Abstract
In the final proximity of rendezvous, linear H <inf xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink">∞</inf> and nonlinear H <inf xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink">∞</inf> control method are adopt for orbital tracking control and attitude tracking control respectively. We use the same thrusters system to implement orbital and attitude control command simultaneously. Because of the coupling caused by implementation, orbital control and attitude control command may conflict; we adopt a logic coordination method to avoid this situation. To the best of our knowledge, this is the first solution for orbital and attitude coupling control by the same implementation system in the final proximity of rendezvous. Numerical simulation verifies the validity and feasibility.
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.
