Satellite Maneuver Evaluation Tool
dc.contributor.advisor | Loomis, Hershel H. | |
dc.contributor.advisor | Zyda, Michael J. | |
dc.contributor.author | Noriega, Carlos Ismael | |
dc.date.accessioned | 2013-11-20T23:33:47Z | |
dc.date.available | 2013-11-20T23:33:47Z | |
dc.date.issued | 1990 | |
dc.identifier.uri | http://hdl.handle.net/10945/37567 | |
dc.description | NA | en_US |
dc.description.abstract | When first introduced to orbital mechanics, students often experience difficulty in visualizing a satellite's actual path through space. The Satellite Maneuver Evaluation Tool (SMET) seeks to alleviate that problem. SMET is a three-dimensional color graphics simulation of satellites in flight. It allows a student to interactively modify a satellite's orbital parameters and see the effects as the satellites' positions are updated continuously with respect to time. The user can change parameters by defining a maneuver or by directly entering a change through keyboard or dial inputs. SMET offers the user the capability to demonstrate difficult concepts, as well as a method to simulate actual satellite maneuvers. Instructors can videotape SMET sessions for classroom demonstrations. Instantaneous images can also be saved for redisplay or for printout. This thesis provides a background on the mathematical formulas modeled by SMET. It also includes a detailed user's guide for SMET. | en_US |
dc.description.uri | http://archive.org/details/satellitemaneuve1094537567 | |
dc.format.extent | viii, 129 p.: ill. | en_US |
dc.language.iso | en_US | |
dc.publisher | Monterey, California. Naval Postgraduate School | en_US |
dc.rights | This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States. | en_US |
dc.subject.lcsh | Computer science | en_US |
dc.subject.lcsh | Astronautics | en_US |
dc.title | Satellite Maneuver Evaluation Tool | en_US |
dc.type | Thesis | en_US |
dc.contributor.secondreader | Loomis, Hershel H. | |
dc.contributor.secondreader | Zyda, Michael J. | |
dc.contributor.corporate | Naval Postgraduate School (U.S.) | |
dc.contributor.school | NA | |
dc.contributor.department | NA | |
dc.subject.author | Orbital mechanics | en_US |
dc.subject.author | Simulation | en_US |
dc.subject.author | Graphics workstation | en_US |
dc.description.funder | NA | en_US |
dc.description.recognition | NA | en_US |
dc.description.service | U.S. Marine Corps (U.S.M.C.) author. | en_US |
dc.identifier.oclc | ocn566196663 | |
etd.thesisdegree.name | M.S. in Systems Technology [Space Systems Operations] | en_US |
etd.thesisdegree.level | Masters | en_US |
etd.thesisdegree.discipline | Systems Technology [Space Systems Operations] | en_US |
etd.thesisdegree.grantor | Naval Postgraduate School | en_US |
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