dc.contributor.author |
Chakravarthi, P. |
en_US |
dc.contributor.author |
Chen, C. |
en_US |
dc.date.accessioned |
2004-10-05T23:53:09Z |
|
dc.date.available |
2004-10-05T23:53:09Z |
|
dc.date.issued |
1994-04-04 |
en_US |
dc.identifier.citation |
Orlando, Florida, USA |
en_US |
dc.identifier.clearanceno |
94-0746 |
en_US |
dc.identifier.uri |
http://hdl.handle.net/2014/34400 |
|
dc.description.abstract |
Laser communication systems offer distinct advantages over radio frequency based systems for near earth and particularly for deep space communicaiton links. Some of the advantages are smaller size, lower power requirements and higher data rates. However, laser beam widths are very narrow and require more precise pointing, acquisition and tracking (PAT) compared to RF communication sytems. In addition to imprecise knowledge of relative position and complex relative motion between the spacecrafts, the problem of pointing and acquisition is complicated by vibrations present in the spacecraft. This paper analyzes the impact of satellite vibration on acquisition time and acquisition probability for a charge coupled device (CCD) based acquisition scheme. |
en_US |
dc.format.extent |
317799 bytes |
|
dc.format.mimetype |
application/pdf |
|
dc.language.iso |
en_US |
|
dc.subject.other |
laser communication spatial acquisition signal detection satellite vibration charge coupled device CCD |
en_US |
dc.title |
Spatial Acquisition in the Presence of Satellite Vibrations for Free Space Optical Communication Link |
en_US |