Student Work
Analysis and design concept of a spacecraft spin management system contingency despin study
公开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.
- Creator
- Publisher
- Identifier
- 03B003M
- Advisor
- Year
- 2003
- Center
- Date created
- 2003-01-01
- Resource type
- Major
- Rights statement
关系
- 属于 Collection:
项目
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