Attitude control system for the high energy transient experiment small satellite
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.
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| Format: | Thesis |
| Language: | eng |
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Massachusetts Institute of Technology
2008
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| Online Access: | http://hdl.handle.net/1721.1/42493 |
| _version_ | 1811086689549942784 |
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| author | Chang, Daniel H |
| author2 | Andreas von Flotow. |
| author_facet | Andreas von Flotow. Chang, Daniel H |
| author_sort | Chang, Daniel H |
| collection | MIT |
| description | Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991. |
| first_indexed | 2024-09-23T13:30:26Z |
| format | Thesis |
| id | mit-1721.1/42493 |
| institution | Massachusetts Institute of Technology |
| language | eng |
| last_indexed | 2024-09-23T13:30:26Z |
| publishDate | 2008 |
| publisher | Massachusetts Institute of Technology |
| record_format | dspace |
| spelling | mit-1721.1/424932019-04-11T03:18:35Z Attitude control system for the high energy transient experiment small satellite Chang, Daniel H Andreas von Flotow. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics Aeronautics and Astronautics Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991. Includes bibliographical references (p. 207-208). by Daniel H. Chang. M.S. 2008-09-03T15:49:56Z 2008-09-03T15:49:56Z 1991 1991 Thesis http://hdl.handle.net/1721.1/42493 25601150 eng M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission. http://dspace.mit.edu/handle/1721.1/7582 261 p. application/pdf Massachusetts Institute of Technology |
| spellingShingle | Aeronautics and Astronautics Chang, Daniel H Attitude control system for the high energy transient experiment small satellite |
| title | Attitude control system for the high energy transient experiment small satellite |
| title_full | Attitude control system for the high energy transient experiment small satellite |
| title_fullStr | Attitude control system for the high energy transient experiment small satellite |
| title_full_unstemmed | Attitude control system for the high energy transient experiment small satellite |
| title_short | Attitude control system for the high energy transient experiment small satellite |
| title_sort | attitude control system for the high energy transient experiment small satellite |
| topic | Aeronautics and Astronautics |
| url | http://hdl.handle.net/1721.1/42493 |
| work_keys_str_mv | AT changdanielh attitudecontrolsystemforthehighenergytransientexperimentsmallsatellite |