Study on the Application Scheme of Aerodynamic Coefficient Identification Based on the Differential Evolution Algorithm

<table class="table-group" id="tab2"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td class="align_left">State</td><td class="align_center">First scenario/second scenario</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">Launching elevation angle (degrees)</td><td class="align_center">42.7</td></tr><tr><td class="align_left">Launching azimuth angle (degrees)</td><td class="align_center">358.953</td></tr><tr><td class="align_left">Velocity (m/s)</td><td class="align_center">41.317</td></tr><tr><td class="align_left">Spin rate (rad/s)</td><td class="align_center">25.133</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Initial conditions for the two scenarios.</div>

Mathematical Problems in Engineering

tab2

Table 2

Table 2: Study on the Application Scheme of Aerodynamic Coefficient Identification Based on the Differential Evolution Algorithm 