Abstract
This paper studies the space rendezvous problem with the target spacecraft in an unknown elliptical orbit. By the measurements of the relative position and velocity between the chaser spacecraft and the target spacecraft, a control strategy is proposed to achieve autonomous rendezvous. In addition, the orbital information can be estimated in the rendezvous process, and then the orbital elements are calculated by the estimate information. Finally, the proposed approach is illustrated by simulations.
Sign-in/Register to access full text options 
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.
