Abstract
In this paper, results of attitude control experiments using Engineering Test Satellite VI (ETS-VI) on orbit are introduced. ETS-VI is a three-axis-stabilized satellite launched by the National Space Development Agency of Japan (NASDA) in August 1994. Identification and attitude control experiments on orbit were one of the ETS-VI mission programs and were carried out from January to March in 1995. The attitude controllers were designed using H∞ control method and two-degree-of-freedom control method. Experimental results show the effectiveness of these controllers for artificial satellite control.
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.
