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LT1339C датащи(PDF) 12 Page - Linear Technology |
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LT1339C датащи(HTML) 12 Page - Linear Technology |
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12 / 20 page ![]() 12 LT1339 APPLICATIONS INFORMATION L VV V If V MIN OUT IN OUT OIN = () − () ()( )( ) ∆ where fO = operating frequency. Given an inductor value (L), the peak inductor current is the sum of the average inductor current (IAVG)and half the inductor ripple current ( ∆I), or: II VV V Lf V PK AVG OUT IN OUT OIN =+ () − () ()()( )( ) 2 The inductor core type is determined by peak current and efficiency requirements. The inductor core must with- stand peak current without saturating, and series winding resistance and core losses should be kept as small as is practical to maximize conversion efficiency. The LT1339 peak current limit threshold is 40% greater than the average current limit threshold. Slope compensa- tion effects reduce this margin as duty cycle increases. This margin must be maintained to prevent peak current limit from corrupting the programmed value for average current limit. Programming the peak ripple current to less than 15% of the desired average current limit value will assure porper operation of the average current limit feature through 90% duty cycle (see Slope Compensation section). Oscillator Synchronization The LT1339 oscillator generates a modified sawtooth waveform at the CT pin between low and high thresholds of about 0.8V (vl) and 2.5V (vh) respectively. The oscillator can be synchronized by driving a TTL level pulse into the SYNC pin. This inputs to a one-shot circuit that reduces the oscillator high threshold to 2V for about 200ns. The SYNC input signal should have minimum high/low times of ≥1µs. Slope Compensation Current mode switching regulators that operate with a duty cycle greater than 50% and have continuous inductor current can exhibit duty cycle instability. While a regulator will not be damaged and may even continue to function acceptably during this type of subharmonic oscillation, an irritating high-pitched squeal is usually produced. The criterion for current mode duty cycle instability is met when the increasing slope of the inductor ripple current is less than the decreasing slope, which is the case at duty cycles greater than 50%. This condition is illustrated in Figure 5a. The inductor ripple current starts at I1, at the beginning of each oscillator switch cycle. Current increases at a rate S1 until the current reaches the control trip level I2. The controller servo loop then disables the main switch (and enables the synchronous switch) and inductor current begins to decrease at a rate S2. If the current switch point (I2) is perturbed slightly and increased by ∆I, the cycle time ends such that the mini- mum current point is increased by a factor of (1 + S2/S1) to start the next cycle. On each successive cycle, this error is multiplied by a factor of S2/S1. Therefore, if S2/S1 is ≥ 1, the system is unstable. Subharmonic oscillations can be eliminated by augment- ing the increasing ripple current slope (S1) in the control loop. This is accomplished by adding an artificial ramp on the inductor current waveform internal to the IC (with a slope SX) as shown in Figure 5b. If the sum of the slopes S1 + SX is greater than S2, the condition for subharmonic oscillation no longer exists. For a buck converter, the required additional current waveform slope, or “Slope Compensation,” follows the relation: S V L DC X IN ≥ − () 21 0.8V 1339 F04 2V 2.5V (vl) SYNC VCT (vh) FREE RUN SYNCHRONIZED Figure 4. Free Run and Synchronized Oscillator Waveforms (at CT Pin) |
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