public void bal(IntegralMeanings S, Coefficient C, Controls del, Statics s)
{
S.V_BAL = s.Vo;
S.Yg_BAL = s.Ho;
del.Tr_BAL = s.Tro;
C.y = (2 * s.G) / (s.S * s.PO_h * S.V_BAL * S.V_BAL);
S.ALPHA_BAL = i.ALPHA(C.y);
S.THETA_BAL = S.ALPHA_BAL;
del.e_rv_BAL = s.mzo + i.mz(S.ALPHA_BAL) * S.ALPHA_BAL;
}
/// <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 bal(IntegralMeanings S, Coefficient C, Controls del, Statics s)
{
S.V_BAL = s.Vo;
S.Yg_BAL = s.Ho;
del.Tr_BAL = s.Tro;
C.y = (2 * s.G) / (s.S * s.PO_h * S.V_BAL * S.V_BAL);
S.ALPHA_BAL = i.ALPHA(C.y);
S.THETA_BAL = S.ALPHA_BAL;
del.e_rv_BAL = s.mzo + i.mz(S.ALPHA_BAL) * S.ALPHA_BAL;
}
