Modelling and Simulation of Fuel Cell Dynamics for Electrical Energy Usage of Hercules Airplanes

<table class="table-group" id="tab3"><tr><td><table class="table"><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr class="thead"><td align="left">H<sub>2</sub> rate</td><td align="center">O<sub>2</sub> rate</td><td align="center">Constants</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td align="left">5.00</td><td align="center">2.17</td><td align="center"><span style="width: 21px;"><svg height="18.3125" id="M76" style="vertical-align:-5.73163pt" version="1.1" viewbox="0 0 21 18.3125" width="21" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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q12 68 2 83t-72 22l6 28h257l-7 -28q-62 -7 -76 -21.5t-27 -83.5l-32 -172q29 11 78 46q112 84 217 179q18 16 23.5 25.5t-1 14.5t-26.5 8l-30 4l5 28h249z" id="x1D43E"></path></g>
<g transform="matrix(.012,-0,0,-.012,13.25,15.188)"><path d="M570 304q0 -108 -87 -199q-40 -42 -94.5 -74t-105.5 -43q-41 0 -65 11l-29 -141q-9 -45 -1.5 -58t45.5 -16l26 -2l-5 -29l-241 -10l4 26q51 10 67.5 24t26.5 60l113 520q-54 -20 -89 -41l-7 26q38 28 105 53l11 49q20 25 77 58l8 -7l-17 -77q39 14 102 14q82 0 119 -36
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</svg></span></td></tr><tr><td align="left">0.5</td><td align="center">0.5</td><td align="center"><span style="width: 15.3125px;"><svg height="15.8375" id="M77" style="vertical-align:-3.39066pt" version="1.1" viewbox="0 0 15.3125 15.8375" width="15.3125" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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<g transform="matrix(.012,-0,0,-.012,11.388,15.637)"><path d="M244 607q0 -25 -15.5 -43t-37.5 -18q-19 0 -32 13t-13 35q0 21 15 41t39 20q20 0 32 -14t12 -34zM222 91q-29 -33 -79 -68t-75 -35q-13 0 -19 7.5t-6 31t10 65.5l62 253q5 26 -1 26q-21 0 -72 -43l-13 24q43 40 91 68t71 28q30 0 10 -78l-71 -274q-8 -30 3 -30
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</svg></span></td></tr><tr><td align="left">0</td><td align="center">0</td><td align="center"><span style="width: 18.674999px;"><svg height="15.8375" id="M78" style="vertical-align:-3.39066pt" version="1.1" viewbox="0 0 18.674999 15.8375" width="18.674999" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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h-35l1 26q39 4 76 13.5t58.5 17t27.5 7.5q16 0 9 -26zM387 375q-11 11 -38.5 20t-51.5 9q-45 0 -79 -23q-46 -32 -77.5 -107.5t-31.5 -143.5q0 -40 9.5 -58.5t23.5 -18.5q40 0 113.5 70t99.5 118z" id="x1D451"></path></g>
</svg></span></td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

Controller parameters for oxygen and hydrogen rate controllers.

The Scientific World Journal

tab3

Table 3

Table 3: Modelling and Simulation of Fuel Cell Dynamics for Electrical Energy Usage of Hercules Airplanes 