public void takeOff(DifferentialMeanings d, IntegralMeanings S, Forses F, Moments M, Controls del, Statics s)
{
d.Vx = (1 / s.m) * F.x;
d.BETA = (1 / (s.m * S.Vx)) * F.z + S.Wy;
d.Wy = 1 / s.Iyy * M.y;
d.X = S.Vx * cos(S.BETA);
d.Z = -S.Vx * sin(S.BETA);
S.Y = s.Cyo * S.q * s.S;
S.Q = s.Cxo * S.q * s.S;
F.x = 20 * del.Tr - S.Q - (s.G - S.Y) * (s.froll + s.fslip * (s.InhibitionL + s.InhibitionR));
F.z = F.zBETA * S.BETA + F.zDELn * del.n + F.zt;
F.zBETA = s.Cz_BETA * s.S * S.q;
F.zDELn = s.Cz_del_n * s.S * S.q;
F.zt = (s.G - S.Y) * s.Czk_BETA * (S.BETA + s.fW * del.fW);
M.y = M.yz + M.yWy + M.yp + M.yt;
M.yz = s.my_BETA * S.q * s.S * s.L * S.BETA + s.my_DELn * del.n;
M.yWy = s.my_Wy * S.q * s.S * s.L * d.Wy;
M.yp = 0; // = (P1 - P2) * s.Zengine
M.yt = (s.fW * s.XfrontWheel * del.fW + s.fslip * (s.G - S.Y) * (s.InhibitionL + s.InhibitionR) * (s.Zchassis / 2));
S.q = (s.PO_h * S.Vx * S.Vx / 2);
d.Xg = S.Vx * cos(S.BETA);
}
/// <summary>
/// Set initial conditions
/// </summary>
public void SetInitialConditions()
{
d = new DifferentialMeanings();
S = new IntegralMeanings();
F = new Forses();
M = new Moments();
C = new Coefficient();
c = new LinearizedCoefficient();
N = new Overload();
del = new Controls();
s = new Statics();
SetInitialValues();
if (stForm == null)
{ stForm = new StaticsForm(this, s); }
else if (stForm != null)
{
stForm.Close();
stForm = new StaticsForm(this, s);
}
if (fpForm == null)
{ fpForm = new FlyParamForm(this); }
else if (fpForm != null)
{
fpForm.Close();
fpForm = new FlyParamForm(this);
}
if (glForm == null)
{ glForm = new GraphicsListForm(this); }
else if (glForm != null)
{
glForm.Close();
glForm = new GraphicsListForm(this);
}
if (dgForm == null)
{ dgForm = new DataGridForm(this); }
else if (dgForm != null)
{
dgForm.Close();
dgForm = new DataGridForm(this);
}
if (avForm == null)
{ avForm = new AviatingForm(this); }
else if (avForm != null)
{
avForm.Close();
avForm = new AviatingForm(this);
}
if (pvForm == null)
{ pvForm = new PlaneVisualisationForm(this.toolStripButton6_Visualisation, S); }
else if (pvForm != null)
{
pvForm.Close();
pvForm = new PlaneVisualisationForm(this.toolStripButton6_Visualisation, S);
}
if (auForm == null)
{ auForm = new AutopilotForm(this); }
else if (auForm != null)
{
auForm.Close();
auForm = new AutopilotForm(this);
}
if (scrForm == null)
{ scrForm = new ScriptingAutopilotForm(this); }
else if (scrForm != null)
{
scrForm.Close();
scrForm = new ScriptingAutopilotForm(this);
}
}
public void takeOff(DifferentialMeanings d, IntegralMeanings S, Forses F, Moments M, Controls del, Statics s)
{
d.Vx = (1 / s.m) * F.x;
d.BETA = (1 / (s.m * S.Vx)) * F.z + S.Wy;
d.Wy = 1 / s.Iyy * M.y;
d.X = S.Vx * cos(S.BETA);
d.Z = -S.Vx * sin(S.BETA);
S.Y = s.Cyo * S.q * s.S;
S.Q = s.Cxo * S.q * s.S;
F.x = 20 * del.Tr - S.Q - (s.G - S.Y) * (s.froll + s.fslip * (s.InhibitionL + s.InhibitionR));
F.z = F.zBETA * S.BETA + F.zDELn * del.n + F.zt;
F.zBETA = s.Cz_BETA * s.S * S.q;
F.zDELn = s.Cz_del_n * s.S * S.q;
F.zt = (s.G - S.Y) * s.Czk_BETA * (S.BETA + s.fW * del.fW);
M.y = M.yz + M.yWy + M.yp + M.yt;
M.yz = s.my_BETA * S.q * s.S * s.L * S.BETA + s.my_DELn * del.n;
M.yWy = s.my_Wy * S.q * s.S * s.L * d.Wy;
M.yp = 0; // = (P1 - P2) * s.Zengine
M.yt = (s.fW * s.XfrontWheel * del.fW + s.fslip * (s.G - S.Y) * (s.InhibitionL + s.InhibitionR) * (s.Zchassis / 2));
S.q = (s.PO_h * S.Vx * S.Vx / 2);
d.Xg = S.Vx * cos(S.BETA);
}