1986
DOI: 10.1117/12.961046
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Analysis Of Burst Error Occurrence On Optical Intersatellite Link (ISL) Design

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Cited by 13 publications
(3 citation statements)
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“…The performance of the space optical link is limited due to vibration of the pointing system caused by two stochastic mechanisms: (i) tracking noise created by the electro-optic tracker and (ii) vibrations created by internal satellite mechanical mechanisms. The effect of satellite vibration and platform jitter is described in [198]- [201]. Misalignment due to any of these reasons may result in link failure or severely degrade the performance of the system.…”
Section: Acquisition Tracking and Pointingmentioning
confidence: 99%
“…The performance of the space optical link is limited due to vibration of the pointing system caused by two stochastic mechanisms: (i) tracking noise created by the electro-optic tracker and (ii) vibrations created by internal satellite mechanical mechanisms. The effect of satellite vibration and platform jitter is described in [198]- [201]. Misalignment due to any of these reasons may result in link failure or severely degrade the performance of the system.…”
Section: Acquisition Tracking and Pointingmentioning
confidence: 99%
“…The acquisition procedure is first tread for formation of FSO link and it includes the transmission scanning with its limited beacon signal over an ambiguity range. In large background radiations, the beam location by the receiver helped with beacon signal which is having adequate peak power and small pulse rate [39]. The once the guide signal is identified, the accepting terminal utilizes beam controlling components to point a relentless guide signal towards the starting terminal frequently balanced by fixed PAA.…”
Section: Acquisition Tracking and Pointing (Atp)mentioning
confidence: 99%
“…. (I) (cosO,,1 -sinO,,1 0) (3) where 0 is the angular direction of the laser beam, f0 is the resonant frequency of the FPI when 8 is zero, f is the frequency deviation of the laser field from the resonant frequency, is the angular bias of the FPI, p is the index of refraction of the electro-optic cavity of the FPI, L is the length of the cavity of the FPI and c is the speed of light in vacuum.…”
Section: Design Of the Fpi For Simultaneous Spatial And Frequency Tramentioning
confidence: 99%