8 Appendix 2: Step-by-Step Derivation of ACOT Loop Gain in S-Domain

The small-signal loop gain of the ACOT control loop can be written as:
Equation 8-1. 
G - ZB ZF · ZC ZLOAD ZC ZLOAD + ZL
Where:
  • ZB = ripple injection path impedance
  • ZF = feedback path impedance
  • ZC = output capacitor impedance
  • ZLOAD = load impedance
  • ZL = output inductor impedance
The ripple injection path consists of RINJ in series with CINJ. Therefore:
Equation 8-2. 
ZB = R INJ + 1 sC INJ
Rearranging:
Equation 8-3. 
ZB = 1 + sR INJ C INJ sC INJ
The feedback path impedance is formed by R1 in parallel with CFF. Therefore:
Equation 8-4. 
ZF = R 1 1 sC FF ZF = R 1 · 1 sC FF R 1 + 1 sC FF
Simplifying:
Equation 8-5. 
ZF = R 1 1 + sR 1 C FF
Substituting ZB and ZF:
Equation 8-6. 
ZB ZF = 1 + sR INJ C INJ sC INJ R 1 1 + sR 1 C FF
Therefore:
Equation 8-7. 
ZB ZF = 1 + sR INJ C INJ 1 + sR 1 C FF sC INJ R 1
The output capacitor impedance is:
Equation 8-8. 
ZC = 1 sC OUT
The load impedance is:
Equation 8-9. 
ZLOAD = R LOAD
Therefore:
Equation 8-10. 
ZC ZLOAD = 1 sC OUT · R LOAD 1 sC OUT + R LOAD
Simplifying:
Equation 8-11. 
ZC ZLOAD = R LOAD 1 + sR LOAD C OUT
The output inductor impedance is:
Equation 8-12. 
ZL = sL
The output stage gain is:
Equation 8-13. 
ZC ZLOAD ZC ZLOAD + ZL
Substituting the impedance expressions:
Equation 8-14. 
ZC ZLOAD ZC ZLOAD + ZL = R LOAD 1 + sR LOAD C OUT R LOAD 1 + sR LOAD C OUT + sL
Multiplying numerator and denominator by (1 + sRLOADCOUT):
Equation 8-15. 
= R LOAD R LOAD + sL 1 + sR LOAD C OUT
Expanding:
Equation 8-16. 
= R LOAD R LOAD + sL + s 2 LR LOAD C OUT
Dividing numerator and denominator by RLOAD:
Equation 8-17. 
= 1 1 + sL R LOAD + s 2 LC OUT
Starting from:
Equation 8-18. 
G - ZB ZF · ZC ZLOAD ZC ZLOAD + ZL
Substituting the derived expressions:
Equation 8-19. 
G s - ( 1 + sR INJ C INJ ) ( 1 + sR 1 C FF ) sC INJ R 1 · 1 1 + sL R LOAD + s 2 LC OUT
Therefore, the ACOT loop gain is:
Equation 8-20. 
G s = - ( 1 + sR INJ C INJ ) ( 1 + sR 1 C FF ) sC INJ R 1 1 + sL R LOAD + s 2 LC OUT
The negative sign indicates the feedback polarity of the control loop. For gain magnitude analysis, the loop gain magnitude is commonly considered as:
Equation 8-21. 
| G ( s ) | = ( 1 + sR INJ C INJ ) ( 1 + sR 1 C FF ) sC INJ R 1 ( 1 + sL R LOAD + s 2 LC OUT )