/// <summary>
/// Initializes the trimming class
/// </summary>
/// <param name="fdmexec">a JSBSim executive object</param>
/// <param name="tm">trim mode</param>
public Trim(FDMExecutive exec, TrimMode tm)
{
N = Nsub = 0;
max_iterations = 60;
max_sub_iterations = 100;
Tolerance = 1E-3;
A_Tolerance = Tolerance / 10;
Debug = 0; DebugLevel = 0;
fdmex = exec;
fgic = fdmex.GetIC();
total_its = 0;
trimudot = true;
gamma_fallback = true;
axis_count = 0;
mode = tm;
xlo = xhi = alo = ahi = 0.0;
targetNlf = 1.0;
debug_axis = StateType.All;
SetMode(tm);
if (log.IsDebugEnabled)
{
log.Debug("Instantiated: FGTrim");
}
}
/// <summary>
/// Constructor
/// </summary>
/// <param name="exec">the parent executive object</param>
public State(FDMExecutive exec)
{
FDMExec = exec;
sim_time = 0.0;
dt = 1.0 / 120.0;
Bind();
}
/// <summary>
/// Constructor
/// </summary>
/// <param name="exec"></param>
public Force(FDMExecutive exec)
{
FDMExec = exec;
mT = Matrix3D.Identity;
vSense = Vector3D.Zero;
if (log.IsDebugEnabled)
{
log.Debug("Instantiated: Force.");
}
}
public TrimAxis(FDMExecutive exec,
InitialCondition ic,
StateType st,
ControlType ctrl)
{
fdmex = exec;
fgic = ic;
state = st;
control = ctrl;
max_iterations = 10;
control_value = 0;
its_to_stable_value = 0;
total_iterations = 0;
total_stability_iterations = 0;
state_convert = 1.0;
control_convert = 1.0;
state_value = 0;
state_target = 0;
switch (state)
{
case StateType.Udot: tolerance = DEFAULT_TOLERANCE; break;
case StateType.Vdot: tolerance = DEFAULT_TOLERANCE; break;
case StateType.Wdot: tolerance = DEFAULT_TOLERANCE; break;
case StateType.Qdot: tolerance = DEFAULT_TOLERANCE / 10; break;
case StateType.Pdot: tolerance = DEFAULT_TOLERANCE / 10; break;
case StateType.Rdot: tolerance = DEFAULT_TOLERANCE / 10; break;
case StateType.Hmgt: tolerance = 0.01; break;
case StateType.Nlf: state_target = 1.0; tolerance = 1E-5; break;
case StateType.All: break;
}
solver_eps = tolerance;
switch (control)
{
case ControlType.Throttle:
control_min = 0;
control_max = 1;
control_value = 0.5;
break;
case ControlType.Beta:
control_min = -30 * Constants.degtorad;
control_max = 30 * Constants.degtorad;
control_convert = Constants.radtodeg;
break;
case ControlType.Alpha:
control_min = fdmex.Aerodynamics.AlphaCLMin;
control_max = fdmex.Aerodynamics.AlphaCLMax;
if (control_max <= control_min)
{
control_max = 20 * Constants.degtorad;
control_min = -5 * Constants.degtorad;
}
control_value = (control_min + control_max) / 2;
control_convert = Constants.radtodeg;
solver_eps = tolerance / 100;
break;
case ControlType.PitchTrim:
case ControlType.Elevator:
case ControlType.RollTrim:
case ControlType.Aileron:
case ControlType.YawTrim:
case ControlType.Rudder:
control_min = -1;
control_max = 1;
state_convert = Constants.radtodeg;
solver_eps = tolerance / 100;
break;
case ControlType.AltAGL:
control_min = 0;
control_max = 30;
control_value = fdmex.Propagate.DistanceAGL;
solver_eps = tolerance / 100;
break;
case ControlType.Theta:
control_min = fdmex.Propagate.GetEuler().Theta - 5 * Constants.degtorad;
control_max = fdmex.Propagate.GetEuler().Theta + 5 * Constants.degtorad;
state_convert = Constants.radtodeg;
break;
case ControlType.Phi:
control_min = fdmex.Propagate.GetEuler().Phi - 30 * Constants.degtorad;
control_max = fdmex.Propagate.GetEuler().Phi + 30 * Constants.degtorad;
state_convert = Constants.radtodeg;
control_convert = Constants.radtodeg;
break;
case ControlType.Gamma:
solver_eps = tolerance / 100;
control_min = -80 * Constants.degtorad;
control_max = 80 * Constants.degtorad;
control_convert = Constants.radtodeg;
break;
case ControlType.Heading:
control_min = fdmex.Propagate.GetEuler().Psi - 30 * Constants.degtorad;
control_max = fdmex.Propagate.GetEuler().Psi + 30 * Constants.degtorad;
state_convert = Constants.radtodeg;
break;
}
}