1 Chapter One 1. Using spherical coordinates, find the capacitance formed by two concentric spherical conducting shells of radius a, and b. What is the capacitance of a metallic marble with a diameter of 1cm in free space? Hint: let ๐๐ โ โ, thus, ๐ถ๐ถ = 4๐๐๐๐0 ๐๐ = 0.55๐๐๐๐.
Solution: Suppose the inner sphere has a surface charge density of +๐๐๐๐ . The outer surface charge density is negative, and proportionally smaller (by (๐๐/๐๐)2) to keep the total charge the same.
+ +ฯS
-
+ -
+ a + -
b
From Gaussโs law: ๏ฟฝ๐ซ๐ซ โ ๐๐๐บ๐บ = ๐๐ = +๐๐๐๐ 4๐๐๐๐2 ๐๐
Thus, inside the sphere (๐๐ โค ๐๐ โค ๐๐):
๐๐2 ๐๐ ๐๐ 2 ๐๐ Assuming a potential of ๐๐0 between the inner and outer surfaces, we have: ๐๐ 1 ๐๐2 ๐๐๐๐ 1 1 ๐๐0 = โ ๏ฟฝ ๐๐๐๐ 2 ๐๐๐๐ = ๐๐2 ( โ ) ๐๐ ๐๐ ๐๐ ๐๐ ๐๐ ๐๐ Thus: ๐๐ ๐๐๐๐ 4๐๐๐๐2 4๐๐๐๐ ๐ถ๐ถ = = = ๐๐0 ๐๐๐๐ ๐๐2 (1 โ 1) 1 โ 1 ๐๐ ๐๐ ๐๐ ๐๐ ๐๐ 1 In the case of a metallic marble, ๐๐ โ โ, and hence: ๐ถ๐ถ = 4๐๐๐๐0 ๐๐. Letting ๐๐0 = 36๐๐ ร ๐ซ๐ซ = ๐๐๐๐
5
10โ9 , and ๐๐ = 0.5๐๐๐๐, it yields ๐ถ๐ถ = 9 ๐๐๐๐ = 0.55๐๐๐๐.
2. Consider the parallel plate capacitor containing two different dielectrics. Find the total capacitance as a function of the parameters shown in the figure.
Area: A
d1
ฮต1
d2
ฮต2
Solution: Since in the boundary no charge exists (perfect insulator), the normal component of the electric flux density has to be equal in each dielectric. That is: ๐ซ๐ซ๐๐ = ๐ซ๐ซ๐๐
Accordingly:
๐๐1 ๐ฌ๐ฌ๐๐ = ๐๐2 ๐ฌ๐ฌ๐๐
Assuming a surface charge density of +๐๐๐๐ for the top plate, and โ๐๐๐๐ for the bottom plate, the electric field (or flux has a component only in z direction, and we have: ๐ซ๐ซ๐๐ = ๐ซ๐ซ๐๐ = โ๐๐๐๐ ๐๐๐๐
If the potential between the top ad bottom plates is ๐๐0, based on the line integral we obtain: ๐๐0 = โ ๏ฟฝ
๐๐1 +๐๐2
0
๐๐2
๐๐1 +๐๐2 โ๐๐๐๐ โ๐๐๐๐ ๐๐๐๐ ๐๐๐๐ ๐ฌ๐ฌ. ๐๐๐๐ = โ ๏ฟฝ ๐๐๐๐ โ ๏ฟฝ ๐๐๐๐ = ๐๐1 + ๐๐2 ๐๐2 ๐๐1 ๐๐1 ๐๐2 0 ๐๐2
Since the total charge on each plate is: ๐๐ = ๐๐๐๐ ๐ด๐ด, the capacitance is found to be: ๐ถ๐ถ =
๐๐ ๐ด๐ด = ๐๐0 ๐๐1 + ๐๐2 ๐๐1 ๐๐2
which is analogous to two parallel capacitors.
3. What would be the capacitance of the structure in problem 2 if there were a third conductor with zero thickness at the interface of the dielectrics? How would the electric field lines look? How does the capacitance change if the spacing between the top and bottom plates are kept the same, but the conductor thickness is not zero?
Solution: If the conductor is perfect, opposite charges are formed on the surface, but the capacitance remains the same, that is to say, the electric fields terminate to the conductor, but are not altered. If the conductor thickness is greater than zero, but the total distance between the top and bottom plates is the same (๐๐1 + ๐๐2 ), we expect the capacitance to increase.
4. Repeat problem 2 if the dielectric boundary were placed normal to the two conducting plates as shown below.
ฮต1
d
A2
A1 ฮต2
Solution: Similar to 2, the electric flux density is in z direction, and we assume a surface charge density of +๐๐๐๐1/2 for the top plates, and โ๐๐๐๐1/2 for the bottom plates. Assuming a potential of ๐๐0 between the plates, unlike 2, as ๐ซ๐ซ is tangent to the surface, in general ๐ซ๐ซ๐๐ โ ๐ซ๐ซ๐๐ . Thus, we do not assume a uniform charge density on the plates. Furthermore, based on the line integral definition, at the boundary the tangent components of the electric field (which are in z direction) must be equal between the two dielectrics, that is: ๐ฌ๐ฌ๐๐ = ๐ฌ๐ฌ๐๐
which yields:
๐๐๐๐1 ๐๐๐๐2 = ๐๐1 ๐๐2
Finally, for the potential the line integral yields: ๐๐0 =
The total charge is: ๐๐ = ๐๐๐๐1 ๐ด๐ด1 + ๐๐๐๐2 ๐ด๐ด2
๐๐๐๐1 ๐๐๐๐2 ๐๐ = ๐๐ ๐๐1 ๐๐2
Consequently: ๐ถ๐ถ =
๐๐ ๐๐1 ๐ด๐ด1 + ๐๐2 ๐ด๐ด2 = ๐๐0 ๐๐
As expected, this case turns out to be similar to two series capacitances.
5. Analogues to the capacitance, using Ohmโs law, show that the leakage conductance of an โซ ๐๐โ ๐๐๐๐
almost perfect conductor with a non-infinite conductivity of ฯ is given by: ๐บ๐บ = ๐๐ โ๐๐ ๐ฌ๐ฌ.๐๐๐ณ๐ณ. Calculate the leakage conductance of a coaxial cable with radii a and b as was used throughout the chapter.
โซ
Solution: In a given conductor we have: ๐ผ๐ผ = ๏ฟฝ๐๐ โ ๐๐๐๐ ๐๐
where ๐๐ is the current density, and by definition, for a conductor: ๐๐ = ฯ๐๐. According to Ohmโs law: โซ ๐๐ โ ๐๐๐๐ โซ ๐๐ โ ๐๐๐๐ ๐ผ๐ผ ๐บ๐บ = = ๐๐ = ๐๐ ๐๐ ๐๐ โ โซ ๐ฌ๐ฌ. ๐๐๐ณ๐ณ โ โซ ๐ฌ๐ฌ. ๐๐๐ณ๐ณ which has a similar form as the capacitance equation: โฎ ๐ฌ๐ฌ โ ๐๐๐บ๐บ ๐๐ ๐ถ๐ถ = = ๐๐ ๐๐ ๐๐ โ โซ ๐ฌ๐ฌ. ๐๐๐ณ๐ณ Note that the surface integral in the capacitance equation is over a closed surface. 6. Consider a very long hollow charge-free super conductor cylindrical shell with inner and outer radios of a and b, respectively. A wire with a current I is placed at the center of the cylinder. Calculate the magnetic field inside and outside considering that the magnetic field inside the shell would have to be zero. If the current I is moved away from the center but inside the shell, how the magnetic fields inside and outside would alter?
I a
b
Solution: Based on Ampereโs law, for ๐๐ โค ๐๐ we have: ๏ฟฝ ๐ฏ๐ฏ โ ๐๐๐ณ๐ณ = ๐ผ๐ผ
Therefore:
๐ผ๐ผ ๐๐ 2๐๐๐๐ ๐๐ For (๐๐ โค ๐๐ โค ๐๐), that is inside the superconductor, the magnetic field (and flux) are zero. In practice, the magnetic flux needs to be constant, so that the voltage is zero. Otherwise, there will be an infinite current induced in the superconductor. In practice however, any small change in magnetic flux will induce an infinite current, and thus, ๐ฉ๐ฉ = 0. Furthermore, a ๐ฏ๐ฏ =
โ๐ผ๐ผ
surface current of 2๐๐๐๐ ๐๐๐๐ flows on the inner surface,
๐ผ๐ผ
Outside the conductor (๐๐ โฅ ๐๐), a surface current of 2๐๐๐๐ ๐๐๐๐ flows on the outer surface, and ๐ผ๐ผ
again, ๐ฏ๐ฏ = 2๐๐๐๐ ๐๐๐๐ .
If the current moves away from the center, ๐ฉ๐ฉ changes for ๐๐ โค ๐๐, but remains the same outside the conductor. The surface current on the inner shell is not uniform anymore, but remains the same for the outer shell.
7. What is the internal inductance (per length) of a long straight wire with a circular cross ๐๐ section of radius a (use energy definition)? Answer: 8๐๐0 .
Solution: Due to symmetry, we can argue that the magnetic field has only a component in the ๐๐๐๐ direction. The current density inside the wire (๐๐ โค ๐๐) is: ๐๐๐๐ 2 ๐๐ 2 ๐ฒ๐ฒ = ๐ผ๐ผ 2 ๐๐๐๐ = ๐ผ๐ผ 2 ๐๐๐๐ ๐๐๐๐ ๐๐ Accordingly, based on Ampereโs law, the magnetic field is found to be: ๐๐ 2 ๐ผ๐ผ 2 ๐๐ ๐ฏ๐ฏ = ๐๐ ๐๐๐๐ = ๐ผ๐ผ ๐๐ 2๐๐๐๐ 2๐๐๐๐2 ๐๐ Next, we shall find the magnetic energy per unit length inside the wire: ๐๐0 ๐๐0 1 ๐๐ 2๐๐ ๐๐ 2 ๐๐0 2 ๐๐ |๐๐| ๐๐๐ป๐ป = ๏ฟฝ dV = ๏ฟฝ ๏ฟฝ ๏ฟฝ (๐ผ๐ผ ) ๐๐๐๐๐๐๐๐๐๐๐๐๐๐ = ๐ผ๐ผ 2 ๐๐ 2 0 0 0 2๐๐๐๐2 16๐๐ 1
Equating the energy to: 2 ๐ฟ๐ฟ๐ผ๐ผ 2 , we obtain the inductance per unit length: ๐๐0 ๐ฟ๐ฟ = 8๐๐
8. Show that the DC inductance of a piece of wire with finite length l and radius r is: ๐ฟ๐ฟ = ๐๐0 ๐๐ 2๐๐
2๐๐
3
(๐๐๐๐ ๐๐ โ 4). What is the inductance of a copper bond-wire with length of 2mm and a
diameter of 25ยตm (practical bonding pads in integrated circuits are typically 50ร50ยตm2)?
Argue why traditionally, as a rule of thumb an inductance of 1nH/mm is assumed for bondwires. Solution: The inductance calculation is detailed by Rosa 1. There are two parts, the internal ๐๐ inductance, ๐ฟ๐ฟ๐๐๐๐๐๐ , which was calculated to be ๐ฟ๐ฟ๐๐๐๐๐๐ = 8๐๐0 ๐๐ in the previous problem, and the
external inductance. As for the external inductance, let us first find the magnetic field. From the law of BiotSavart, the magnetic field at a point P normal to the paper due to an element of length ๐๐๐๐ is: ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ ๐๐๐๐ = ๐ ๐ ๐ ๐ ๐ ๐ ๐ ๐ = 4๐๐๐ ๐ 2 4๐๐(๐ฅ๐ฅ 2 + (๐ฆ๐ฆ โ ๐๐)2 )3/2 where ๐ผ๐ผ is the wire current uniformly distributed, and the rest of the parameters are shown in the figure below.
Wire dx dy ฮธ
R
l
y
P
b x The magnetic field at P due to the entire length of the wire is then: ๐๐ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ ๐ผ๐ผ ๐๐ โ ๐๐ ๐๐ = ( + ) ๐ป๐ป = ๏ฟฝ 2 2 3/2 4๐๐๐๐ ๏ฟฝ๐ฅ๐ฅ 2 + (๐๐ โ ๐๐)2 โ๐ฅ๐ฅ 2 + ๐๐ 2 0 4๐๐(๐ฅ๐ฅ + (๐ฆ๐ฆ โ ๐๐) ) ๐ผ๐ผ
If the integral were to be taken from โโ to +โ, the field would be 2๐๐๐๐ as we calculated before for a piece of wire with infinite length. To find the inductance, we calculate the magnetic flux as follows: ๐๐ = ๏ฟฝ๐๐ โ ๐๐๐๐ = ๐๐
๐๐0 ๐ผ๐ผ โ ๐๐ ๐๐ โ ๐๐ ๐๐ ๏ฟฝ ๏ฟฝ ( + ) ๐๐๐๐๐๐๐๐ 4๐๐ ๐ฅ๐ฅ=๐๐ ๐๐=0 ๐ฅ๐ฅ๏ฟฝ๐ฅ๐ฅ 2 + (๐๐ โ ๐๐)2 ๐ฅ๐ฅโ๐ฅ๐ฅ 2 + ๐๐ 2
1 Edward B. Rosa, Bulletin of the Bureau of Standards, vol. 4, no.2 , pp 301-305, 1907.
which is found to be: ๐๐0 ๐ผ๐ผ ๐๐ + โ๐๐ 2 + ๐๐ 2 ๐๐ โ๐๐ 2 + ๐๐ 2 ๐๐[๐๐๐๐ + โ ] 2๐๐ ๐๐ ๐๐ ๐๐ From this the external inductance is: ๐๐ =
๐๐0 ๐๐ + โ๐๐ 2 + ๐๐ 2 ๐๐ โ๐๐ 2 + ๐๐ 2 ๐๐[๐๐๐๐ + โ ] 2๐๐ ๐๐ ๐๐ ๐๐ And the total inductance would be: ๐ฟ๐ฟ๐๐๐๐๐๐ =
๐๐0 ๐๐ + โ๐๐ 2 + ๐๐ 2 ๐๐ 1 โ๐๐ 2 + ๐๐ 2 ๐๐[๐๐๐๐ + + โ ] 2๐๐ ๐๐ ๐๐ 4 ๐๐ For ๐๐ โช ๐๐, the inductance is roughly: ๐๐0 2๐๐ 3 ๐ฟ๐ฟ โ ๐๐(๐๐๐๐ โ ) 2๐๐ ๐๐ 4 For typical values of ๐๐ = 12.5๐๐๐๐ , and ๐๐ = 2๐๐๐๐, the inductance is found to be about ๐ฟ๐ฟ = ๐ฟ๐ฟ๐๐๐๐๐๐ + ๐ฟ๐ฟ๐๐๐๐๐๐ =
2๐๐
2.01nH. Given the logarithmic nature of the term ๐๐๐๐ ๐๐ , as a rule of thumb we assign an inductance of about 1nH/mm for a piece of wire. For the reference, a 1mm long wire inductance is 0.87nH.
9. In Faradayโs experiment, assume the switch has a resistance of R, and the two coils are identical with an inductance of L. The battery voltage is VBAT. Find the time-varying current in the coil. Assuming the iron toroid has a large permeability, find the magnetic flux in the second coil and estimate the emf read by the galvanometer.
Solution: We use the following circuit model to obtain the current in the primary:
VBAT
i1
L
i2
emf
R VBAT t
Setting ๐ก๐ก = 0 at the instant of switch closing, the primary inductor current is readily found to be: ๐๐๐ต๐ต๐ต๐ต๐ต๐ต ๐๐1 = (1 โ ๐๐ โ๐ก๐ก/๐๐ ) ๐ ๐ where ๐๐ = ๐ฟ๐ฟ/๐ ๐ is the time constant. The secondary current (๐๐2 ) is equal to this, and from that the flux in the secondary is: ๐๐๐ต๐ต๐ต๐ต๐ต๐ต ๐๐2 = ๐ฟ๐ฟ๐ฟ๐ฟ2 = ๐ฟ๐ฟ (1 โ ๐๐ โ๐ก๐ก/๐๐ ) ๐ ๐ Thus, the voltage read by the galvanometer is: ๐๐๐๐2 ๐๐๐๐๐๐ = = ๐๐๐ต๐ต๐ต๐ต๐ต๐ต ๐๐ โ๐ก๐ก/๐๐ ๐๐๐๐ Indicating a voltage spike of ๐๐๐ต๐ต๐ต๐ต๐ต๐ต , decaying eventually to zero, as shown in the figure above.
10. Consider a series RLC circuit below where the inductor has an initial current of I0. Solve the circuit differential equation, and find the inductor current. What are the total energies stored in the inductor, and dissipated in the resistor over time?
I0
L
C
R
Solution: The differential equation describing the circuit is: ๐๐ 2 ๐๐๐ฟ๐ฟ ๐ ๐ ๐๐๐๐๐ฟ๐ฟ 1 + + ๐๐ = 0 2 ๐๐๐ก๐ก ๐ฟ๐ฟ ๐๐๐๐ ๐ฟ๐ฟ๐ฟ๐ฟ ๐ฟ๐ฟ
The equation may be solved readily using our findings for the parallel circuit, and the duality: ๐๐๐ฟ๐ฟ (๐ก๐ก) = ๐ผ๐ผ0
๐๐0 โ๐ผ๐ผ๐ผ๐ผ ๐๐ cos(๐๐๐๐ ๐ก๐ก + ๐๐) ๐๐๐๐
๐ฃ๐ฃ๐ถ๐ถ (๐ก๐ก) =
๐ผ๐ผ0 โ๐ผ๐ผ๐ผ๐ผ ๐๐ sin ๐๐๐๐ ๐ก๐ก ๐ถ๐ถ๐๐๐๐
where ๐ผ๐ผ = ๐ ๐ /2๐ฟ๐ฟ, and the rest of the parameters have been already defined for the parallel circuit. Additionally, we have:
vC(t)
-1
ฯi(t) From the equation, the signal must be multiplied by the instantaneous frequency (๐๐๐๐ ), integrated, multiplied by ๐๐๐๐ and integrated again, and subtracted from itself. Thus, the output of the system shown above is a sinusoid whose instantaneous frequency (the input of the system) is set by ๐๐๐๐ (๐ก๐ก). 24. Show that the following circuit may be employed as an FM demodulator. Propose a proper circuitry to perform the differentiation suitable for high frequencies.
Envelope Detector
d/dt
Hint: Use the circuit below known as a balanced slope demodulator.
+ vo(t) -
is
f0 < f C
f0 > f C
Solution: Given the FM signal: once differentiated, we will have:
is
๐ฃ๐ฃ๐ถ๐ถ (๐ก๐ก) = ๐ด๐ด๐ถ๐ถ ๐๐๐๐๐๐(๏ฟฝ ๐๐๐๐ (๐๐) ๐๐๐๐)
๐ฃ๐ฃ๐ถ๐ถโฒ = ๐ด๐ด๐ถ๐ถ ๐๐๐๐ (๐ก๐ก)๐ ๐ ๐ ๐ ๐ ๐ (๏ฟฝ ๐๐๐๐ (๐๐) ๐๐๐๐)
โ
Clearly, the envelope of the differentiated signal above is proportional to the instantaneous frequency. Thus, all needed is to pass ๐ฃ๐ฃ๐ถ๐ถโฒ thought an envelope detector, and extract ๐๐๐๐ (๐ก๐ก). This is then essentially an FM demodulator. Realizing a good differentiator at high frequency may not be a trivial task. A suitable circuit to accomplish this is shown above, and whose frequency response is depicted below.
ฯ01
ฯ02
ฯ
ฯC
Approximate Differentiator
The circuit, known as a balanced slope detector, comprises of two LC tanks, one slightly high tuned, where as the other is slightly low tuned with respect to the carrier frequency. The FM signal is fed to each tank, performing the differentiation, after which is passed to an envelope detector as desired. From the frequency response plotted above, once the two LC tanks outputs are subtracted, around the carrier frequency (๐๐๐ถ๐ถ ), the composite response may be approximated by a straight line, hence representing a differentiator (whose frequency response is ideally ๐พ๐พ๐พ๐พ). To understand better how the slope detector works, suppose the carrier frequency is ๐๐๐ถ๐ถ , and that the LC tanks are tuned to ๐๐01 and ๐๐02 respectively. Furthermore, we shall assume the two tanks have equal resistor (๐ ๐ ) and capacitor (๐ถ๐ถ), and only the inductors are different to tune them as desired. If the tank Q is high enough (say ten or more), the composite response may be expressed as: ๐ ๐ ๐ ๐ |๐๐๐๐ (๐๐๐๐)| โ โ 2 ๐๐ โ ๐๐02 2 ๏ฟฝ1 + ๏ฟฝ๐๐ โ ๐๐01 ๏ฟฝ ๏ฟฝ1 + ( ๐ผ๐ผ ) ๐ผ๐ผ 1
๐ต๐ต๐ต๐ต
where ๐๐01 and ๐๐02 are the tank center frequencies, and ๐ผ๐ผ = 2๐ ๐ ๐ ๐ = 2 . In addition, we shall set: ๐๐01 = ๐๐๐ถ๐ถ + ฮ๐๐ ๐๐02 = ๐๐๐ถ๐ถ โ ฮ๐๐
Which is to say the two tanks are symmetrically high and low tuned around carrier frequency (๐๐๐ถ๐ถ ) by an arbitrary amount of ฮ๐๐, whose optimum value, we shall determine shortly. To gain more insight, let us use Taylor series to expand |๐๐๐๐ (๐๐๐๐)|: |๐๐๐๐ (๐๐๐๐)| = |๐๐๐๐ (๐๐๐๐)|โฒ (๐๐ โ ๐๐๐ถ๐ถ ) + |๐๐๐๐ (๐๐๐๐)|โฒโฒโฒ(๐๐ โ ๐๐๐ถ๐ถ )3 + |๐๐๐๐ (๐๐๐๐)|โฒโฒโฒโฒโฒ(๐๐ โ ๐๐๐ถ๐ถ )5 + โฏ Note that the balanced operation results in even-order derivatives not to appear. One can verify that by choosing: 3 ฮ๐๐ = ๏ฟฝ ๐ผ๐ผ 2
the 3rd-order derivative is eliminated, and thus: |๐๐๐๐ (๐๐๐๐)| =
4๐ ๐ 3 ๐๐ โ ๐๐๐ถ๐ถ 64 ๐๐ โ ๐๐๐ถ๐ถ 5 ๏ฟฝ [ โ ๏ฟฝ ๏ฟฝ + โฏ] ๐ผ๐ผ ๐ผ๐ผ 5 5 625
For small frequency deviations with respect to bandwidth, the second terms may be ignored, and ๐๐โ๐๐๐ถ๐ถ
thus a linear response is obtained as desired. To be precise, for ๏ฟฝ
๐ผ๐ผ
๏ฟฝ < 0.5, the second terms is
less than 0.5% and shall be comfortably ignored. The slope detector may be realized using only one LC tank based on the same principle. However, the particular circuit proposed above has all the nice properties of the balanced circuits in general. More details of the circuit operation may be found in Clarke and Hess 4.
4 K. Clarke, and D. Hess, Communications circuits: analysis and design.
3 Chapter Three 1. Find the L matrix for the following circuits:
+ v1 -
i2
+ v2 -
Ideal
i1
L3
i2
i1
+ v1 -
L1
L2
L1
L2
+ v2 -
n1 : n 2 Solution: The voltages and currents are labeled as shown in the figure. For the circuit on the left, we can write: ๐๐ ๐๐ ๐๐ ๐๐ ๐ฃ๐ฃ1 = ๐ฟ๐ฟ1 ๐๐1 + ๐ฟ๐ฟ3 (๐๐1 + ๐๐2 ) = (๐ฟ๐ฟ1 + ๐ฟ๐ฟ3 ) ๐๐1 + ๐ฟ๐ฟ3 ๐๐2 ๐๐๐๐ ๐๐๐๐ ๐๐๐๐ ๐๐๐๐ ๐๐ ๐๐ ๐๐ ๐๐ ๐ฃ๐ฃ2 = ๐ฟ๐ฟ2 ๐๐2 + ๐ฟ๐ฟ3 (๐๐1 + ๐๐2 ) = ๐ฟ๐ฟ3 ๐๐1 + (๐ฟ๐ฟ2 + ๐ฟ๐ฟ3 ) ๐๐2 ๐๐๐๐ ๐๐๐๐ ๐๐๐๐ ๐๐๐๐ Thus: ๐ฟ๐ฟ + ๐ฟ๐ฟ3 ๐ฟ๐ฟ3 ๐ฟ๐ฟ = ๏ฟฝ 1 ๏ฟฝ ๐ฟ๐ฟ3 ๐ฟ๐ฟ2 + ๐ฟ๐ฟ3 For the circuit on right, we have: ๐๐ ๐๐1 ๐ฃ๐ฃ1 = ๐ฟ๐ฟ1 ๐๐1 + ๐ฃ๐ฃ2 ๐๐๐๐ ๐๐2 ๐๐ ๐๐1 ๐๐1 ๐๐ ๐๐ ๐ฃ๐ฃ2 = ๐ฟ๐ฟ2 ๏ฟฝ๐๐2 + ๐๐1 ๏ฟฝ = ๏ฟฝ ๐ฟ๐ฟ2 ๏ฟฝ ๐๐1 + ๐ฟ๐ฟ2 ๐๐2 ๐๐๐๐ ๐๐2 ๐๐2 ๐๐๐๐ ๐๐๐๐ Expressing ๐ฃ๐ฃ2 based on the currents in the ๐ฃ๐ฃ1 equation yields: ๐๐ ๐๐1 ๐๐ ๐๐1 ๐๐1 ๐๐ ๐๐1 ๐๐ ๐ฃ๐ฃ1 = ๐ฟ๐ฟ1 ๐๐1 + ๏ฟฝ๐ฟ๐ฟ2 ๏ฟฝ๐๐2 + ๐๐1 ๏ฟฝ๏ฟฝ = ๏ฟฝ๐ฟ๐ฟ1 + ( )2 ๐ฟ๐ฟ2 ๏ฟฝ ๐๐1 + ( ๐ฟ๐ฟ2 ) ๐๐2 ๐๐๐๐ ๐๐2 ๐๐๐๐ ๐๐2 ๐๐2 ๐๐๐๐ ๐๐2 ๐๐๐๐ Thus: ๐๐1 ๐๐1 ๐ฟ๐ฟ1 + ( )2 ๐ฟ๐ฟ2 ๐ฟ๐ฟ ๐๐2 ๐๐2 2 ๐ฟ๐ฟ = ๏ฟฝ ๏ฟฝ ๐๐1 ๐ฟ๐ฟ2 ๐ฟ๐ฟ2 ๐๐2 Notice that for both circuits, ๐ฟ๐ฟ12 = ๐ฟ๐ฟ21 .
2. Find the transfer function and input impedance of the double-tuned circuit shown below.
+ vIN -
i1 iS
R
C
M
L
i2 L C
R
+
vOUT -
ZIN Solution: For the coupled inductor, given the currents and voltages labeled above, we can write: ๐๐๐๐๐๐ ๐๐๐๐๐๐ ๐ผ๐ผ1 ๐๐ ๏ฟฝ๏ฟฝ ๏ฟฝ ๏ฟฝ ๐ผ๐ผ๐ผ๐ผ ๏ฟฝ = ๏ฟฝ ๐๐๐๐๐๐๐๐ ๐๐๐๐๐๐ ๐๐๐๐๐๐ ๐ผ๐ผ2 ๐๐
Or, solving for the currents, knowing that ๐๐ = ๐ฟ๐ฟ we arrive at:
1 (๐๐ โ ๐๐๐๐๐๐๐๐๐๐ ) ๐๐๐๐๐๐(1 โ ๐๐ 2 ) ๐ผ๐ผ๐ผ๐ผ 1 ๐ผ๐ผ2 = (โ๐๐๐๐๐ผ๐ผ๐ผ๐ผ + ๐๐๐๐๐๐๐๐ ) ๐๐๐๐๐๐(1 โ ๐๐ 2 ) ๐ผ๐ผ1 =
Furthermore, a KCL at the input yields: ๐ผ๐ผ๐ ๐ = ๐บ๐บ๐บ๐บ๐ผ๐ผ๐ผ๐ผ + ๐๐๐ถ๐ถ๐ถ๐ถ๐ถ๐ถ๐ผ๐ผ๐ผ๐ผ + ๐ผ๐ผ1 where ๐บ๐บ = 1/๐ ๐ . Also a KCL at the output gives: ๐บ๐บ๐บ๐บ๐๐๐๐๐๐ + ๐๐๐ถ๐ถ๐ถ๐ถ๐ถ๐ถ๐๐๐๐๐๐ + ๐ผ๐ผ2 = 0 Replacing ๐ผ๐ผ1 and ๐ผ๐ผ2 with their voltage equivalent in the two equations above, we will have: 1 ๐๐ ๏ฟฝ๐บ๐บ + ๐๐๐๐๐๐ + ๏ฟฝ ๐๐๐ผ๐ผ๐ผ๐ผ โ ๐๐ = ๐ผ๐ผ๐ ๐ 2 ๐๐๐๐๐๐(1 โ ๐๐ ) ๐๐๐๐๐๐(1 โ ๐๐ 2 ) ๐๐๐๐๐๐ โ๐๐ 1 ๐๐๐ผ๐ผ๐ผ๐ผ + ๏ฟฝ๐บ๐บ + ๐๐๐๐๐๐ + ๏ฟฝ ๐๐ =0 2 ๐๐๐๐๐๐(1 โ ๐๐ ) ๐๐๐๐๐๐(1 โ ๐๐ 2 ) ๐๐๐๐๐๐ We may directly solve the equations above for ๐๐๐๐๐๐๐๐ , but given the symmetry of the circuit, we take a different approach, which is easier and more intuitive. Let us define: ๐๐๐ผ๐ผ๐ผ๐ผ + ๐๐๐๐๐๐๐๐ ๐๐1 = 2 ๐๐๐ผ๐ผ๐ผ๐ผ โ ๐๐๐๐๐๐๐๐ ๐๐2 = 2 By adding and subtracting the main two equations, we will have: 1 ๏ฟฝ๐บ๐บ + ๐๐๐๐๐๐ + ๏ฟฝ ๐๐ = ๐ผ๐ผ๐ ๐ /2 ๐๐๐๐๐๐(1 + ๐๐) 1 1 ๏ฟฝ๐บ๐บ + ๐๐๐๐๐๐ + ๏ฟฝ ๐๐ = ๐ผ๐ผ๐ ๐ /2 ๐๐๐๐๐๐(1 โ ๐๐) 2 Thus:
1 1 ๐๐1 = ๐ ๐ ๐ผ๐ผ๐ ๐ ๐๐ ๐๐ 2 1 + ๐๐๐๐1 (๐๐ โ ๐๐1 ) 1 1 1 ๐๐2 = ๐ ๐ ๐ผ๐ผ๐ ๐ ๐๐ ๐๐ 2 1 + ๐๐๐๐2 (๐๐ โ ๐๐2 ) 2 where, as we defined in Chapter 3, 1 ๐๐1/2 = ๏ฟฝ๐ฟ๐ฟ๐ฟ๐ฟ(1 ยฑ ๐๐) ๐๐1/2 = ๐ ๐ ๐ ๐ ๐๐1/2 Thus, we finally arrive at: ๐๐๐๐๐๐๐๐ ๐ ๐ 1 1 = [ โ ] 2 1 + ๐๐๐๐ ๏ฟฝ ๐๐ โ ๐๐1 ๏ฟฝ 1 + ๐๐๐๐2 ( ๐๐ โ ๐๐2 ) ๐ผ๐ผ๐ ๐ 1 ๐๐ ๐๐2 ๐๐ ๐๐ 1 And: ๐๐๐ผ๐ผ๐ผ๐ผ ๐ ๐ 1 1 = [ + ] ๐๐๐ผ๐ผ๐ผ๐ผ = ๐๐ ๐๐ ๐ผ๐ผ๐ ๐ 2 1 + ๐๐๐๐ ๏ฟฝ โ 1 ๏ฟฝ 1 + ๐๐๐๐2 ( ๐๐ โ ๐๐2 ) 1 ๐๐ ๐๐2 ๐๐ ๐๐ 1 Which is the result we presented in Chapter 3 example. 3. Using parallel-series transformation, find the values of L and C to match the 250โฆ amplifier input resistance to 50โฆ.
L
C
RIN
Matching Network Solution: Using parallel to series conversion, the parallel ๐ ๐ ๐ผ๐ผ๐ผ๐ผ and ๐ถ๐ถ may be represented by a series resistance of: ๐๐๐ถ๐ถ 2 ๐ ๐ ๐ผ๐ผ๐ผ๐ผ ๐ ๐ ๐ผ๐ผ๐ผ๐ผ 2 + ๐๐๐ถ๐ถ 2 And a reactance of: ๐ ๐ ๐ผ๐ผ๐ผ๐ผ 2 โ๐๐๐ถ๐ถ ๐ ๐ ๐ผ๐ผ๐ผ๐ผ 2 + ๐๐๐ถ๐ถ 2 where ๐๐๐ถ๐ถ is the capacitance impedance. To match to ๐ ๐ ๐ ๐ = 50ฮฉ, we shall set:
๐ ๐ ๐ผ๐ผ๐ผ๐ผ
which results in:
๐๐๐ถ๐ถ 2
๐ ๐ ๐ผ๐ผ๐ผ๐ผ 2 + ๐๐๐ถ๐ถ 2
= ๐ ๐ ๐ ๐
๐ ๐ ๐ ๐ ๐๐๐ถ๐ถ = ๐ ๐ ๐ผ๐ผ๐ผ๐ผ ๏ฟฝ = 125ฮฉ ๐ ๐ ๐ผ๐ผ๐ผ๐ผ โ ๐ ๐ ๐ ๐
With ๐๐๐ถ๐ถ = 125ฮฉ, the corresponding series capacitive reactance is: ๐ ๐ ๐ผ๐ผ๐ผ๐ผ 2 โ๐๐๐ถ๐ถ = โ100ฮฉ ๐ ๐ ๐ผ๐ผ๐ผ๐ผ 2 + ๐๐๐ถ๐ถ 2 Accordingly, the series inductor reactance must be: ๐๐๐ฟ๐ฟ = 100ฮฉ.
4. Repeat the problem by using Smith Chart.
Solution: The calculations are shown on the chart below. We start with a resistance of 250โฆ, or normalized resistance of 5 shown as the point P1.
x3=0.4 r=1
P3 P2 r2=0.2
P1 P4 x4=-2
For ease of calculations, we convert that to a conductance of 0.2 shown as point P2, and perform the calculations in the admittance domain. To match to 50โฆ, we must move P2 on the mirrored version of r=1 circle as highlighted in the chart above. This corresponds to point P3, which is capacitive (note we are dealing with admittance). The other solution on the circle is inductive and hence invalid. On the chart we can read a value of x=0.4 for the point P3. Accordingly, the amount of capacitance needed to move P2 to P3 must be: 0.4 ๐๐๐ถ๐ถ โ1 = 50
Which leads to ๐๐๐ถ๐ถ = 125ฮฉ, as calculated in the previous problem. When converted back to impedance, we arrive at point P4, which clearly resides on r=1 circle, and whose normalized reactance is read to be -2 on the chart. Consequently, we shall add and inductance value of ๐๐๐ฟ๐ฟ = 2 ร 50 = 100ฮฉ to match to 50โฆ.
5. Using parallel-series transformation, design an LC matching network to match an amplifier with an input impedance of 20โฆ||1pF to 50โฆ.
20โฆ
1pF
-80โฆ
-80ร202/(202+802)=-4.7โฆ
20ร802/(202+802)=19โฆ
Solution: We shall first represent the amplifier with a series equivalent circuit as shown below. The steps are obvious, and depicted in the figure. We assume the frequency of operation is 2GHz, and hence the capacitance impedance will be -80โฆ.
XLโ=XL-4.7
XC
The series inductor from the matching network, along with the series capacitance from the amplifier itself may be represented by a net reactance of ๐๐๐ฟ๐ฟโฒ as follows: ๐๐๐ฟ๐ฟโฒ = ๐๐๐ฟ๐ฟ โ 4.7ฮฉ Converting the series combination of ๐๐๐ฟ๐ฟโฒ and the amplifier resistance (which is 19โฆ), we arrive at a new parallel resistance of: 192 + ๐๐๐ฟ๐ฟ โฒ2 19 Which is set to 50โฆ to create the desired impedance for matching. This results in ๐๐๐ฟ๐ฟโฒ = 24ฮฉ, or ๐๐๐ฟ๐ฟ = 28.7ฮฉ. From this, the shunt reactance is:
(192+XLโ2)/19
XC
XL
19โฆ
-4.7โฆ
(192+XLโ2)/XLโ
Next, we will add the matching network as shown below.
192 + ๐๐๐ฟ๐ฟ โฒ2 = 39ฮฉ ๐๐๐ฟ๐ฟ โฒ
And thus, ๐๐๐ถ๐ถ = โ39ฮฉ
6. Plot on Smith chart the impedance of a series RLC circuit over frequency. Solution: The impedance of the series RLC circuit is: 1 ๐๐ = ๐ ๐ + ๐๐๐๐๐๐ + = ๐ ๐ + ๐๐๐๐ ๐๐๐๐๐๐ And the reactance is: ๐ฟ๐ฟ(๐๐2 โ ๐๐0 2 ) ๐๐ = ๐๐ 1 where ๐๐0 = is the resonance frequency. The real part of the impedance is frequency โ๐ฟ๐ฟ๐ฟ๐ฟ
๐ ๐
independent, and hence the impedance resides on the constant ๐๐ = ๐ ๐ circle as shown below. 0
Above the resonance, the reactive part is negative, and the impedance moves on the constant ๐๐ circle, but in the bottom half of the chart. On the other hand, below resonance, the impedance is inductive and it moves on the top half of the constant ๐๐ circle.
R
ฯ<ฯ0 ฯ=ฯ0 ฯ>ฯ0
jX
ฯ0
At ๐๐0 , the impedance is purely resistive, and is shown above on the chart. At DC or infinity, it resides on the open circuit point at the far right of the chart. 7. Consider the following two-port system terminated to admittance ๐๐๐ฟ๐ฟ in the second port and to a voltage source ๐ฃ๐ฃ๐ ๐ with output admittance ๐๐๐ ๐ in the first port. (a) Prove that:
๐๐12 ๐๐21 ๐๐22 + ๐๐๐ฟ๐ฟ ๐๐12 ๐๐21 ๐๐๐๐๐๐๐๐ = ๐๐22 โ ๐๐11 + ๐๐๐๐ ๐๐๐ฟ๐ฟ ๐๐๐๐ ๐๐21 ๐ด๐ด๐ฃ๐ฃ = = โ (๐๐๐๐ + ๐๐11 )(๐๐๐ฟ๐ฟ + ๐๐22 ) โ ๐๐12 ๐๐21 ๐๐๐ ๐ (b) Repeat part (a) and calculate ๐๐๐๐๐๐ , ๐๐๐๐๐๐๐๐ and ๐ด๐ด๐ฃ๐ฃ in terms of Z parameters. ๐๐๐๐๐๐ = ๐๐11 โ
Ys
vs
[Y]
YIN
YL
YOUT
Solution: Assuming voltage and current phasors of ๐๐1, ๐๐2, ๐ผ๐ผ1 , and ๐ผ๐ผ2 at the two ports, we have: ๐ผ๐ผ1 = ๐๐๐ ๐ (๐๐๐ ๐ โ ๐๐1 ) ๐ผ๐ผ2 + ๐๐๐ฟ๐ฟ ๐๐2 = 0 Also from Y matrix definition: ๐ผ๐ผ1 = ๐๐11 ๐๐1 + ๐๐12 ๐๐2 ๐ผ๐ผ2 = ๐๐21 ๐๐1 + ๐๐22 ๐๐2 Accordingly: (๐๐๐ฟ๐ฟ + ๐๐22 )๐๐2 + ๐๐21 ๐๐1 = 0 Hence: โ๐๐21 ๐๐1 ๐ผ๐ผ1 = ๐๐11 ๐๐1 + ๐๐12 ๐๐2 = ๐๐11 ๐๐1 + ๐๐12 ๐๐๐ฟ๐ฟ + ๐๐22 which leads to the input admittance: ๐ผ๐ผ1 ๐๐12 ๐๐21 ๐๐๐ผ๐ผ๐ผ๐ผ = = ๐๐11 โ ๐๐1 ๐๐22 + ๐๐๐ฟ๐ฟ For the output admittance, by definition the source voltage must be shorted. Thus: ๐ผ๐ผ1 = โ๐๐๐ ๐ ๐๐1 , which leads to: ๐ผ๐ผ1 = ๐๐11 ๐๐1 + ๐๐12 ๐๐2 = โ๐๐๐ ๐ ๐๐1 Or: ๐๐12 ๐๐2 ๐๐1 = โ ๐๐11 + ๐๐๐ ๐ Thus: โ๐๐12 ๐๐2 ๐ผ๐ผ2 = ๐๐21 ๐๐1 + ๐๐22 ๐๐2 = ๐๐21 + ๐๐22 ๐๐2 ๐๐11 + ๐๐๐ ๐ which leads to the output admittance:
๐ผ๐ผ2 ๐๐12 ๐๐21 = ๐๐22 โ ๐๐2 ๐๐11 + ๐๐๐ ๐ Knowing the input admittance, the output admittance may have been deduced by inspection and given the symmetry of the circuit. To calculate the voltage gain, we have: ๐ผ๐ผ1 = ๐๐๐ ๐ (๐๐๐ ๐ โ ๐๐1 ) = ๐๐11 ๐๐1 + ๐๐12 ๐๐2 (๐๐๐ฟ๐ฟ + ๐๐22 )๐๐2 + ๐๐21 ๐๐1 = 0 Thus: โ(๐๐๐ฟ๐ฟ + ๐๐22 ) ๐๐๐ ๐ ๐๐๐ ๐ = (๐๐๐ ๐ + ๐๐11 )๐๐1 + ๐๐12 ๐๐2 = (๐๐๐ ๐ + ๐๐11 ) ๐๐2 + ๐๐12 ๐๐2 ๐๐21 which leads to the voltage gain: ๐๐2 ๐๐๐๐ ๐๐21 ๐ด๐ด๐ฃ๐ฃ = = โ (๐๐๐๐ + ๐๐11 )(๐๐๐ฟ๐ฟ + ๐๐22 ) โ ๐๐12 ๐๐21 ๐๐๐ ๐ Note that clearly: ๐๐๐ฟ๐ฟ = ๐๐2 . Similar procedure leads to very similar equations expressed in terms of impedances: ๐๐12 ๐๐21 ๐๐๐๐๐๐ = ๐๐11 โ ๐๐22 + ๐๐๐ฟ๐ฟ ๐๐12 ๐๐21 ๐๐๐๐๐๐๐๐ = ๐๐22 โ ๐๐11 + ๐๐๐๐ ๐๐๐ฟ๐ฟ ๐๐21 ๐ด๐ด๐ฃ๐ฃ = โ (๐๐๐๐ + ๐๐11 )(๐๐๐ฟ๐ฟ + ๐๐22 ) โ ๐๐12 ๐๐21 This is expected from duality. ๐๐๐๐๐๐๐๐ =
8. In problem 7, prove that the condition of ๐๐๐ ๐ + ๐๐๐๐๐๐ = 0 or ๐๐๐ฟ๐ฟ + ๐๐๐๐๐๐๐๐ = 0 for the boundary between stable and unstable regions both lead to (๐๐๐ ๐ + ๐๐11 )(๐๐๐ฟ๐ฟ + ๐๐22 ) โ ๐๐12 ๐๐21 = 0, which is equivalent to the condition that ๐ด๐ด๐ฃ๐ฃ approaches infinity.
Solution: The condition ๐๐๐ ๐ + ๐๐๐๐๐๐ = 0 for instance leads to: ๐๐12 ๐๐21 ๐๐๐ ๐ + ๐๐๐๐๐๐ = ๐๐๐ ๐ + ๐๐11 โ =0 ๐๐22 + ๐๐๐ฟ๐ฟ Thus: (๐๐๐ ๐ + ๐๐11 )(๐๐๐ฟ๐ฟ + ๐๐22 ) โ ๐๐12 ๐๐21 = 0 Exact same equation is deduced by setting ๐๐๐ฟ๐ฟ + ๐๐๐๐๐๐๐๐ to zero. In either condition the denominator of ๐ด๐ด๐ฃ๐ฃ approaches zero, or ๐ด๐ด๐ฃ๐ฃ approaches infinity.
9. In problem 7, when the input and output are simultaneously conjugate matched the power gain becomes maximum. This would happen if ๐๐๐ ๐ and ๐๐๐ฟ๐ฟ are found such that the following two equations are met: ๐๐12 ๐๐21 ๐๐๐๐๐๐ = ๐๐11 โ = ๐๐๐ ๐ โ ๐๐22 + ๐๐๐ฟ๐ฟ
๐๐12 ๐๐21 = ๐๐๐ฟ๐ฟโ ๐๐11 + ๐๐๐ ๐ Such ๐๐๐ ๐ and ๐๐๐ฟ๐ฟ are called ๐๐๐ ๐ ,๐๐๐๐๐๐ and ๐๐๐ฟ๐ฟ,๐๐๐๐๐๐ . (a) Prove that ๐๐๐ ๐ ,๐๐๐๐๐๐ and ๐๐๐ฟ๐ฟ,๐๐๐๐๐๐ are given by: ๐๐๐๐๐๐๐๐ = ๐๐22 โ
๐๐12 ๐๐21 + |๐๐12 ๐๐21 |(๐พ๐พ + โ๐พ๐พ 2 โ 1) 2๐ ๐ ๐ ๐ (๐๐22 ) ๐๐12 ๐๐21 + |๐๐12 ๐๐21 |(๐พ๐พ + โ๐พ๐พ 2 โ 1) ๐๐๐ฟ๐ฟ,๐๐๐๐๐๐ = 2๐ ๐ ๐ ๐ (๐๐11 ) ๐๐๐ ๐ ,๐๐๐๐๐๐ =
Where ๐พ๐พ is equal to: ๐พ๐พ =
2๐ ๐ ๐ ๐ (๐๐11 )๐ ๐ ๐ ๐ (๐๐22 )โ๐ ๐ ๐ ๐ (๐๐12 ๐๐21 ) |๐๐12 ๐๐21 |
๐๐
(b) Prove that under the above optimum condition the power gain is equal to: ๐บ๐บ๐๐ = ๏ฟฝ๐๐21 ๏ฟฝ (๐พ๐พ โ 12
โ๐พ๐พ 2 โ 1), which also proves that for a reciprocal network (๐๐21 = ๐๐12 ) the power gain is less than unity. As a special case, an LTI passive network cannot amplify the power. Solution: Solving the set of equations:
๐๐12 ๐๐21 โง๐๐๐ ๐ ,๐๐๐๐๐๐ โ = ๐๐11 โ โช ๐๐22 + ๐๐๐ฟ๐ฟ,๐๐๐๐๐๐ ๐๐12 ๐๐21 โจ๐๐ โ โช ๐ฟ๐ฟ,๐๐๐๐๐๐ = ๐๐22 โ ๐๐ + ๐๐ 11 ๐ ๐ ,๐๐๐๐๐๐ โฉ leads to the answer. The math is too difficult however, and instead, we take a more intuitive approach. We shall first find the power gain and the available gain of the circuit. By definition: ๐๐๐ฟ๐ฟ ๐๐2 2 ๐ ๐ ๐ ๐ [๐๐๐ฟ๐ฟ ] ๐บ๐บ๐๐ = =๏ฟฝ ๏ฟฝ ๐๐๐ผ๐ผ๐ผ๐ผ ๐๐1 ๐ ๐ ๐ ๐ [๐๐๐ผ๐ผ๐ผ๐ผ ] From the previous problem, we have: ๐๐12 ๐๐21 ๐๐๐ผ๐ผ๐ผ๐ผ = ๐๐11 โ ๐๐22 + ๐๐๐ฟ๐ฟ (๐๐๐ฟ๐ฟ + ๐๐22 )๐๐2 + ๐๐21 ๐๐1 = 0 Thus: ๐๐21 2 ๐ ๐ ๐ ๐ [๐๐๐ฟ๐ฟ ] ๐บ๐บ๐๐ = ๏ฟฝ ๏ฟฝ ๐๐๐ฟ๐ฟ + ๐๐22 ๐ ๐ ๐ ๐ [๐๐๐ผ๐ผ๐ผ๐ผ ] Interestingly, the power gain is only a function of ๐๐๐ฟ๐ฟ (and not ๐๐๐ ๐ ). Thus, assuming ๐๐๐ฟ๐ฟ = ๐บ๐บ๐ฟ๐ฟ + ๐๐๐ต๐ต๐ฟ๐ฟ , we can argue that the optimum condition occurs by maximizing the power gain. That is by setting: ๐๐๐๐๐๐ =0 ๐๐๐บ๐บ๐ฟ๐ฟ ๐๐๐๐๐๐ =0 ๐๐๐ต๐ต๐ฟ๐ฟ Similarly, the available gain is: