Patent ID: 11878810
Assignee: THE BOEING COMPANY
Field: Transport (Mechanical engineering)
Classification: CPC B  F | IPC B  F

Claim 15:
16. The auxiliary power system of claim 15, wherein the BAT sensor suite includes a plurality of BAT magnitude sensors, wherein each BAT magnitude sensor of the plurality of BAT magnitude sensors is configured to generate a corresponding BAT magnitude sensor signal indicative of a corresponding BAT magnitude measurement, and further wherein the BAT signal is based, at least in part, on at least one corresponding BAT magnitude sensor signal of at least one BAT magnitude sensor of the plurality of BAT magnitude sensors, and further wherein the BAT signal is based, at least in part, on at least one of:
(i) an average of the corresponding BAT magnitude measurement from each BAT magnitude sensor of the plurality of BAT magnitude sensors;
(ii) a mean of the corresponding BAT magnitude measurement from each BAT magnitude sensor of the plurality of BAT magnitude sensors;
(iii) a median of the corresponding BAT magnitude measurement from each BAT magnitude sensor of the plurality of BAT magnitude sensors;
(iv) a minimum corresponding BAT magnitude measurement from the plurality of BAT magnitude sensors;
(v) a maximum corresponding BAT magnitude measurement from the plurality of BAT magnitude sensors; and
(vi) a linear combination of the corresponding BAT magnitude measurement from each BAT magnitude sensor of the plurality of BAT magnitude sensors.