Paper
16 August 1994 Functional testing of the Laser Intersatellite Transmission Experiment (LITE) engineering model
William C. Goltsos, Don M. Boroson, Catherine Ellen DeVoe
Author Affiliations +
Abstract
Acquisition and tracking performance of a space-based optical communications system engineering model has been quantitatively measured using a dedicated optical test set. The test set includes a beacon with simulated angle jitter for tracking, a heterodyne optical receiver, and an accurate, calibrated line- of-sight monitor. The system has the capability of measuring each component of the pointing and tracking budget with angles down to approximately 1% of a diffraction-limited bandwidth. Acquisition and handover-to-tracking probabilities exceeding 99.9% are achieved at power levels 9-dB below expected on-orbit levels, and tracking rejection with jitter amplitudes comparable to expected spacecraft levels has been measured optically at -70 dB. Point- ahead angle repeatability over a POM 15 bandwidth range is found to be better than 0.01 beamwidths.
© (1994) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
William C. Goltsos, Don M. Boroson, and Catherine Ellen DeVoe "Functional testing of the Laser Intersatellite Transmission Experiment (LITE) engineering model", Proc. SPIE 2123, Free-Space Laser Communication Technologies VI, (16 August 1994); https://doi.org/10.1117/12.184686
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KEYWORDS
Optical testing

Sensors

Optical tracking

Mirrors

Receivers

Heterodyning

Telescopes

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