{"id":{"repo_id":"nps","oai_identifier":"oai:calhoun.nps.edu:10945/9504"},"canonical_url":"https://search.dev.ndltd.org/etd/nps/oai:calhoun.nps.edu:10945/9504","repository":{"repo_id":"nps","name":"Naval Postgraduate School","base_url":"https://calhoun.nps.edu/server/oai/request"},"display":{"title":"Evaluating a satellite surveillance system","abstract":"A simple analytic model is formulated which should prove useful for evaluating a satellite surveillance system. This model describes the fraction of orbits in which a long lived satellite will \"see\" a selected position on the earth's surface. The fraction of orbits, denoted by P, is a function of the latitude of the ground position in question, the orbital inclination of the satellite, and the sweep width of the satellite's sensor. P is used to find estimates for the mean time to nest sighting of a selected ground position given that position has suddenly become of interest, to estimate the number and locations of ground readout stations, and to estimate the number of times a satellite would sight a transitting object on the earth's surface. in addition, the application of P to the problems of optimum orbit, evasive countermeasures, and satellite weapon delivery is discussed.","abstract_html":"A simple analytic model is formulated which should prove useful for evaluating a satellite surveillance system. This model describes the fraction of orbits in which a long lived satellite will "see" a selected position on the earth's surface. The fraction of orbits, denoted by P, is a function of the latitude of the ground position in question, the orbital inclination of the satellite, and the sweep width of the satellite's sensor. P is used to find estimates for the mean time to nest sighting of a selected ground position given that position has suddenly become of interest, to estimate the number and locations of ground readout stations, and to estimate the number of times a satellite would sight a transitting object on the earth's surface. in addition, the application of P to the problems of optimum orbit, evasive countermeasures, and satellite weapon delivery is discussed.","abstract_has_math":false,"creators":["Clark, Rolf H."],"institution":"Monterey, California. U.S. Naval Postgraduate School","degree_name":null,"degree_level":null,"degree_discipline":null,"degree_department":"Department of Operations Analysis","school":null,"contributors":[],"advisors":["McMasters, Alan W."],"committee_chairs":[],"committee_members":[],"year":1966,"date_issued":"1966-10","date_published":"1966-10","updated_at":"2026-07-27T20:24:57Z","subjects":[],"languages":["en_US"],"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."],"rights_urls":[],"identifier_entries":[]},"links":{"outbound_url":"https://hdl.handle.net/10945/9504","outbound_label":"Handle","outbound_source":"dc:identifier.uri"},"metadata_groups":[{"id":"people","label":"People","entries":[{"key":"dc:contributor.advisor","label":"Advisor","values":["McMasters, Alan W."]},{"key":"dc:contributor.department","label":"Department","values":["Department of Operations Analysis"]},{"key":"dc:creator","label":"Author","values":["Clark, Rolf H."]}]},{"id":"academic_context","label":"Academic Context","entries":[{"key":"dc:date","label":"Dc Date","values":["October 1966"]},{"key":"dc:date.accessioned","label":"Dc Date Accessioned","values":["2012-08-09T19:31:58Z"]},{"key":"dc:date.available","label":"Dc Date Available","values":["2012-08-09T19:31:58Z"]},{"key":"dc:date.issued","label":"Date","values":["1966-10"]},{"key":"dc:publisher","label":"Institution","values":["Monterey, California. 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The fraction of orbits, denoted by P, is a function of the latitude of the ground position in question, the orbital inclination of the satellite, and the sweep width of the satellite's sensor. P is used to find estimates for the mean time to nest sighting of a selected ground position given that position has suddenly become of interest, to estimate the number and locations of ground readout stations, and to estimate the number of times a satellite would sight a transitting object on the earth's surface. in addition, the application of P to the problems of optimum orbit, evasive countermeasures, and satellite weapon delivery is discussed."]},{"key":"dc:title","label":"Title","values":["Evaluating a satellite surveillance system"]}]}],"canonical_facts":{"dc:contributor.advisor":["McMasters, Alan W."],"dc:contributor.department":["Department of Operations Analysis"],"dc:creator":["Clark, Rolf H."],"dc:date":["October 1966"],"dc:date.accessioned":["2012-08-09T19:31:58Z"],"dc:date.available":["2012-08-09T19:31:58Z"],"dc:date.issued":["1966-10"],"dc:description.abstract":["A simple analytic model is formulated which should prove useful for evaluating a satellite surveillance system. This model describes the fraction of orbits in which a long lived satellite will \"see\" a selected position on the earth's surface. The fraction of orbits, denoted by P, is a function of the latitude of the ground position in question, the orbital inclination of the satellite, and the sweep width of the satellite's sensor. P is used to find estimates for the mean time to nest sighting of a selected ground position given that position has suddenly become of interest, to estimate the number and locations of ground readout stations, and to estimate the number of times a satellite would sight a transitting object on the earth's surface. in addition, the application of P to the problems of optimum orbit, evasive countermeasures, and satellite weapon delivery is discussed."],"dc:identifier.uri":["https://hdl.handle.net/10945/9504"],"dc:language.iso":["en_US"],"dc:publisher":["Monterey, California. U.S. Naval Postgraduate School"],"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."],"dc:title":["Evaluating a satellite surveillance system"],"dc:type":["Thesis"]},"updated_at":"2026-07-27T20:24:57Z"}