The Nonlinear Single Controller of DGEN380 Aero Engine Design

<table class="table-group" id="tab4"><tr><td><table class="table"><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr class="thead"><td class="align_left">Power point</td><td class="align_center">Proportional gain</td><td class="align_center">Integral gain</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td class="align_left">Idle power</td><td class="align_center">29.77</td><td class="align_center">5.20</td></tr><tr><td class="align_left">Cruise power</td><td class="align_center">33.52</td><td class="align_center">5.58</td></tr><tr><td class="align_left">Climb power</td><td class="align_center">34.90</td><td class="align_center">6.86</td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>PI speed controller parameters.</div>

International Journal of Aerospace Engineering

tab4

Table 4

Table 4: The Nonlinear Single Controller of DGEN380 Aero Engine Design 