Abstract
An adaptive output feedback control design methodology is presented for cooperative spacecraft rendezvous and docking system without velocity and angular velocity measurements. A Lagrangian derivation of the rendezvous and docking model is considered to produce position and attitude dynamics for pursue spacecraft relative target spacecraft, assuming that the target spacecraft follows controlled attitude trajectory and transmissions its attitude information to the pursuer real time. Then, a control law is designed to provide a filtered relative velocity and angular velocity measurement and a desired adaptive compensation with uniformly ultimately bounded relative position and attitude tracking under the pursuer inertia uncertainties and bounded external disturbances. The simulation results demonstrate the effectiveness of control algorithm for the cooperative spacecraft rendezvous and docking systems.
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.
