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KA3842A Datasheet, PDF (2/5 Pages) Wing Shing Computer Components – Linear Integrated Circuit(CURRENT-MODE PWM CONTROLLER)
KA3842A/KA3842AM
Electrical characteristics (*VCC=15V, RT=10kΩ, CT=3.3nF, TA=00C to +700C, unless
otherwise specified)
Characteristics
Reference Section
Reference Output Voltege
Line Regulation
Load Regulation
Short Circit Output Current
Oscillator Section
Oscillation Freguency
Frequency Change with
Voltage
Oscillator Amplitude
Error Amplifier Section
Input Bias Current
Input Voltage
Open Loop Voltage Gain
Power Supply Rejection Ratio
Output Sink Current
Output Source Current
High Output Voltage
Low Output Voltage
Current Sense Section
Gain
Maximum Input Signal
Power Supply Rejection Ratio
Input Bias Current
Output Section
Low Output Voltage
Symbol
VREF
∆VREF
∆VREF
ISC
f
∆f/∆VCCF
V(OSC)
IBIAS
VI(E.A)
GVO
PSRR
ISINK
ISOURCE
VOH
VOL
GV
VI(MAX)
PSRR
IBIAS
VOL
High Output Voltage
VOH
Rise Time
tR
Fall Time
tF
Under−Voltage Lockout Section
Start Theshold
VTH(ST)
Test Condition
TJ = 25°C, IREF = 1 mA
12V ≤ VCC ≤ 25 V
1 mA ≤ IREF ≤ 20mA
TA = 25°C
TJ = 25°C
12V ≤ VCC ≤ 25 V
V1 = 2.5V
2V ≤ V0 ≤ 4V
12V ≤ VCC ≤ 25 V
V2 = 2.7V, V1 = 1.1V
V2 = 2.3V, V1 = 5V
V2 = 2.3V, RL = 15KΩ to GND
V2 = 2.7V, RL = 15KΩ to PIN 8
(Note 1 & 2)
V1 = 5V (Note1)
12V ≤ VCC ≤ 25 V (Note 1)
ISINK = 20 mA
ISINK = 200 mA
ISINK = 20 mA
ISINK = 200 mA
TJ = 25°C, CL = 1nF (Note 3)
TJ = 25°C, CL = 1nF (Note 3)
Min
4.9
47
2.42
65
60
2
-0.5
5.0
2.85
0.9
13
12
14.5
Typ
5.0
6.0
6.0
-100
52
0.05
1.6
-0.1
2.5
90
70
7
-1.0
6.0
0.8
3.0
1.0
70
-3.0
0.08
1.4
13.5
13.0
45
35
16.0
Max
5.1
20
25
-180
57
1.0
-2
2.58
1.1
3.15
1.1
-10
0.4
2.2
Unit
V
mV
mA
KHz
%
Vp-p
µA
V
dB
mA
mA
V
V/V
V
dB
µA
V
150
nS
150
17.5
V
Min. Operating Voltage
(After Turn On)
PWM Section
Max. Duty Cycle
Min. Duty Cycle
Total Standby Current
Start−Up Current
VOPR(min)
D(MAX)
D(MAX)
IST
8.5
10
11.5
V
95
97
100
%
0
0.17
0.3
mA
Operating Supply Current
Zener Voltage
ICC (OPR)
VZ
V3 = V2 = 0V
14
17
30
38
V
* Adjust VCC above the start threshold before setting at 15V
Note 1: Parameter measured at trip point of lath with V2=0
Note 2: Gain defined as A=∆V1/∆V3 ; 0 ≤ V3 ≤ 0.8V
Note 3: These parameters, although guaranteed, are not 100% tested in production.
2