Abstract
The problem of synthesis of a reduced ellipsoidal state observer is considered for multidimensional linear stationary dynamic systems. The algorithms developed possess the robustness property, i.e., they are not sensitive to violation of a priori assumptions ah he system. Computer simulation of an adaptive spacecraft attitude control system confirms the cjjiciency of the algorithm developed.
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.
