In-Situ Radio-Metric Tracking to Support Navigation for Interplanetary Missions with Multiple Spacecraft

Kahn, R. D.; Thurman, S. W.; Edwards, C. D.

dc.contributor.author	Kahn, R. D.	en_US
dc.contributor.author	Thurman, S. W.	en_US
dc.contributor.author	Edwards, C. D.	en_US
dc.date.accessioned	2004-10-06T01:29:45Z
dc.date.available	2004-10-06T01:29:45Z
dc.date.issued	1993-02	en_US
dc.identifier.citation	Pasadena, California, USA	en_US
dc.identifier.clearanceno	93-0377	en_US
dc.identifier.uri	http://hdl.handle.net/2014/34931
dc.description.abstract	Doppler and ranging measurements between spacecraft can be obtained only when the ratio of the total received signal power to noise power density at the receiving spacecraft is sufficiently large that reliable signal detection can be achieved within a reasonable time period.	en_US
dc.format.extent	706593 bytes
dc.format.mimetype	application/pdf
dc.language.iso	en_US
dc.subject.other	carrier signal acquisition doppler measurement precision ranging signal acquisition	en_US
dc.title	In-Situ Radio-Metric Tracking to Support Navigation for Interplanetary Missions with Multiple Spacecraft	en_US