Proceedings, IEEE Aerospace Conference
DOI: 10.1109/aero.2002.1035265
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Carrier synchronization of offset QPSK for deep space telemetry

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Cited by 5 publications
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“…In summary, the channel is modeled according to the following steps. For a given transmission band (X, Ka or S) and SEP angle, we first obtain obtain the scintillation index m following [5] and the magnitude spectrum S r (f ) following [11]. Then, we consider a uniform sampling of S r (f ) in the unit interval in N H points and obtain the correlation coefficients ρ r (i), i = 0, .…”
Section: Solar Scintillation Channel Modelmentioning
confidence: 99%
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“…In summary, the channel is modeled according to the following steps. For a given transmission band (X, Ka or S) and SEP angle, we first obtain obtain the scintillation index m following [5] and the magnitude spectrum S r (f ) following [11]. Then, we consider a uniform sampling of S r (f ) in the unit interval in N H points and obtain the correlation coefficients ρ r (i), i = 0, .…”
Section: Solar Scintillation Channel Modelmentioning
confidence: 99%
“…were considered: the "Solar-X" scenario refers to a transmission in X band with SEP angle equal to 1 deg, whereas the "Solar-Ka" scenario emulates a Ka band transmission with SEP angle equal to 0.5 deg. In both cases, we used the parametrization of the channel magnitude spectrum in [11] and the scintillation index was chosen according to [5].…”
Section: Numerical Evaluationmentioning
confidence: 99%
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“…But the loop filter is very complex. The error function used in [1] is more complex but the loop filter is quite simple. Many other methods are based on the Costas loop.…”
Section: Introductionmentioning
confidence: 99%
“…Many carrier recovery methods of OQPSK are based on PLL [1]. The researches of PLL generally focus on design of the error function and the loop filter [2].…”
Section: Introductionmentioning
confidence: 99%