Full Text
Sign-in/Register to access full text options
Published version (Free)
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Similar Papers
Paper Title
Journal
Date