| dc.contributor.advisor | Richard H. Battin. | en_US |
| dc.contributor.author | Gossner, Jesse Ross | en_US |
| dc.date.accessioned | 2008-09-03T15:50:54Z | |
| dc.date.available | 2008-09-03T15:50:54Z | |
| dc.date.copyright | 1991 | en_US |
| dc.date.issued | 1991 | en_US |
| dc.identifier.uri | http://hdl.handle.net/1721.1/42498 | |
| dc.description | Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991. | en_US |
| dc.description | Includes bibliographical references (p. 93-94). | en_US |
| dc.description.statementofresponsibility | by Jesse Ross Gossner. | en_US |
| dc.format.extent | 94 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 | An analytic method of propagating a covariance matrix to a maneuver condition for linear covariance analysis during redezvous | 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 | 25601220 | en_US |
