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3 synchronizer design considerations, 4 constraints on the boost stage, An374 – Cirrus Logic AN374 User Manual

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AN374

AN374REV2

17

4.3 Synchronizer Design Considerations

The synchronizer circuit drives an external MOSFET, which may be ground referenced depending on the topology.

Constraint 1: Non-isolated synchronizer circuit considerations
In the case of a non-isolated flyback, the secondary ground of the flyback can be referenced to the primary
ground thereby having the least expensive synchronous circuit solution consisting of the synchronous
MOSFET and the diode. The MOSFET is directly driven from the SYNC pin of the CS1630/31.
In the case of the buck topology, the outputs are referenced to link voltage and the following two options are
possible:
1. Level shifting the SYNC pin output to a higher voltage using an external BJT and a P-channel MOSFET

(see Figure 7).

2. Driving the synchronizer externally using flip-flop from the switching node or another winding off of the

buck converter.

4.4 Constraints on the Boost Stage

Constraint 1: Maximum power should be power at full AC sine wave
It is recommended to design the dimming curve such that the maximum output power is delivered to the load
at 100% brightness when the driver is behind the full AC sine wave.

Constraint 2: Power should be monotonically increasing
The output power in the driver should be close to monotonically increasing. If the available power from the
dimmer cut waveform at any conduction angle is smaller than the requested output power, then the link voltage
may not be in regulation at that conduction angle. In such a case, the peak currents on the boost inductor need
to be increased, and all design calculations mentioned in application note AN368 are no longer valid for that
particular design. Increasing peak currents may compromise EMI and efficiency.

R22

R21

R23

Q4

L3

CS1630 /31

FBAUX

GND

13

GD

FBSENSE

15

12

11

D3

V

B S T

C16

C15

D11

R27

Channel 1 LED
(White)

Channel 2 LED
(Red)

GND

R25

Q6

R26

SYNC

Q5

GND

Figure 7. Non-isolated Synchronizer Buck Series Output Model