Supposing I have a 700W back-up fuel pump in an aeroplane (my personal plane is a Cessna, but I am enquiring for friends who fly airliners)
Do you agree that the control of the pump motor (DC brushed motor) should not involve a dynamically complicated feedback loop. After all, all that is needed is to rotate the pump motor at 8000 rpm in order to pump the fuel at the required rate.
Therefore, would you agree that the control algorithm should be
1...Place 20V at the motor terminals and then 2000ms later read the motor speed...
2...If speed is greater than 8000 rpm then decrement the motor voltage (decrease motor speed)
3....If speed is less than 8000 rpm then increment the motor voltage (increase motor speed)
4....delay for 250ms
5...Go back to part 2.
Do you agree that this is all that is needed?...and that this could be done with an SMPS providing the motor voltage.....and by "Increment the motor voltage", all one does is increment the SMPS duty cycle.
Does this sound like the way forward?