Path: utzoo!utgpu!news-server.csri.toronto.edu!cs.utexas.edu!uunet!motcid!wang From: wang@motcid.UUCP (Jerry Wang) Newsgroups: sci.electronics Subject: Re: A question about a PLL synth loop filter Message-ID: <5057@shale8.UUCP> Date: 3 Nov 90 00:44:42 GMT References: <1990Oct31.210242.20619@aplcen.apl.jhu.edu> <12890@chaph.usc.edu> <46225@apple.Apple.COM> Organization: Motorola Inc., Cellular Infrastructure Div., Arlington Heights, IL Lines: 107 kchen@Apple.COM (Kok Chen) writes: >kjh@aludra.usc.edu (Kenneth J. Hendrickson) writes: >>In article <1990Oct31.210242.20619@aplcen.apl.jhu.edu> @aplvax.jhuapl.edu:mjj@stda.jhuapl.edu (Marshall Jose) writes: >>%I have been trying to understand a passive loop filter I have twice seen used >>%in ham radio construction articles. It looks like this: >>% >>% >>% O---VVVVV----+-------+------O >>% R1 | | >>% | > >>% | > R2 >>% | > >>% --- | >>% --- C1 | >>% | | >>% | --- >>% | --- C2 >>% | | >>% O------------+-------+------O >>% >>% >>% C(as + 1) >>% H(s) = --------------------- >>% 3 2 >>% s + ps + qs + r >>% >>Your first clue, is that since you have two energy storage devices, that >>you should have two poles. When I solve this, I get: >> c1r1 * s + 1 >>H(s) = --------------------------------------------- >> c1c2r1r2 * s^2 + (c2r2 + c1r1 + c2r1) * s + 1 >Ken, you forgot the ( K/s ) term of the VCO. I believe that in >Marshall's original posting, he gave the correct closed-loop transfer >function > H(s) = A(s)B(s)/( 1 + A(s)B(s) ) >where A(s) is the 2-pole filter above and B(s) is the VCO transfer >function. >I have always avoided 2nd-order loop filter for precisely this >reason. Very hard to estimate what a 3rd-order system would do. >One of the poles is necessarily real, and it's locus better not >fall on the wrong side of the plane. Agree. There is another way to look at this. 1. By eliminating C1 or making it negligibly small, this becomes a first order 'lag-lead' filter. The resulting second order PLL is stable by a properly chosen R2. 2. The above system is characterized by its damping factor d, and undamped natural frequency Wn. Wn = sqrt ( K / (T1+T2) ) -------- (1) d = Wn * (T2 + 1/K) / 2 -------- (2) where K is the loop gain determined by Kvco and N, N being the divide ratio in the feedback loop. T1 = R1*C2 T2 = R2*C2 The system has optimum unit (phase) step response when d =1. 3. Theoretically we can choose an arbitary Wn (which determines the frequency response of the system), calculate T2 by setting d = 1 in equation 2, then solve T1 by equation 1. Note: If the PLL is programable, K will vary based on the operating point of VCO and N value for the feedback counter. d will vary according to K. Under all situations, d >= 1 must be maintained in order to maintain the stability of the loop. 4. But PLL is unique in a way that the phase detector output is best modeled by a bipolar pulse train at the frequency of it's refernce input. The amount of 'glitch' attenuation priveded by the above lag-lead filter is roughly R1/(R1+R2), which is poor. The poorly attenuated phase detector output glitches will be translated into phase jitter by the VCO. 5. So how do we deal with this? a. Choose a Wn much much less than the reference frequency (this produces large T1 + T2). b. Follow the steps in #3 to determine T1 and T2. c. Now let's introduce a C1 to attenuate the phase detector output glitches at the reference frequency. Since the Wn is much much less than the reference frequency, R1*C1 can be much less than T1+T2 and becomes negligible as assumed in #1. d. The best strategy is still a clean VCO and a clean refernce input, which will generate pulses with nearly zero pulse width. The nearly zero energy associated with nearly zero pulse width will reduce the R1*C1 requirement. Jerry Wang (Motorola - Radio Telephone System Group)