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 |