internal void Calc_dynamics(int lr, AirPlane ap, Vector3D dv, double k_q, double k_S)
{
d_fv.SetVec(0.0D, 0.0D, 0.0D);
d_tv.SetVec(0.0D, 0.0D, 0.0D);
if (type == 0)
{
return;
}
baseWingBlock.Calc_dynamics(lr, null, ap, dv, k_q, k_S);
d_cl = baseWingBlock.cl;
d_cdi = baseWingBlock.cdi;
Vector3D fv_base = new Vector3D(baseWingBlock.fv);
Vector3D tv_base = new Vector3D(baseWingBlock.tv);
baseWingBlock.Calc_dynamics(lr, this, ap, dv, k_q, k_S);
d_cl = (baseWingBlock.cl - d_cl);
d_cdi = (baseWingBlock.cdi - d_cdi);
d_fv = baseWingBlock.fv.Sub(fv_base);
d_tv = baseWingBlock.tv.Sub(tv_base);
}
internal void Calc_dynamics(AirPlane ap, Vector3D[] dv, double[] k_q, double[] k_S)
{
fv.SetVec(0.0D, 0.0D, 0.0D);
tv.SetVec(0.0D, 0.0D, 0.0D);
for (int lr = 0; lr < n_lr; lr++)
{
for (int i = 0; i < n_wing_block; i++)
{
WingPlane wpi = wp[i, lr];
if (wpi.flag != 0)
{
wpi.Calc_dynamics(lr, null, ap, dv[lr], k_q[lr], k_S[lr]);
fv = fv.Add(wpi.fv);
tv = tv.Add(wpi.tv);
}
}
}
}