Development of Dual Power Multirotor System

Table 6

Larger-size quadrotor’s configuration for flight time simulation and result.

Battery capacity (Wh)	Battery weight (g)	AUW (g)	Battery resistance (ohm)	ESC internal resistance (ohm)	Battery specific energy (MJ/Kg)	Flight time (minute)
106.56	752	5407	0.0081	0.0025	0.5101	8.9
195.36	1376	6094	0.0044	0.0025	0.5111	13.8
296	2096	6886	0.0029	0.0025	0.5084	17.5
473.6	3344	8258	0.0018	0.0025	0.5099	21.5
592	4176	9174	0.0015	0.0025	0.5103	23
710.4	5008	10089	0.0012	0.0025	0.5107	24
947.2	6672	11919	0.0009	0.0025	0.5111	24.9
1302.4	9168	14665	0.0007	0.0025	0.5114	25