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IR3522 Datasheet(PDF) 11 Page - International Rectifier

Part # IR3522
Description  XPHASE3TM DDR & VTT CONTROL IC
PDF  32 Pages
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Manufacturer  IRF [International Rectifier]
Direct Link  http://www.irf.com
Logo IRF - International Rectifier

IR3522 Datasheet(HTML) 11 Page - International Rectifier

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IR3522
Page 11
V3.01
Figure 5 PWM Operating Waveforms
Lossless Average Inductor Current Sensing
Inductor current can be sensed by connecting a series RC network in parallel with the inductor and measuring the
voltage across the capacitor, as shown in Figure 6. The equation of this sensing network is,
(
)
.
1
1
)
(
1
1
)
(
)
(
CS
CS
L
L
L
CS
CS
L
C
C
sR
R
L
s
R
s
i
C
sR
s
v
s
v
+
+
=
+
=
Usually, the resistor Rcs and capacitor Ccs are chosen so that the RC time constant equals the time constant of the
inductor which is the inductance L divided by the inductor’s DCR (RL). If the two time constants match, the voltage
across Ccs is proportional to the current through L, and the sense circuit can be treated as if only a sense resistor
with the value of RL was used. The mismatch of the time constants does not affect the measurement of inductor DC
current, but affects the AC component of the inductor current.
Figure 6 Inductor Current Sensing and Current Sense Amplifier
The advantage of sensing the inductor current versus high side or low side sensing is that actual output current
being delivered to the load is obtained rather than peak or sampled information about the switch currents. The
output voltage can be positioned to meet a load line based on real time information. Except for a sense resistor in
series with the inductor, this is the only sense method that can support a single cycle transient response. Other
methods provide no information during either load increase (low side sensing) or load decrease (high side sensing).
CO
L
RL
RCS
CCS
VO
Current
Sense Amp
CSOUT
iL
vL
vCS
c
PHASE IC
CLOCK
PULSE
VDAC
EAIN
PWMRMP
GATEL
GATEH
DUTY CYCLE DECREASE
DUE TO VIN INCREASE
(FEED-FORWARD)
DUTY CYCLE INCREASE
DUE TO LOAD
INCREASE
STEADY-STATE
OPERATION
STEADY-STATE
OPERATION
DUTY CYCLE DECREASE DUE TO LOAD
DECREASE (BODY BRAKING) OR FAULT
(VCC UV, OCP, VID FAULT)



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