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dc.contributor.authorCHI, DTen_US
dc.contributor.authorSU, YTen_US
dc.date.accessioned2014-12-08T15:03:16Z-
dc.date.available2014-12-08T15:03:16Z-
dc.date.issued1995-07-01en_US
dc.identifier.issn0018-9251en_US
dc.identifier.urihttp://dx.doi.org/10.1109/7.395249en_US
dc.identifier.urihttp://hdl.handle.net/11536/1825-
dc.description.abstractThe earth coverage area for a satellite in an Earth synchronous orbit with a non-zero inclination angle is a function of the time of day. Locating the area where an Earth terminal can establish a link with a geosynchronous satellite at a certain period of the day is of great concern to system designers: A special case of much interest is when the time period of satellite coverage is 24 h. Two simple and rapid algorithms for locating 24 h satellite coverage areas are presented. One of the proposed algorithms can also be applied to determine other airborne antenna coverage problems.en_US
dc.language.isoen_USen_US
dc.titleON A SATELLITE COVERAGE PROBLEMen_US
dc.typeArticleen_US
dc.identifier.doi10.1109/7.395249en_US
dc.identifier.journalIEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMSen_US
dc.citation.volume31en_US
dc.citation.issue3en_US
dc.citation.spage891en_US
dc.citation.epage896en_US
dc.contributor.department電信工程研究所zh_TW
dc.contributor.department電子與資訊研究中心zh_TW
dc.contributor.departmentInstitute of Communications Engineeringen_US
dc.contributor.departmentMicroelectronics and Information Systems Research Centeren_US
dc.identifier.wosnumberWOS:A1995RJ72800003-
dc.citation.woscount4-
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