Year-end Sale % OFF 
Abstract
The paper presents the modeling and control design issues associated with a change in the operating environment for the Middeck Active Control Experiment (MACE): a Shuttle program scheduled to fly on STS-67, March 1995. MACE was designed to investigate the extent to which the on-orbit behavior of flexible spacecraft can be predicted and controlled using analysis and ground testing. In this paper, a refined analytic model is used to predict the on-orbit dynamics, and several techniques for estimating the on-orbit errors are discussed. Current closed-loop results using error models based on prior ground experiments predict a 35 dB performance improvement.
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.
