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U. Glaeser

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greater than one, the system is overdamped as the PLL output initially responds rapidly but then takes<br />

a long time to reach the final phase. The rate of the initial response increases and the rate of the final<br />

response decreases as the damping factor is increased above one.<br />

PLL with Higher-Order Roll-Off<br />

It is very common for an actual PLL implementation to contain an extra capacitor, C2, in shunt with the<br />

loop filter, as shown in Fig. 10.8. This capacitor may have been introduced intentionally for filtering or<br />

may result from parasitic capacitances within the resistor or at the input of the VCO.<br />

Because the charge pump and phase detector are activated once every reference frequency cycle, they<br />

can cause a periodic disturbance on the control voltage node. This disturbance is usually not an issue for<br />

loops with N equal to one because the disturbance will occur in every VCO cycle. However, the disturbance<br />

can cause a constant shift in the duty cycle of the VCO output. When N is greater than one, the disturbance<br />

will occur once every N VCO cycles, which could cause the first one or two of the N cycles to be different<br />

from the others, leading to jitter in the PLL output period. In the frequency domain, this periodic<br />

disturbance will cause sidebands on the fundamental peak of the VCO frequency spaced at intervals of<br />

the reference frequency.<br />

Capacitor C2 will help filter out this reference frequency noise by introducing a pole at ωC. It will<br />

decrease the magnitude of the reference frequency sidebands by the ratio of ω REF/ωC. However, the<br />

introduction of C2 can also cause stability problems for the PLL since it converts the PLL into a thirdorder<br />

system. In addition, C2 makes the analysis of the PLL much more difficult.<br />

The PLL is now characterized by the four loop parameters ω N, ωC, ζ, and N. The damping factor, ζ,<br />

is changed by C2 as follows:<br />

© 2002 by CRC Press LLC<br />

F REF<br />

N<br />

Phase<br />

Detect<br />

FIGURE 10.8 Typical PLL block diagram with C 2 (clock distribution omitted).<br />

U<br />

D<br />

Charge<br />

Pump<br />

ζ = 1�2 ⋅ (1 � N ⋅ I CH ⋅ K V ⋅ R 2 ⋅ C 2 �(C + C 2)) 0.5<br />

The loop bandwidth, ω N, is changed by C 2 through its dependency on ζ. The added pole in the openloop<br />

response is at frequency ω C given by<br />

ω C = (C + C 2) �(R ⋅ C ⋅ C 2)<br />

This pole can reduce the stability of the loop if it is too close to the loop bandwidth frequency. Typically,<br />

it should be set at least a factor of ten above the loop bandwidth so as not to compromise the stability loop.<br />

Because the stability of the loop is now established by both ζ and ω C�ω N, a figure of merit can be<br />

defined that represents the potential stability of the loop as<br />

ζ ⋅ ω C �ω N = (C/C 2 + 1)�2<br />

This definition is useful because it actually defines the maximum possible phase margin given an optimal<br />

choice for the loop gain magnitude.<br />

Consider the normalized loop gain magnitude and phase plots for the PLL with different ratios of C<br />

to C 2 shown in Fig. 10.9. From these plots, it is clear that the added pole at ω C causes the loop gain<br />

magnitude slope to increase to −40 dB per decade and the loop gain phase to “increase” to −180° above<br />

the frequency of the pole. Between the zero at 1/(R ⋅ C) and the pole at ω C there is a region where the<br />

C<br />

R<br />

C2 VCTRL VCO<br />

I CH (A) K V (Hz/V)<br />

F O

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