a complete 1ø system containing three feedback loops

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R. W. Erickson Department of Electrical, Computer, and Energy Engineering University of Colorado, Boulder

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Energy storage capacitor voltage then does not change, andthis capacitor does not store or release energy

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Page 1: A complete 1ø system containing three feedback loops

R. W. Erickson Department of Electrical, Computer, and Energy Engineering

University of Colorado, Boulder

Page 2: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 62 Chapter 18: PWM Rectifiers

A complete 1ø systemcontaining three feedback loops

Boost converter

Wide-bandwidth input current controller

vac(t)

iac(t) +

vg(t)

ig(t)

ig(t)vg(t)

+

vC(t)

i2(t)

Q1

L

C

D1

vcontrol(t)

Multiplier X

+–vref1(t)

= kxvg(t)vcontrol(t)

Rsva(t)

Gc(s)

PWM

Compensator

verr(t)

DC–DCConverter Load

+

v(t)

i(t)

d(t)

+–Compensatorand modulator

vref3

Wide-bandwidth output voltage controller

+–Compensatorvref2

Low-bandwidth energy-storage capacitor voltage controller

vC(t)

v(t)

Page 3: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 63 Chapter 18: PWM Rectifiers

Bandwidth of capacitor voltage loop

• The energy-storage-capacitor voltage feedback loop causes thedc component of vc(t) to be equal to some reference value

• Average rectifier power is controlled by variation of Re.

• Re must not vary too quickly; otherwise, ac line current harmonicsare generated

• Extreme limit: loop has infinite bandwidth, and vc(t) is perfectlyregulated to be equal to a constant reference value

• Energy storage capacitor voltage then does not change, andthis capacitor does not store or release energy

• Instantaneous load and ac line powers are then equal

• Input current becomes

iac(t) =pac(t)vac(t)

= pload(t)vac(t)

= Pload

VM sin ωt

Page 4: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 64 Chapter 18: PWM Rectifiers

Input current waveform, extreme limit

vac(t)

iac(t)

t

iac(t) =pac(t)vac(t)

= pload(t)vac(t)

= Pload

VM sin ωt THD → ∞

Power factor → 0

So bandwidth ofcapacitor voltageloop must belimited, and THDincreases rapidlywith increasingbandwidth

Page 5: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 65 Chapter 18: PWM Rectifiers

18.4.2 Modeling the outer low-bandwidthcontrol system

This loop maintains power balance, stabilizing the rectifier outputvoltage against variations in load power, ac line voltage, andcomponent valuesThe loop must be slow, to avoid introducing variations in Re at theharmonics of the ac line frequency

Objective of our modeling efforts: low-frequency small-signal modelthat predicts transfer functions at frequencies below the ac linefrequency

Page 6: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 66 Chapter 18: PWM Rectifiers

Large signal modelaveraged over switching period Ts

Re (vcontrol )⟨ vg(t)⟩Ts

vcontrol

+

Ideal rectifier (LFR)

acinput

dcoutput

+–

⟨ ig(t)⟩Ts

⟨p(t)⟩Ts

⟨ i2(t)⟩Ts

⟨ v(t)⟩TsC Load

Ideal rectifier model, assuming that inner wide-bandwidth loopoperates ideally

High-frequency switching harmonics are removed via averaging

Ac line-frequency harmonics are included in model

Nonlinear and time-varying

Page 7: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 67 Chapter 18: PWM Rectifiers

Predictions of large-signal model

Re (vcontrol )⟨ vg(t)⟩Ts

vcontrol

+

Ideal rectifier (LFR)

acinput

dcoutput

+–

⟨ ig(t)⟩Ts

⟨p(t)⟩Ts

⟨ i2(t)⟩Ts

⟨ v(t)⟩TsC Load

vg(t) = 2 vg,rms sin ωt

If the input voltage is

Then theinstantaneous poweris:

p(t) Ts=

vg(t) Ts

2

Re(vcontrol(t))=

vg,rms2

Re(vcontrol(t))1 – cos 2ωt

which contains a constant term plus a second-harmonic term

Page 8: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 68 Chapter 18: PWM Rectifiers

Separation of power source into its constant andtime-varying components

+

⟨ i2(t)⟩Ts

⟨ v(t)⟩TsC LoadV g,rms

2

Re–

V g,rms2

Recos2 2ωt

Rectifier output port

The second-harmonic variation in power leads to second-harmonicvariations in the output voltage and current

Page 9: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 69 Chapter 18: PWM Rectifiers

Removal of even harmonics via averaging

t

v(t)

⟨ v(t)⟩T2L

⟨ v(t)⟩Ts

T2L = 122πω = π

ω

Page 10: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 70 Chapter 18: PWM Rectifiers

Resulting averaged model

+

⟨ i2(t)⟩T2L

⟨ v(t)⟩T2LC LoadV g,rms

2

Re

Rectifier output port

Time invariant model

Power source is nonlinear

Page 11: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 71 Chapter 18: PWM Rectifiers

Perturbation and linearization

v(t) T2L= V + v(t)

i2(t) T2L= I2 + i2(t)

vg,rms = Vg,rms + vg,rms(t)vcontrol(t) = Vcontrol + vcontrol(t)

V >> v(t)I2 >> i2(t)

Vg,rms >> vg,rms(t)

Vcontrol >> vcontrol(t)

Let with

The averaged model predicts that the rectifier output current is

i2(t) T2L=

p(t) T2L

v(t) T2L

=vg,rms2 (t)

Re(vcontrol(t)) v(t) T2L

= f vg,rms(t), v(t) T2L, vcontrol(t))

Page 12: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 72 Chapter 18: PWM Rectifiers

Linearized result

I2 + i2(t) = g2vg,rms(t) + j2v(t) –vcontrol(t)

r2

g2 =df vg,rms, V, Vcontrol)

dvg,rmsvg,rms = Vg,rms

= 2Re(Vcontrol)

Vg,rms

V

where

– 1r2

=df Vg,rms, v T2L

, Vcontrol)

d v T2L v T2L= V

= – I2V

j2 =df Vg,rms, V, vcontrol)

dvcontrolvcontrol = Vcontrol

= –V g,rms2

VRe2(Vcontrol)

dRe(vcontrol)dvcontrol vcontrol = Vcontrol

Page 13: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 73 Chapter 18: PWM Rectifiers

Small-signal equivalent circuit

C

Rectifier output port

r2g2 vg,rms j2 vcontrol R

i2+

v

v(s)vcontrol(s)

= j2 R||r2 11 + sC R||r2

v(s)vg,rms(s)

= g2 R||r2 11 + sC R||r2

Predicted transfer functions

Control-to-output

Line-to-output

Page 14: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 74 Chapter 18: PWM Rectifiers

Model parameters

Table 18.1 Small-signal model parameters for several types of rectifier control schemes

Controller type g2 j2 r2

Average current control withfeedforward, Fig. 18.14 0

Current-programmed control,Fig. 18.16

Nonlinear-carrier charge controlof boost rectifier, Fig. 18.21

Boost with critical conduction mode control, Fig. 18.20

DCM buck-boost, flyback, SEPIC,or Cuk converters

PavVVcontrol

V 2

Pav

2PavVVg,rms

PavVVcontrol

V 2

Pav

2PavVVg,rms

PavVVcontrol

V 2

2Pav

2PavVVg,rms

PavVVcontrol

V 2

Pav

2PavVVg,rms

2PavVD

V 2

Pav

Page 15: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 75 Chapter 18: PWM Rectifiers

Constant power load

vac(t)

iac(t)

Re

+

Ideal rectifier (LFR)

C

i2(t)ig(t)

vg(t)

i(t)

load

+

v(t)

pload(t) = VI = Pload

Energy storagecapacitor

vC(t)

+

Dc-dcconverter

+–Pload V

⟨ pac(t)⟩Ts

Rectifier and dc-dc converter operate with same average power

Incremental resistance R of constant power load is negative, and is

R = – V 2

Pav

which is equal in magnitude and opposite in polarity to rectifierincremental output resistance r2 for all controllers except NLC

Page 16: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 76 Chapter 18: PWM Rectifiers

Transfer functions with constant power load

v(s)vcontrol(s)

=j2

sC

v(s)vg,rms(s)

=g2sC

When r2 = – R, the parallel combination r2 || R becomes equal to zero.The small-signal transfer functions then reduce to

Page 17: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 77 Chapter 18: PWM Rectifiers

18.5 RMS values of rectifier waveforms

t

iQ(t)

Doubly-modulated transistor current waveform, boost rectifier:

Computation of rms value of this waveform is complex and tedious

Approximate here using double integral

Generate tables of component rms and average currents for variousrectifier converter topologies, and compare

Page 18: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 78 Chapter 18: PWM Rectifiers

RMS transistor current

t

iQ(t)RMS transistor current is

IQrms = 1Tac

iQ2 (t)dt

0

Tac

Express as sum of integrals overall switching periods containedin one ac line period:

IQrms = 1Tac

Ts1Ts

iQ2 (t)dt

(n-1)Ts

nTs

∑n = 1

Tac/Ts

Quantity in parentheses is the value of iQ2, averaged over the nth

switching period.

Page 19: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 79 Chapter 18: PWM Rectifiers

Approximation of RMS expression

IQrms = 1Tac

Ts1Ts

iQ2 (t)dt

(n-1)Ts

nTs

∑n = 1

Tac/Ts

When Ts << Tac, then the summation can be approximated by anintegral, which leads to the double-average:

IQrms ≈1

TaclimTs→0

Ts1Ts

iQ2 (τ)dτ

(n-1)Ts

nTs

∑n=1

Tac/Ts

= 1Tac

1Ts

iQ2 (τ)dτ

t

t+Ts

0

Tac

dt

= iQ2 (t)

Ts Tac

Page 20: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 80 Chapter 18: PWM Rectifiers

18.5.1 Boost rectifier example

For the boost converter, the transistor current iQ(t) is equal to the inputcurrent when the transistor conducts, and is zero when the transistoris off. The average over one switching period of iQ

2(t) is therefore

iQ2

Ts= 1Ts

iQ2 (t)dt

t

t+Ts

= d(t)iac2 (t)

If the input voltage isvac(t) = VM sin ωt

then the input current will be given by

iac(t) =VMRe

sin ωt

and the duty cycle will ideally beV

vac(t)= 11 – d(t)

(this neglectsconverter dynamics)

Page 21: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 81 Chapter 18: PWM Rectifiers

Boost rectifier example

Duty cycle is therefored(t) = 1 – VM

V sin ωt

Evaluate the first integral:

iQ2

Ts= V M

2

Re2 1 – VM

V sin ωt sin2 ωt

Now plug this into the RMS formula:

IQrms = 1Tac

iQ2

Ts0

Tac

dt

= 1Tac

V M2

Re2 1 – VM

V sin ωt sin2 ωt0

Tac

dt

IQrms = 2Tac

V M2

Re2 sin2 ωt – VM

V sin3 ωt0

Tac/2

dt

Page 22: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 82 Chapter 18: PWM Rectifiers

Integration of powers of sin θ over complete half-cycle

1π sinn(θ)dθ

0

π

=2π2⋅4⋅6 (n – 1)1⋅3⋅5 n if n is odd

1⋅3⋅5 (n – 1)2⋅4⋅6 n if n is even

n 1π sinn (θ)dθ

0

π

1 2π

2 12

3 43π

4 38

5 1615π

6 1548

Page 23: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 83 Chapter 18: PWM Rectifiers

Boost example: transistor RMS current

IQrms =VM

2Re1 – 8

3πVMV = Iac rms 1 – 8

3πVMV

Transistor RMS current is minimized by choosing V as small aspossible: V = VM. This leads to

IQrms = 0.39Iac rms

When the dc output voltage is not too much greater than the peak acinput voltage, the boost rectifier exhibits very low transistor current.Efficiency of the boost rectifier is then quite high, and 95% is typical ina 1kW application.

Page 24: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 84 Chapter 18: PWM Rectifiers

Table of rectifier current stresses for various topologies

Table 18. 3 Summary of rectifier current stresses for several converter topologies

rms Average Peak

CCM boostTransistor Iac rms 1 – 8

3πVMV

Iac rms2 2π 1 – π8

VMV

Iac rms 2

Diode Idc163π

VVM

Idc 2 IdcV

VM

Inductor Iac rms Iac rms2 2π Iac rms 2

CCM flyback, with n:1 isolation transformer and input filterTransistor,xfmr primary

Iac rms 1 + 83π

VMnV

Iac rms2 2π

Iac rms 2 1 + Vn

L1 Iac rms Iac rms2 2π Iac rms 2

C1 Iac rms83π

VMnV

0 Iac rms 2 max 1, VMnV

Diode,xfmr secondary

Idc32 +

163π

nVVM

Idc 2Idc 1 + nVVM

Page 25: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 85 Chapter 18: PWM Rectifiers

Table of rectifier current stressescontinued

CCM SEPIC, nonisolatedTransistor Iac rms 1 + 8

3πVMV

Iac rms2 2π Iac rms 2 1 + VM

V

L1 Iac rms Iac rms2 2π Iac rms 2

C1 Iac rms83π

VMV

0 Iac rms max 1, VMV

L2 Iac rmsVMV

32

Iac rms

2VMV

Iac rmsVMV 2

Diode Idc32 +

163π

VVM

Idc 2Idc 1 + VVM

CCM SEPIC, with n:1 isolation transformertransistor Iac rms 1 + 8

3πVMnV

Iac rms2 2π Iac rms 2 1 + VM

nV

L1 Iac rms Iac rms2 2π Iac rms 2

C1,xfmr primary

Iac rms83π

VMnV

0 Iac rms 2 max 1, n

Diode,xfmr secondary

Idc32 +

163π

nVVM

Idc 2Idc 1 + nVVM

with, in all cases, Iac rmsIdc

= 2 VVM

, ac input voltage = VM sin(ω t)

dc output voltage = V

Page 26: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 86 Chapter 18: PWM Rectifiers

Comparison of rectifier topologies

Boost converter

• Lowest transistor rms current, highest efficiency

• Isolated topologies are possible, with higher transistor stress

• No limiting of inrush current

• Output voltage must be greater than peak input voltage

Buck-boost, SEPIC, and Cuk converters

• Higher transistor rms current, lower efficiency

• Isolated topologies are possible, without increased transistorstress

• Inrush current limiting is possible

• Output voltage can be greater than or less than peak inputvoltage

Page 27: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 87 Chapter 18: PWM Rectifiers

Comparison of rectifier topologies

1kW, 240Vrms example. Output voltage: 380Vdc. Input current: 4.2Arms

Converter Transistor rmscurrent

Transistorvoltage

Diode rmscurrent

Transistor rmscurrent, 120V

Diode rmscurrent, 120V

Boost 2 A 380 V 3.6 A 6.6 A 5.1 A

NonisolatedSEPIC

5.5 A 719 V 4.85 A 9.8 A 6.1 A

IsolatedSEPIC

5.5 A 719 V 36.4 A 11.4 A 42.5 A

Isolated SEPIC example has 4:1 turns ratio, with 42V 23.8A dc load

Page 28: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 88 Chapter 18: PWM Rectifiers

18.6 Modeling losses and efficiencyin CCM high-quality rectifiers

Objective: extend procedure of Chapter 3, to predict the outputvoltage, duty cycle variations, and efficiency, of PWM CCM lowharmonic rectifiers.

Approach: Use the models developed in Chapter 3. Integrate overone ac line cycle to determine steady-state waveforms and averagepower.

Boost example

+– Q1

L

C R

+

v(t)

D1

vg(t)

ig(t) RL i(t)

+– R

+

v(t)

vg(t)

ig(t)RL i(t)

DRon

+ –

D' : 1VF

Dc-dc boost converter circuit Averaged dc model

Page 29: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 89 Chapter 18: PWM Rectifiers

Modeling the ac-dc boost rectifier

Rvac(t)

iac(t) +

vg(t)

ig(t)+

v(t)

id(t)

Q1

L

C

D1

controller

i(t)

RL

+– R

+

v(t) = V

vg(t)

ig(t)RL i(t) = I

d(t) Ron

+ –

d'(t) : 1VF id(t)

C(large)

Boostrectifiercircuit

Averagedmodel

Page 30: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 90 Chapter 18: PWM Rectifiers

Boost rectifier waveforms

0

2

4

6

8

10

0

100

200

300

vg(t)

vg(t)

ig(t)

ig(t)

0° 30° 60° 90° 120° 150° 180°

d(t)

0

0.2

0.4

0.6

0.8

1

0° 30° 60° 90° 120° 150° 180°

0

1

2

3

4

5

6

id(t)

i(t) = I

ωt0° 30° 60° 90° 120° 150° 180°

Typical waveforms(low frequency components)

ig(t) =vg(t)Re

Page 31: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 91 Chapter 18: PWM Rectifiers

Example: boost rectifierwith MOSFET on-resistance

+– R

+

v(t) = V

vg(t)

ig(t) i(t) = I

d(t) Ron

d'(t) : 1id(t)

C(large)

Averaged model

Inductor dynamics are neglected, a good approximation when the acline variations are slow compared to the converter natural frequencies

Page 32: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 92 Chapter 18: PWM Rectifiers

18.6.1 Expression for controller duty cycle d(t)

+– R

+

v(t) = V

vg(t)

ig(t) i(t) = I

d(t) Ron

d'(t) : 1id(t)

C(large)

Solve input side ofmodel:ig(t)d(t)Ron = vg(t) – d'(t)v

with ig(t) =vg(t)Re

eliminate ig(t):

vg(t)Re

d(t)Ron = vg(t) – d'(t)v

vg(t) = VM sin ωt

solve for d(t):

d(t) =v – vg(t)

v – vg(t)RonRe

Again, these expressions neglect converter dynamics, and assumethat the converter always operates in CCM.

Page 33: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 93 Chapter 18: PWM Rectifiers

18.6.2 Expression for the dc load current

+– R

+

v(t) = V

vg(t)

ig(t) i(t) = I

d(t) Ron

d'(t) : 1id(t)

C(large)

Solve output side ofmodel, using chargebalance on capacitor C:

I = id Tac

id(t) = d'(t)ig(t) = d'(t)vg(t)Re

Butd’(t) is:

d'(t) =vg(t) 1 –

RonRe

v – vg(t)RonRe

hence id(t) can be expressed as

id(t) =vg2(t)Re

1 – RonRe

v – vg(t)RonRe

Next, average id(t) over an ac line period, to find the dc load current I.

Page 34: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 94 Chapter 18: PWM Rectifiers

Dc load current I

I = id Tac= 2

Tac

V M2

Re

1 – RonRe

sin2 ωt

v – VM RonRe

sin ωtdt

0

Tac/2

Now substitute vg (t) = VM sin ωt, and integrate to find ⟨id(t)⟩Tac:

This can be written in the normalized form

I = 2Tac

V M2

VRe1 – Ron

Re

sin2 ωt1 – a sin ωt

dt0

Tac/2

with a = VMV

RonRe

Page 35: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 95 Chapter 18: PWM Rectifiers

Integration

By waveform symmetry, we need only integrate from 0 to Tac/4. Also,make the substitution θ = ωt:

I = V M2

VRe1 – Ron

Re

sin2 θ

1 – a sin θdθ

0

π/2

This integral is obtained not only in the boost rectifier, but also in thebuck-boost and other rectifier topologies. The solution is

sin2 θ

1 – a sin θdθ

0

π/2

= F(a) = 2a2π – 2a – π +

4 sin– 1 a + 2 cos– 1 a1 – a2

• Result is in closed form

• a is a measure of the lossresistance relative to Re

• a is typically much smaller thanunity

Page 36: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 96 Chapter 18: PWM Rectifiers

The integral F(a)

F(a)

a–0.15 –0.10 –0.05 0.00 0.05 0.10 0.15

0.85

0.9

0.95

1

1.05

1.1

1.15

sin2 θ

1 – a sin θdθ

0

π/2

= F(a) = 2a2π – 2a – π +

4 sin– 1 a + 2 cos– 1 a1 – a2

F(a) ≈ 1 + 0.862a + 0.78a2

Approximation viapolynomial:

For | a | ≤ 0.15, thisapproximate expression iswithin 0.1% of the exactvalue. If the a2 term isomitted, then the accuracydrops to ±2% for | a | ≤ 0.15.The accuracy of F(a)coincides with the accuracyof the rectifier efficiency η.

Page 37: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 97 Chapter 18: PWM Rectifiers

18.6.3 Solution for converter efficiency η

Converter average input power is

Pin = pin(t) Tac= V M

2

2Re

Average load power is

Pout = VI = V V M2

VRe1 – Ron

Re

F(a)2 with a = VM

VRonRe

So the efficiency is

η = PoutPin

= 1 – RonRe

F(a)

Polynomial approximation:

η ≈ 1 – RonRe

1 + 0.862 VMV

RonRe+ 0.78 VM

VRonRe

2

Page 38: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 98 Chapter 18: PWM Rectifiers

Boost rectifier efficiency

η = PoutPin

= 1 – RonRe

F(a)

0.0 0.2 0.4 0.6 0.8 1.00.75

0.8

0.85

0.9

0.95

1

VM /V

η

Ron/Re = 0.05

Ron/Re = 0.1

R on/R e =

0.15

R on/R e =

0.2

• To obtain highefficiency, choose Vslightly larger than VM

• Efficiencies in the range90% to 95% can then beobtained, even with Ronas high as 0.2Re

• Losses other thanMOSFET on-resistanceare not included here

Page 39: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 99 Chapter 18: PWM Rectifiers

18.6.4 Design example

Let us design for a given efficiency. Consider the followingspecifications:

Output voltage 390 VOutput power 500 Wrms input voltage 120 VEfficiency 95%

Assume that losses other than the MOSFET conduction loss arenegligible.

Average input power isPin =

Poutη = 500 W0.95 = 526 W

Then the emulated resistance is

Re =V g, rms2

Pin= (120 V)

2

526 W = 27.4Ω

Page 40: A complete 1ø system containing three feedback loops

Fundamentals of Power Electronics 100 Chapter 18: PWM Rectifiers

Design example

Also, VMV = 120 2 V390 V = 0.435

0.0 0.2 0.4 0.6 0.8 1.00.75

0.8

0.85

0.9

0.95

1

VM /V

η

Ron/Re = 0.05

Ron/Re = 0.1

R on/R e =

0.15

R on/R e =

0.2

95% efficiency withVM/V = 0.435 occurswith Ron/Re ≈ 0.075.

So we require aMOSFET with onresistance ofRon ≤ (0.075) Re

= (0.075) (27.4Ω) = 2 Ω