Abstract
Precision payloads require the spacecraft platform to provide an ultra-quiet working environment. Vibration isolators can be used for disturbance rejection purpose but may result in undesirable impact to the spacecraft attitude control performance. This paper studies the issues in relation to isolator-control interactions and proposed guidelines for selection of key parameters of a passive isolation system. An integrated design and analysis environment developed for high-fidelity control performance assessment is also introduced.
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.
