Research Article
Development of Dual Power Multirotor System
Table 5
Medium-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) |
| 24.42 | 174 | 1319 | 0.0066 | 0.008 | 0.5052 | 5.8 | 36.63 | 258 | 1412 | 0.0044 | 0.008 | 0.5111 | 7.8 | 46.62 | 330 | 1491 | 0.0035 | 0.008 | 0.5086 | 9.2 | 55.5 | 393 | 1560 | 0.0029 | 0.008 | 0.5084 | 10.2 | 88.8 | 627 | 1818 | 0.0018 | 0.008 | 0.5099 | 13 | 155.4 | 1095 | 2333 | 0.0012 | 0.008 | 0.5109 | 15.3 | 177.6 | 1251 | 2504 | 0.0011 | 0.008 | 0.5111 | 15.7 |
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