2011 International Conference on Space Optical Systems and Applications (ICSOS) 2011
DOI: 10.1109/icsos.2011.5783656
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Development of acquisition and tracking sensor for next-generation optical inter-satellite communication

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Cited by 5 publications
(4 citation statements)
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“…The power reduction corresponding to the uncertainty angle can be easily calculated from the radiation pattern of the circular aperture of the optical antenna [40]. Considering a residual pointing uncertainty < 10 µrad [35,41,42], the pointing loss can be estimated as 2 dB. In the power budget, we also have to take into account other losses due to non-idealities of the transmitter and the receiver.…”
Section: Loss Budgetmentioning
confidence: 99%
“…The power reduction corresponding to the uncertainty angle can be easily calculated from the radiation pattern of the circular aperture of the optical antenna [40]. Considering a residual pointing uncertainty < 10 µrad [35,41,42], the pointing loss can be estimated as 2 dB. In the power budget, we also have to take into account other losses due to non-idealities of the transmitter and the receiver.…”
Section: Loss Budgetmentioning
confidence: 99%
“…Moreover, the performance results of the control system, which consists of a fine pointing mechanism (FPM) [4] and fine pointing sensor (FPS) [3], are presented. This control system is very important for tracking the laser from the target satellite during communication.…”
Section: Introductionmentioning
confidence: 99%
“…This paper examines the various aspect of the optical intersatellite development. Figures 1 and 2 shows communication by laser beam between a LEO satellite and a data relay satellite in geostationary orbit GEO [1][2].…”
Section: Introductionmentioning
confidence: 99%