Airbus Top-of-Descent calculations with configuration
I have been trying to find whether or not the Airbus top of descent calculation takes into account any existing configuration .
This is only in a scenario with any slats or flaps locked and a flight which continues to its intended destination assuming a short flight
Please do not bother with the specifics as to why a flight would continue to its destination with any slats , flaps locked . I just need to know if the fmgs takes into account the existing configuration for calculating the top of descent