Electronic – Second order RLC filter and load resistance choice

circuit analysisfilterimpedance-matchinglow passtransfer function

In this 2nd order, low-pass filter circuit

schematic

simulate this circuit – Schematic created using CircuitLab

I am interested in the transfer function

$$ H(s) = V_L (s) / V_g (s) $$

which is (hoping that I didn't make mistakes)

$$H(s) = V_g \displaystyle \frac{R_L}{s^2 L C R_L + s(C R_g R_L + L) + R_L + R_g}$$

Which could be the benefits of having

$$ R_L = \sqrt{L/C} $$

?

I have some notes referring to this condition as to a "matching condition" and this recalls some transmission lines concepts, but I don't know how the transfer function could be simplified by applying that condition.

Even with \$ R_g = R_L = \sqrt{L/C} \$ it can be written as

$$H(s) = V_g \displaystyle \frac{1}{s^2 L C R_L + s(C R_L + L / R_L) + 2}$$

$$H(s) = V_g \displaystyle \frac{1}{s^2 LC + 2s\sqrt{LC} + 2}$$

but, again, I don't see anything useful.

Does the complex conjugate poles have a particular position? Or what else?

Best Answer

Your selection \$R_g=R_L=\sqrt{L/C}\$ gives a conjugate-complex pole pair with a quality factor \$Q_p=0.707\$. Hence, this dimensioning gives you a passive second-order lowpass with Butterworth response (maximally flat). More than that, it can been shown that for each passive ladder structure (and your circuit is the simplest form of a ladder) the sensitivity to parts tolerances is at its theoretical minimum for \$R_g=R_L\$ (matched input and output terminations).

"Does the complex conjugate poles have a particular position?"

Yes - the position of the pole pair has an extraordinary property: The poles are located in the complex \$s\$-plane with a (negative) real part which is identical to the imaginary part (Re=Img). Hence, there is an angle of \$45^{\circ}\$ between a line pointing to the pole and the real axis.

UPDATE: The classical second-order function is \$H(s)=N(s)/D(s)\$. For a lowpass we have \$N(s)=A_o\$ (gain at \$\omega=0\$) and \$D(s)=[1+s/(\omega_pQ_p)+(s/\omega_p)^2]\$.

For finding the maximum of \$H(s)\$ we have to write down the magnitude of the complex function \$H(s=j\omega)\$. As a next step we find the first derivation (differential quotient) and set it to zero. So we find the frequency \$\omega\$, max where \$|H(j\omega)|\$ has its maximum - and inserting this frequency \$\omega\$, max into the expression for the magnitude \$|H(j\omega)|\$ we find the VALUE of the maximum, which is: $$|H,\text{max}|=\frac{A_oQ_p}{\sqrt{1-1/(2Q_p)^2}}$$

From these expressions we can derive that we have \$\omega\$,max=0 and \$|H,\text{max}|=A_o\$ for the special case \$Q_p=\sqrt{0.5}=0.7071\$. This allows the following interpretation:

For \$Q_p=0.7071\$ there is no amplitude peaking and the maximum is reached at \$\omega=0\$. More than that, the magnitude response for this 2nd-order filter has a "maximum flat" characteristic (Butterworth response).