Development of Dual Power Multirotor System

Table 4

Small-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 (min)
13.32	96	605	0.0108	0.008	0.4995	4.8
24.42	174	691	0.0059	0.008	0.5052	7.6
33.3	237	760	0.0043	0.008	0.5058	9.4
44.4	315	846	0.0033	0.008	0.5074	11.1
49.95	354	889	0.0029	0.008	0.5080	11.9
55.5	393	932	0.0026	0.008	0.5084	12.5
66.6	471	1017	0.0022	0.008	0.5090	13.5