Attitude Determination and Control System for CubeSat
PublicDownloadable Content
open in viewerThis project continued the work on the development and testing of an Attitude Determination and Control Subsystem (ADCS) for a three-unit Cube Satellite mission led by WPI, the NASA Goddard Space Flight Center, and the Space Research Centre in Poland. This project focused on hardware selection in three areas: sensors, actuators, and processors. The attitude maintenance and control scheme was validated using numerical code written in MATLABĀ®. A secondary goal of the project was to outline a design for a test-bed where the control policies could be verified experimentally. This project developed a complete test-bed stand, leaving the construction portion for future ADCS teams, as well as recommendations for the parts to be used in the experimental section.
- 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
- E-project-030113-141835
- Advisor
- Year
- 2013
- Center
- Date created
- 2013-03-01
- Location
- Greenbelt
- Resource type
- Major
- Rights statement
Relations
- In Collection:
Items
Items
Thumbnail | Title | Visibility | Embargo Release Date | Actions |
---|---|---|---|---|
2013_ADC_Report_Final.pdf | Public | Download |
Permanent link to this page: https://digital.wpi.edu/show/vx021g92s