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A low phase noise and low spur phase locked loop(PLL) frequency synthesizer for use in global navigation satellite system(GNSS) receivers is proposed. To get a low spur, the symmetrical structure of the phase frequencydetector(PFD)producesfourcontrolsignals,whichcanreachthechargepump(CP)simultaneously,and an improved CP is realized to minimize the charge sharing and the charge injection and make the current matched.Additionally, the delay is controllable owing to the programmable PFD, so the dead zone of the CP can be eliminated. The output frequency of the VCO can be adjusted continuously and precisely by using a programmable LC-TANK. The phase noise of the VCO is lowered by using appropriate MOS sizes. The proposed PLL frequency synthesizer is fabricated in a 0.18 m mixed-signal CMOS process. The measured phase noise at 1 MHz offset from the center frequency is –127.65 dBc/Hz and the reference spur is –73.58 dBc.
To get a low spur, the symmetrical structure of the phase frequencydetector (PFD) produces fuel control signals, whichcanreachthechargepump (CP ) simultaneously, and an improved CP is realized to minimize the charge sharing and the charge injection and make the current matched. Additionally, the delay is controllable due to the programmable PFD, so the dead zone of the CP can be eliminated. The VCO can be adjusted continuously and precisely by using a programmable LC-TANK. The phase noise of the VCO is lowered by using appropriate MOS sizes. The proposed PLL frequency synthesizer is fabricated in a 0.18 m mixed-signal CMOS process. The measured phase noise at 1 MHz offset from the center frequency is -127.65 dBc / Hz and the reference spur is -73.58 dBc.