Abstract
Satellite orbit transfer problems are treated using Feedback Linearization technique. The nonlinear dynamic system comprise of a spacecraft, which moves around the planet under the influence of Earth's gravitational field, whose dynamics is given by the two body problem. The trajectory is planned using optimal fuel transfer method, Hohmann Transfer. It gives the least speed change required for the coplanar transfer. Guidance law is designed using Feedback Linearization or Nonlinear Dynamic Inversion (NDI) technique, which transform a controllable nonlinear system into a linear form. The main objective is to plan the trajectory using Hohmann Transfer method and track it through Feedback Linearization technique.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
