A hybrid drive train for an aircraft, the hybrid drive train comprising a plurality of power sources, a plurality of power consumers and a plurality of drive elements, each of the drive element being associated with at least one of the power sources and at least one of the power consumers, the hybrid drive train comprising at least one calculator and databases accessible by the calculator, the calculator being configured to:
- acquire measurements of a plurality of power parameters of the hybrid drive train, at least two of the measurements being expressed according to different magnitudes,
- compare each of the measurements with at least one limitation threshold, determined respectively for each power parameter from a threshold database, so as to deduce therefrom at least one gross power margin for said power parameter,
- convert from a transformation database, the gross power margins of said power parameters into refined power margins expressed according to a same common magnitude,
- transpose from a yield database, the refined power margins into standardized power margins in at least one reference point, the yield database determining yields of transmission members between an acquisition point and a reference point,
- determine a source power margin, from the standardized power margins of the sources at the said reference point, and a consumer power margin, from the standardized power margins of the power consumers at said reference point, and
- determine the minimum power margin by selecting a lowest power margin between the consumer power margin and the source power margin at said reference point.