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CS5317 Scheda tecnica(PDF) 13 Page - Cirrus Logic |
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CS5317 Scheda tecnica(HTML) 13 Page - Cirrus Logic |
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13 / 32 page ![]() characteristic form in which the damping factor, ζ, and the natural frequency, ωn , are evident: θ2 θ1 = 2 ζωns + ωn 2 s 2 + 2ζωns + ωn 2 Both the natur al frequency and the damping fac- tor are particularly important in determining the transient response of the phase-locked loop when subjected to a step input of phase or frequency. A family of curves are illustrated in Figure 6 that indicate the overshoot and stability of the loop as a function of the damping factor. Each response is plotted as a function of the normalized time, ωn t. For a given ζ and lock time, t, the ωn required can be determined. Alternatively, phase lock con- trol loop bandwidth may be a specified parameter. In some systems it may be desirable to reduce the -3dB bandwidth of the PLL control loop to re- duce the effects of jitter in the phase of the input clock. The 3 dB bandwidth of the PLL control loop is defined by the following equation: ω3dB = ωn √ 2 ζ2 + 1 + √ (2ζ2 + 1)2 + 1 The equations used to describe the PLL and the 3 dB bandwidth are valid only if the frequency of CLKIN is approximately 20 times greater than the 3 dB corner frequency of the control loop. Filter Components Using the equations which describe the transfer function of the PLL system, the following exter- nal filter component equations can be determined: C = KoKd N ωn 2 R = 2 ζωn N KoKd The gain factors (Ko, Kd) are specified in the Analog Characteristics table. In the event the sys- tem calls for very low bandwidth, hence a corresponding reduction in loop gain, the phase detector gain factor Kd can be reduced. A large series resistor (R1) can be inserted between the output of the detector and the filter. Then the 50 µA current sources will saturate to the supplies and yield the following gain factor: Kd ≈ −5V 2 πR1 0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 1.1 1.2 1.3 01 23 456 78 9 10 0.1 1 10 -10 -9 -8 -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 Figure 6a. θ2 Unit Step Response Figure 6b. Second Order PLL Frequency Response ω n t. θ 2 normalized to θ 1 ω/ω n 20 log( θ 2 / θ 1 ) ζ = 0.5 ζ = 0.6 ζ = 0.7 ζ = 0.8 ζ = 0.9 ζ = 1.0 ζ = 1.5 ζ = 2.0 ζ = 3.0 ζ = 10.0 ζ= 10.0 ζ= 0.5 ζ = 0.5 ζ = 10 CS5317 DS27F4 13 |
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