Effect of microaccelerations on an optical space communication terminal

Details Effect of microaccelerations on an optical space communication terminal Effect of microaccelerations on an optical space communication terminal

May 1991

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1991spie.1522..278w&link_type=abstract

In: Optical space communication II; Proceedings of the Meeting, Munich, Germany, June 10, 11, 1991 (A93-32077 12-17), p. 278-287

Physics

Feedback Control, Optical Communication, Satellite Communication, Space Communication, Spaceborne Lasers, Vibration Effects, Optical Tracking, Telescopes, Transfer Functions

Scientific paper

The requirement for arcsec-range (and lower) beamwidths in future laser intersatellite systems entails the inducing of mechanical vibrations into the optical terminals by their host satellite. It is therefore critically important to know the level of microvibrations on a spacecraft for the design of the tracking control loop of an optical communications payload. An effort is presently made to optimize the tracking control loop of an optical communications payload, taking into account such error sources as detector noise and microvibrations.

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