Multirotor Sizing Methodology with Flight Time Estimation

<table class="table-group" id="tab4"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">Number of rotors</td><td class="align_center">4</td></tr><tr><td class="align_left">Diagonal size</td><td class="align_center">350 mm</td></tr><tr><td class="align_left">Total weight</td><td class="align_center">1375 g</td></tr><tr><td class="align_left">Battery weight</td><td class="align_center">468 g</td></tr><tr><td class="align_left">Battery capacity</td><td class="align_center">5870 mAh</td></tr><tr><td class="align_left">Battery nominal voltage</td><td class="align_center">15.2 V</td></tr><tr><td class="align_left">Battery type</td><td class="align_center">LiHV 4S</td></tr><tr><td class="align_left">Propeller diameter</td><td class="align_center">9 inch</td></tr><tr><td class="align_left">Propeller pitch</td><td class="align_center">5.5 inch</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Basic DJI Phantom 4 V2.0 parameters.</div>

Journal of Advanced Transportation

tab4

Table 4

Table 4: Multirotor Sizing Methodology with Flight Time Estimation 