Satellite receiver system having doppler frequency shift...

H - Electricity – 04 – B

Patent

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Details

H04B 7/195 (2006.01) H04B 7/01 (2006.01) H04B 7/185 (2006.01) H04L 27/227 (2006.01)

Patent

CA 2180143

A satellite receiver system (400) provides acquisition and frequency tracking of a Doppler-shifted radio signal received from an orbiting satellite. The satellite receiver system (400) includes a Costas phase-lock loop (100) that receives the radio signal and provides an error signal at an error signal output (134) for controlling a conversion frequency generated by a voltage controlled oscillator (200). The voltage controlled oscillator (200) is coupled to the Costas phase-lock loop (100) and generates the conversion frequency for down- converting the radio signal in the Costas phase-lock loop (100). The satellite receiver system (400) further includes a Doppler frequency acquisition and tracking element (300) coupled to the voltage controlled oscillator (200). The Doppler frequency acquisition and tracking element (300) adjusts the conversion frequency to compensate for a Doppler frequency shift occuring in the radio signal due to orbital motion of the orbiting satellite.

Un système de réception par satellite (400) assure l'acquisition et la poursuite en fréquence d'un signal radio à décalage Doppler reçu d'un satellite en orbite. Le système de réception par satellite (400) comporte une boucle de Costas à phase asservie (100) recevant le signal radio et délivrant un signal d'erreur par une sortie de signal d'erreur (134), commandant ainsi la fréquence de conversion générée par un oscillateur commandé en tension (200). Celui-ci est couplé à la boucle de Costas à phase asservie (100) et génère la fréquence de conversion utilisée par la boucle de Costas à phase asservie (100) pour abaisser la fréquence du signal radio. Le système de réception par satellite (400) comporte en plus un élément d'acquisition et de poursuite par décalage de fréquence Doppler (300) couplé à l'oscillateur commandé en tension (200). L'élément d'acquisition et de poursuite par décalage de fréquence Doppler (300) adapte la fréquence de conversion pour compenser le décalage de fréquence Doppler se produisant dans le signal radio en raison du défilement du satellite en orbite.

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