Research on Instability Boundaries of Control Force for Trajectory Correction Projectiles

<table class="fixed-width table-group" id="tab2"><tr><td><table class="table"><colgroup><col style="width:16.98em"/><col style="width:2.83em"/></colgroup><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td class="align_center" colspan="2">Aerodynamic coefficients</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">lift force coefficient</td><td class="align_center">1.7</td></tr><tr><td class="align_left">drag force coefficient</td><td class="align_center">0.13</td></tr><tr><td class="align_left">Magnus force coefficient derivative</td><td class="align_center">-1.5</td></tr><tr><td class="align_left">static moment coefficient derivative</td><td class="align_center">3.8</td></tr><tr><td class="align_left">Magnus moment coefficient derivative</td><td class="align_center">0.2</td></tr><tr><td class="align_left">damping moment coefficient derivative</td><td class="align_center">-8.0</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Aerodynamic coefficients of the example projectile.</div>

Mathematical Problems in Engineering

tab2

Table 2

Table 2: Research on Instability Boundaries of Control Force for Trajectory Correction Projectiles 