| 摘要 |
<p>The system has a main satellite (10) comprising a going intersatellite optical repeater including a wavelength demultiplexer to separate optical carriers transmitted by a bi-directional intersatellite link (13) and optical-electrical demodulators to demodulate optical signals from the link and to restore radio frequency signals. The main satellite includes a return intersatellite optical repeater with electro-optical modulators to modulate the carriers through radiofrequency signals from the cells and a wave length multiplexer to group the carriers to be emitted to a companion satellite (11).</p> |
