Analysis and design concept of a spacecraft spin management system contingency despin studyPublic
This project, prepared in coordination with NASA's Goddard Space Flight Center, creates and analyzes a model for taking a satellite out of an abnormally high spin. Using the software package MATLAB, the designers created an analytical model that simulates the behavior of the system. In addition, the team developed a preliminary design concept of a deployment mechanism.
- This report represents the work of one or more WPI undergraduate students submitted to the faculty as evidence of completion of a degree requirement. WPI routinely publishes these reports on its website without editorial or peer review.
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