Precise Real-Time Low Earth Orbitor Navigation With GPS

Bertiger, W.; Haines, B.; Kuang, D.; Lough, M.; Lichten, S.; Muellerschoen, R. J.; Vigue, Y.; Wu, S.

dc.contributor.author	Bertiger, W.	en_US
dc.contributor.author	Haines, B.	en_US
dc.contributor.author	Kuang, D.	en_US
dc.contributor.author	Lough, M.	en_US
dc.contributor.author	Lichten, S.	en_US
dc.contributor.author	Muellerschoen, R. J.	en_US
dc.contributor.author	Vigue, Y.	en_US
dc.contributor.author	Wu, S.	en_US
dc.date.accessioned	2004-09-25
dc.date.available	2004-09-25
dc.date.issued	1998-09-15	en_US
dc.identifier.citation	Institute of Navigation	en_US
dc.identifier.citation	Nashville, TN, U.S.A.	en_US
dc.identifier.clearanceno	98-1498	en_US
dc.identifier.uri	http://hdl.handle.net/2014/20508
dc.description.abstract	Technology is currently available to support real-time on-board knowledge of the position of a low earth orbitor at the 5-15 meter level using the civilian broadcast GPS signal with sophisticated models and filtering techniques onboard the spacecraft.	en_US
dc.format.extent	1321607 bytes
dc.format.mimetype	application/pdf
dc.language.iso	en_US
dc.subject.other	Navigation Low Earth Orbitor GPS	en_US
dc.title	Precise Real-Time Low Earth Orbitor Navigation With GPS	en_US