| dc.contributor.advisor | Ronald J. Proulx and Paul J. Cefola. | en_US |
| dc.contributor.author | Fonte, Daniel John | en_US |
| dc.date.accessioned | 2009-11-06T16:05:45Z | |
| dc.date.available | 2009-11-06T16:05:45Z | |
| dc.date.issued | 1993 | en_US |
| dc.identifier.uri | http://hdl.handle.net/1721.1/49587 | |
| dc.description | Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993. | en_US |
| dc.description | Includes bibliographical references (p. 305-315). | en_US |
| dc.description.statementofresponsibility | by Daniel Fonte, Jr. | en_US |
| dc.format.extent | 315 p. | en_US |
| dc.language.iso | eng | en_US |
| dc.publisher | Massachusetts Institute of Technology | en_US |
| dc.rights | 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. | en_US |
| dc.rights.uri | http://dspace.mit.edu/handle/1721.1/7582 | en_US |
| dc.subject | Aeronautics and Astronautics | en_US |
| dc.title | Implementing a 50x50 gravity field model in an orbit determination system | en_US |
| dc.type | Thesis | en_US |
| dc.description.degree | M.S. | en_US |
| dc.contributor.department | Massachusetts Institute of Technology. Department of Aeronautics and Astronautics | |
| dc.identifier.oclc | 29423259 | en_US |
