public static dynamic GetTSObject(ControlPlane dynObject)
{
if (dynObject is null)
{
return(null);
}
return(dynObject.teklaObject);
}
private void ReadControlPlaneAllFType(ControlPlane cpR, ControlPlane cpL, bool flagMessage)
{
cpR.gamma_h = MathTool.DegToRad(ReadDblValue("gamma_H", flagMessage));
cpR.hc = ReadVector("HC", flagMessage);
if (cpR.type != 0)
{
cpL.gamma_h = cpR.gamma_h;
cpL.hc = cpR.hc;
}
}
// Use this for initialization
void Start()
{
planes = new ControlPlane();
// Register Global Message 1
GlobalSignal.GlobalMsg1 = MessageManager.CreatMessage();
MessageManager.RegisterHander(GlobalSignal.GlobalMsg1, this.simulateAndSave);
// Register Global Message 2
GlobalSignal.GlobalMsg2 = MessageManager.CreatMessage();
MessageManager.RegisterHander(GlobalSignal.GlobalMsg2, this.restartSimulation);
//GlobalSignal.LoadDataToTable ("/Results/iso", "txt", 0);
//GlobalSignal.SaveTableToFile ("testCorse.txt", 0);
}
static void Main(string[] args)
{
int THREADS = 2;
int OBJECTS = 2;
if (args.Length != 0)
{
for (int i = 0; i < args.Length; i++)
{
if (args[i] == "--threads")
{
i++;
if (int.Parse(args[i]) > THREADS)
{
THREADS = int.Parse(args[i]);
}
}
if (args[i] == "--objects")
{
i++;
OBJECTS = int.Parse(args[i]);
}
}
}
Console.WriteLine("Using {0} threads", THREADS);
Console.WriteLine("Creating {0} objects", OBJECTS);
Thread.Sleep(1000);
Random rand = new Random();
System.Collections.ArrayList objs = new System.Collections.ArrayList();
PhysicsSimulation m_Physics = new PhysicsSimulation(THREADS);
for (int i = 0; i < OBJECTS; i++)
{
Spheroid m_Spheroid = new Spheroid(
new Vector3(rand.Next(-100, 100), rand.Next(-100, 100), rand.Next(-100, 100)),
new Vector3(1, 1, 1),
rand.Next(1, 9));
objs.Add(m_Spheroid);
}
Console.SetCursorPosition(0, Console.CursorTop);
Console.Write(">");
ControlPlane control = new ControlPlane(objs, THREADS);
control.Start();
}
void Start()
{
image = GetComponent <Image>();
knobImage = transform.GetChild(0).gameObject.GetComponent <Image>();
ControlPlane control = ControlPlane.Get();
input = control.DigitalInputs[InputIndex];
if (LedIndex >= 0)
{
led = control.Leds[LedIndex];
}
else
{
knobImage.color = LedOffColor;
}
}
public double Get_max_k_stall_htail()
{
double ret = 0.0D;
int i;
for (i = 0; i < n_htail; i++)
{
Wing wg = htail[i];
for (int lr = 0; lr < wg.n_lr; lr++)
{
for (int j = 0; j < wg.n_wing_block; j++)
{
WingPlane wp = wg.wp[j, lr];
if (wp.k_stall <= ret)
{
continue;
}
ret = wp.k_stall;
}
}
}
for (i = 0; i < n_elevator; i++)
{
for (int lr_0 = 0; lr_0 <= 1; lr_0++)
{
ControlPlane cp = elevator[i, lr_0];
if (cp.type != 0)
{
WingPlane wp_1 = cp.baseWingBlock;
if (wp_1.k_stall <= ret)
{
continue;
}
ret = wp_1.k_stall;
}
}
}
return(ret);
}
// Constructor Function
public SizeAvatar(Mesh sized, Mesh templateLen, HumanBody template)
{
testList = new ArrayList();
templateBody = template;
sizedMesh = sized;
templateMesh = template.getMesh();
templateBone = template.getBones();
mRoot = template.getTransform();
templateLenMesh = templateLen;
measurement = new Dictionary <HumanSize, float> ();
initMeasurements = new float[(int)HumanSize.Undefined];
planes = new ControlPlane();
mLocalPosInBone0 = new Vector3[templateMesh.vertexCount];
mLocalPosInBone1 = new Vector3[templateMesh.vertexCount];
mLocalPosInBone2 = new Vector3[templateMesh.vertexCount];
mLocalPosInBone3 = new Vector3[templateMesh.vertexCount];
templateShoulderLPos = templateBody.boneInfo [HumanBone.L_Clavicle].localPosition;
templateShoulderRPos = templateBody.boneInfo [HumanBone.R_Clavicle].localPosition;
updateLocalPosInBones();
initMearsurement();
}
private void ReadControlPlaneFlapType(ControlPlane cpR, ControlPlane cpL, bool flagMessage)
{
String flap_type_name = ReadString("flap", flagMessage);
cpR.flap_type = 0;
cpL.flap_type = 0;
for (int i = 0; i < Flap.flap_type_name.Length; i++)
{
if (Flap.flap_type_name[i].Equals(flap_type_name))
{
cpR.flap_type = i;
}
}
cpR.cf_c = ReadDblValue("cf/c", flagMessage);
cpR.dCLmax = ReadDblValue("dCLmax", flagMessage);
if (cpR.type != 0)
{
cpL.flap_type = cpR.flap_type;
cpL.cf_c = cpR.cf_c;
cpL.dCLmax = cpR.dCLmax;
}
}
private void ReadControlPlane(Wing wg, ControlPlane cpR, ControlPlane cpL,
bool flagMessage)
{
cpR.type = 0;
cpL.type = 0;
String typeStr = ReadString("type", flagMessage);
if (typeStr.Equals("all_flying"))
{
cpR.type = 2;
}
else if (typeStr.Equals("tailing_edge"))
{
cpR.type = 1;
}
else if (typeStr.Equals("leading_edge"))
{
cpR.type = 1;
}
else
{
cpR.type = 0;
}
typeStr = ReadString("actuate_type", flagMessage);
if (typeStr.Equals("actuator_drive"))
{
cpR.actuate_type = 1;
}
else
{
cpR.actuate_type = 0;
}
if (wg.n_lr == 2)
{
cpL.type = cpR.type;
cpL.actuate_type = cpR.actuate_type;
}
ReadWingPlane(wg, cpR.baseWingBlock, cpL.baseWingBlock, flagMessage);
cpR.delta_max = MathTool.DegToRad(ReadDblValue("delta_max", flagMessage));
cpR.delta_min = MathTool.DegToRad(ReadDblValue("delta_min", flagMessage));
cpR.lamda_h = MathTool.DegToRad(ReadDblValue("lamda_H", flagMessage));
if (cpL.type != 0)
{
cpL.delta_max = cpR.delta_max;
cpL.delta_min = cpR.delta_min;
cpL.lamda_h = cpR.lamda_h;
}
if ((cpR.type == 1) || (cpR.type == 1))
{
ReadControlPlaneFlapType(cpR, cpL, flagMessage);
}
if (cpR.type == 2)
{
ReadControlPlaneAllFType(cpR, cpL, flagMessage);
}
if (cpR.actuate_type == 1)
{
cpR.t_move = ReadDblValue("t_moving", flagMessage);
if ((cpL.baseWingBlock != null) && (cpL.baseWingBlock.flag == 1))
{
cpL.t_move = cpR.t_move;
}
}
cpR.Init();
cpL.Init();
}
void Start()
{
led = ControlPlane.Get().Leds[Index];
image = GetComponent <Image>();
}
private void button1_Click(object sender, EventArgs e)
{
if (MyModel.GetConnectionStatus())
{
double off1 = Convert.ToDouble(textBox4.Text);
double off2 = Convert.ToDouble(textBox5.Text);
TransformationPlane currentPlane = MyModel.GetWorkPlaneHandler().GetCurrentTransformationPlane();
Picker piku = new Picker();
ArrayList info = new ArrayList();
info = new ArrayList {
"END_X", "END_Y", "END_Z", "START_X", "START_Y", "START_Z"
};
ArrayList info2 = new ArrayList();
info2 = new ArrayList {
"END_X", "END_Y", "END_Z", "START_X", "START_Y", "START_Z"
};
ModelObject part = new Beam();
ModelObject part2 = new Beam();
Hashtable p1 = new Hashtable();
Hashtable p2 = new Hashtable();
part = piku.PickObject(Picker.PickObjectEnum.PICK_ONE_PART);
part.GetDoubleReportProperties(info, ref p1);
double rotpart = (part as Part).Position.RotationOffset;
part2 = piku.PickObject(Picker.PickObjectEnum.PICK_ONE_PART);
part2.GetDoubleReportProperties(info2, ref p2);
double rotpart2 = (part2 as Part).Position.RotationOffset;
Point st1 = new Point(Convert.ToDouble(p1["START_X"]), Convert.ToDouble(p1["START_Y"]), Convert.ToDouble(p1["START_Z"]));
Point st2 = new Point(Convert.ToDouble(p2["END_X"]), Convert.ToDouble(p2["END_Y"]), Convert.ToDouble(p2["END_Z"]));
Point st3 = new Point(Convert.ToDouble(p1["END_X"]), Convert.ToDouble(p1["END_Y"]), Convert.ToDouble(p1["END_Z"]));
Point st4 = new Point(Convert.ToDouble(p2["START_X"]), Convert.ToDouble(p2["START_Y"]), Convert.ToDouble(p2["START_Z"]));
LineSegment l1 = new LineSegment(st1, st2);
LineSegment l3 = new LineSegment(st1, st3); Vector vl3 = l3.GetDirectionVector(); vl3.Normalize();
LineSegment l4 = new LineSegment(st2, st1);
LineSegment l5 = new LineSegment(st2, st4); Vector vl5 = l5.GetDirectionVector(); vl5.Normalize();
st1.Translate(vl3.X * (off1 / vl3.GetLength()), vl3.Y * (off1 / vl3.GetLength()), vl3.Z * (off1 / vl3.GetLength()));
st2.Translate(vl5.X * (off2 / vl5.GetLength()), vl5.Y * (off2 / vl5.GetLength()), vl5.Z * (off2 / vl5.GetLength()));
ControlLine cl1 = new ControlLine(l1, true);
cl1.Color = ControlLine.ControlLineColorEnum.YELLOW_RED;
//cl1.Insert();
CoordinateSystem cs1 = new CoordinateSystem();
cs1 = part.GetCoordinateSystem();
CoordinateSystem cs2 = new CoordinateSystem();
cs2 = part2.GetCoordinateSystem();
Tekla.Structures.Model.Plane pl1 = new Tekla.Structures.Model.Plane();
pl1.AxisX = cs1.AxisX;
pl1.AxisY = cs1.AxisY;
pl1.Origin = cs1.Origin;
Tekla.Structures.Model.Plane pl2 = new Tekla.Structures.Model.Plane();
pl2.AxisX = cs2.AxisX;
pl2.AxisY = cs2.AxisY;
pl2.Origin = cs2.Origin;
GeometricPlane gp1 = new GeometricPlane(cs1);
GeometricPlane gp2 = new GeometricPlane(cs2);
ControlPlane cp1 = new ControlPlane(pl1, true);
//cp1.Insert();
ControlPlane cp2 = new ControlPlane(pl2, true);
//cp2.Insert();
LineSegment l2 = Projection.LineSegmentToPlane(l1, gp1);
LineSegment l6 = Projection.LineSegmentToPlane(l4, gp2);
ControlLine cl2 = new ControlLine(l2, true);
ControlLine cl3 = new ControlLine(l6, true);
cl2.Color = ControlLine.ControlLineColorEnum.YELLOW_RED;
//cl2.Insert();
cl3.Color = ControlLine.ControlLineColorEnum.YELLOW_RED;
//cl3.Insert();
Part p3 = part as Part;
Solid sl1 = p3.GetSolid();
ArrayList al1 = sl1.Intersect(l2);
Point px = new Point(al1[1] as Point);
ControlPoint cpp1 = new ControlPoint(px);
//cpp1.Insert();
Part p4 = part2 as Part;
Solid sl2 = p4.GetSolid();
ArrayList al2 = sl2.Intersect(l6);
Point py = new Point(al2[1] as Point);
ControlPoint cpp4 = new ControlPoint(py);
//cpp4.Insert();
double distance = Distance.PointToLineSegment(st3, l2);
double distance1 = l3.Length();
double cos = distance / distance1;
double distance2 = Distance.PointToLineSegment(st4, l6);
double distance3 = l5.Length();
double cos1 = distance2 / distance3;
Point p10 = dlugosc(st1, st3, 4, cos, px);
ControlPoint cpp2 = new ControlPoint(p10);
//cpp2.Insert();
Point p20 = dlugosc(st2, st4, 4, cos1, py);
ControlPoint cpp5 = new ControlPoint(p20);
//cpp5.Insert();
Point p5 = new Point(l2.StartPoint);
Point p6 = new Point(l2.EndPoint);
Vector v1 = new Vector((p6.X - p5.X) / 10000, (p6.Y - p5.Y) / 10000, (p6.Z - p5.Z) / 10000);
double v1d = v1.GetLength();
double dlbl = Convert.ToDouble(textBox2.Text);
Point p11 = new Point(px);
p11.Translate(v1.X * (dlbl / v1d), v1.Y * (dlbl / v1d), v1.Z * (dlbl / v1d));
Point p12 = dlugosc(st1, st3, 4, cos, p11);
ControlPoint cpp3 = new ControlPoint(p12);
//cpp3.Insert();
Point p7 = new Point(l6.StartPoint);
Point p8 = new Point(l6.EndPoint);
Vector v2 = new Vector((p8.X - p7.X) / 10000, (p8.Y - p7.Y) / 10000, (p8.Z - p7.Z) / 10000);
double v2d = v2.GetLength();
double dlbl1 = Convert.ToDouble(textBox2.Text);
Point p21 = new Point(py);
p21.Translate(v2.X * (dlbl1 / v2d), v2.Y * (dlbl1 / v2d), v2.Z * (dlbl1 / v2d));
Point p22 = dlugosc(st2, st4, 4, cos1, p21);
ControlPoint cpp6 = new ControlPoint(p22);
//cpp6.Insert();
Beam blachast = CreateBlacha(p10, p12, rotpart, 0, textBox1.Text);
blachast.Insert();
int id1 = blachast.Identifier.ID;
Identifier id11 = new Identifier(id1);
MyModel.GetWorkPlaneHandler().SetCurrentTransformationPlane(setWorkPlane(st1, vl3, v1));
ModelObject blachast3 = MyModel.SelectModelObject(id11);
double rotblachast = (blachast3 as Beam).Position.RotationOffset;
MyModel.GetWorkPlaneHandler().SetCurrentTransformationPlane(currentPlane);
//textBox1.Text = Convert.ToString(rotblachast);
blachast.Position.RotationOffset = -rotblachast;
blachast.PartNumber.Prefix = "PL";
blachast.PartNumber.StartNumber = 1001;
blachast.Modify();
Beam blachast2 = CreateBlacha(p20, p22, rotpart2, 1, textBox1.Text);
blachast2.Insert();
int id2 = blachast2.Identifier.ID;
Identifier id12 = new Identifier(id2);
MyModel.GetWorkPlaneHandler().SetCurrentTransformationPlane(setWorkPlane(st2, vl5, v2));
ModelObject blachast4 = MyModel.SelectModelObject(id12);
double rotblachast2 = (blachast4 as Beam).Position.RotationOffset;
MyModel.GetWorkPlaneHandler().SetCurrentTransformationPlane(currentPlane);
blachast2.Position.RotationOffset = -rotblachast2;
blachast2.PartNumber.Prefix = "PL";
blachast2.PartNumber.StartNumber = 1001;
blachast2.Modify();
Point p15 = new Point(p12);
p15.Translate(v1.X * (-30 / v1d), v1.Y * (-30 / v1d), v1.Z * (-30 / v1d));
ControlPoint cpp7 = new ControlPoint(p15);
//cpp7.Insert();
Point p16 = new Point(p22);
p16.Translate(v2.X * (-30 / v2d), v2.Y * (-30 / v2d), v2.Z * (-30 / v2d));
ControlPoint cpp8 = new ControlPoint(p16);
//cpp8.Insert();
Vector v11516 = new Vector((p16.X - p15.X) / 10000, (p16.Y - p15.Y) / 10000, (p16.Z - p15.Z) / 10000);
Point p151 = new Point(p15); Point p152 = new Point(p15); Point p153 = new Point(p15);
Point p161 = new Point(p16); Point p162 = new Point(p16); Point p163 = new Point(p16);
p151.Translate(v11516.X * (-30 / v11516.GetLength()), v11516.Y * (-30 / v11516.GetLength()), v11516.Z * (-30 / v11516.GetLength()));
p152.Translate(v11516.X * (120 / v11516.GetLength()), v11516.Y * (120 / v11516.GetLength()), v11516.Z * (120 / v11516.GetLength()));
p153.Translate(v11516.X * (70 / v11516.GetLength()), v11516.Y * (70 / v11516.GetLength()), v11516.Z * (70 / v11516.GetLength()));
p161.Translate(v11516.X * (30 / v11516.GetLength()), v11516.Y * (30 / v11516.GetLength()), v11516.Z * (30 / v11516.GetLength()));
p162.Translate(v11516.X * (-120 / v11516.GetLength()), v11516.Y * (-120 / v11516.GetLength()), v11516.Z * (-120 / v11516.GetLength()));
p163.Translate(v11516.X * (-70 / v11516.GetLength()), v11516.Y * (-70 / v11516.GetLength()), v11516.Z * (-70 / v11516.GetLength()));
Beam BlSt1 = BlachaSt(p151, p152, 0);
BlSt1.Insert();
int id3 = BlSt1.Identifier.ID;
Identifier id13 = new Identifier(id3);
MyModel.GetWorkPlaneHandler().SetCurrentTransformationPlane(setWorkPlane(st1, vl3, v1));
ModelObject blachast5 = MyModel.SelectModelObject(id13);
double rot5 = (blachast5 as Beam).Position.RotationOffset;
MyModel.GetWorkPlaneHandler().SetCurrentTransformationPlane(currentPlane);
//textBox1.Text = Convert.ToString(rotblachast);
BlSt1.Position.RotationOffset = -rot5;
BlSt1.PartNumber.Prefix = "PL";
BlSt1.PartNumber.StartNumber = 1001;
BlSt1.Modify();
Beam BlSt2 = BlachaSt(p161, p162, 1);
BlSt2.Insert();
int id4 = BlSt2.Identifier.ID;
Identifier id14 = new Identifier(id4);
MyModel.GetWorkPlaneHandler().SetCurrentTransformationPlane(setWorkPlane(st2, vl5, v2));
ModelObject blachast6 = MyModel.SelectModelObject(id14);
double rot6 = (blachast6 as Beam).Position.RotationOffset;
MyModel.GetWorkPlaneHandler().SetCurrentTransformationPlane(currentPlane);
//textBox1.Text = Convert.ToString(rotblachast);
BlSt2.Position.RotationOffset = -rot6;
BlSt2.PartNumber.Prefix = "PL";
BlSt2.PartNumber.StartNumber = 1001;
BlSt2.Modify();
Beam St12 = CreateStezenie12(p153, p163);
St12.Insert();
int id5 = St12.Identifier.ID;
Identifier id15 = new Identifier(id5);
MyModel.GetWorkPlaneHandler().SetCurrentTransformationPlane(setWorkPlane(st1, vl3, v1));
ModelObject stezenie1 = MyModel.SelectModelObject(id15);
(stezenie1 as Beam).StartPointOffset.Dy = 4;
(stezenie1 as Part).PartNumber.Prefix = "Pr";
(stezenie1 as Part).PartNumber.StartNumber = 1001;
stezenie1.Modify();
MyModel.GetWorkPlaneHandler().SetCurrentTransformationPlane(currentPlane);
MyModel.GetWorkPlaneHandler().SetCurrentTransformationPlane(setWorkPlane(st2, vl5, v2));
ModelObject stezenie2 = MyModel.SelectModelObject(id15);
(stezenie2 as Beam).EndPointOffset.Dy = -6;
(stezenie2 as Part).PartNumber.Prefix = "Pr";
(stezenie2 as Part).PartNumber.StartNumber = 1001;
stezenie2.Modify();
MyModel.GetWorkPlaneHandler().SetCurrentTransformationPlane(currentPlane);
double split = Convert.ToDouble(textBox3.Text);
Point pointsplit = new Point(p163);
pointsplit.Translate(v11516.X * (-split / v11516.GetLength()), v11516.Y * (-split / v11516.GetLength()), v11516.Z * (-split / v11516.GetLength()));
BoltArray b1 = sruby(p151, p152, BlSt1, blachast);
b1.Insert();
int id6 = b1.Identifier.ID;
Identifier id16 = new Identifier(id6);
MyModel.GetWorkPlaneHandler().SetCurrentTransformationPlane(setWorkPlane(st1, vl3, v1));
ModelObject b1m = MyModel.SelectModelObject(id16);
(b1m as BoltArray).Position.RotationOffset = 0;
(b1m as BoltArray).BoltStandard = "4017-8.8";
(b1m as BoltArray).ExtraLength = 5;
b1m.Modify();
MyModel.GetWorkPlaneHandler().SetCurrentTransformationPlane(currentPlane);
BoltArray b2 = sruby(p161, p162, BlSt2, blachast2);
b2.Insert();
int id7 = b2.Identifier.ID;
Identifier id17 = new Identifier(id7);
MyModel.GetWorkPlaneHandler().SetCurrentTransformationPlane(setWorkPlane(st2, vl5, v2));
ModelObject b2m = MyModel.SelectModelObject(id17);
(b2m as BoltArray).Position.RotationOffset = 180;
b2m.Modify();
MyModel.GetWorkPlaneHandler().SetCurrentTransformationPlane(currentPlane);
Weld w = new Weld();
Weld w2 = new Weld();
Weld w3 = new Weld();
Weld w4 = new Weld();
w.MainObject = stezenie2;
w.SecondaryObject = BlSt1;
w.ShopWeld = true;
w.Insert();
w2.MainObject = stezenie2;
w2.SecondaryObject = BlSt2;
w2.ShopWeld = true;
w2.Insert();
w3.MainObject = part;
w3.SecondaryObject = blachast;
w3.ShopWeld = true;
w3.Insert();
w4.MainObject = part2;
w4.SecondaryObject = blachast2;
w4.ShopWeld = true;
w4.Insert();
Beam st122 = Operation.Split(stezenie2 as Beam, pointsplit);
Connection sr = new Connection();
sr.Name = "Połączenie śrubą rzymską";
sr.Number = 126;
sr.LoadAttributesFromFile("82269_M12");
sr.SetPrimaryObject(stezenie2);
sr.SetSecondaryObject(st122);
sr.Insert();
}
MyModel.CommitChanges();
}
public void ControlLink(double dt)
{
int i;
for (i = 0; i < n_elevator; i++)
{
if (elevator[i, 0].type != 0)
{
ControlPlane ele = elevator[i, 0];
ele.delta = ((1.0D - cif.stick_pos_y) / 2.0D * (ele.delta_max - ele.delta_min) + ele.delta_min);
}
if (elevator[i, 1].type != 0)
{
elevator[i, 1].delta = elevator[i, 0].delta;
}
}
for (i = 0; i < n_canard_elevator; i++)
{
if (canard_elevator[i, 0].type != 0)
{
if (cif.stick_pos_y > 0.0D)
{
canard_elevator[i, 0].delta = (cif.stick_pos_y * canard_elevator[i, 0].delta_min);
}
else
{
canard_elevator[i, 0].delta = (-cif.stick_pos_y * canard_elevator[i, 0].delta_max);
}
}
if (canard_elevator[i, 1].type != 0)
{
canard_elevator[i, 1].delta = canard_elevator[i, 0].delta;
}
}
for (i = 0; i < n_aileron; i++)
{
if (aileron[i, 0].type != 0)
{
if (cif.stick_pos_x >= 0.0D)
{
aileron[i, 0].delta = (cif.stick_pos_x * aileron[i, 0].delta_min);
}
else
{
aileron[i, 0].delta = (-cif.stick_pos_x * aileron[i, 0].delta_max);
}
}
if (aileron[i, 1].type != 0)
{
if (cif.stick_pos_x >= 0.0D)
{
aileron[i, 1].delta = (cif.stick_pos_x * aileron[i, 1].delta_max);
}
else
{
aileron[i, 1].delta = (-cif.stick_pos_x * aileron[i, 1].delta_min);
}
}
}
for (i = 0; i < n_rudder; i++)
{
if (rudder[i, 0].type != 0)
{
if (cif.rudder_pos > 0.0D)
{
rudder[i, 0].delta = (-cif.frudder_pos.output * rudder[i, 0].delta_min);
}
else
{
rudder[i, 0].delta = (cif.frudder_pos.output * rudder[i, 0].delta_max);
}
}
if (rudder[i, 1].type != 0)
{
rudder[i, 1].delta = rudder[i, 1].delta;
}
}
for (i = 0; i < n_LandingGear; i++)
{
if (landing_gear[i, 0].flag != 0)
{
landing_gear[i, 0].brake = cif.brakeRight_pos;
}
if (landing_gear[i, 1].flag != 0)
{
landing_gear[i, 1].brake = cif.brakeLeft_pos;
}
}
for (i = 0; i < n_t_flap; i++)
{
t_flap[i, 0].Update(cif.flap_sw, dt);
t_flap[i, 1].delta = t_flap[i, 0].delta;
}
for (i = 0; i < n_powerPlant; i++)
{
powerPlant[i].throttle = (1.0D - System.Math.Cos(cif.throttle_pos * Math.PI * 0.5D));
}
}
public double Get_max_k_stall_wing()
{
double ret = 0.0D;
int i;
for (i = 0; i < n_wing; i++)
{
Wing wg = wing[i];
for (int lr = 0; lr < wg.n_lr; lr++)
{
for (int j = 0; j < wg.n_wing_block; j++)
{
WingPlane wp = wg.wp[j, lr];
if (wp.k_stall <= ret)
{
continue;
}
ret = wp.k_stall;
}
}
}
for (i = 0; i < n_aileron; i++)
{
for (int lr_0 = 0; lr_0 <= 1; lr_0++)
{
ControlPlane cp = aileron[i, lr_0];
if (cp.type != 0)
{
WingPlane wp_1 = cp.baseWingBlock;
if (wp_1.k_stall <= ret)
{
continue;
}
ret = wp_1.k_stall;
}
}
}
for (i = 0; i < n_t_flap; i++)
{
for (int lr_2 = 0; lr_2 <= 1; lr_2++)
{
ControlPlane cp_3 = t_flap[i, lr_2];
if (cp_3.type != 0)
{
WingPlane wp_4 = cp_3.baseWingBlock;
if (wp_4.k_stall <= ret)
{
continue;
}
ret = wp_4.k_stall;
}
}
}
for (i = 0; i < n_l_flap; i++)
{
for (int lr_5 = 0; lr_5 <= 1; lr_5++)
{
ControlPlane cp_6 = l_flap[i, lr_5];
if (cp_6.type != 0)
{
WingPlane wp_7 = cp_6.baseWingBlock;
if (wp_7.k_stall <= ret)
{
continue;
}
ret = wp_7.k_stall;
}
}
}
return(ret);
}
public void MakeObject()
{
int i;
for (i = 0; i < 7; i++)
{
for (int lr = 0; lr <= 1; lr++)
{
fuslage[i, lr] = new Fuselage();
}
}
for (i = 0; i < 1; i++)
{
wing[i] = new Wing();
}
for (i = 0; i < 1; i++)
{
htail[i] = new Wing();
}
for (i = 0; i < 1; i++)
{
vtail[i] = new Wing();
}
for (i = 0; i < 1; i++)
{
canard[i] = new Wing();
}
for (i = 0; i < 5; i++)
{
fin[i] = new Wing();
}
for (i = 0; i < 1; i++)
{
for (int lr_0 = 0; lr_0 <= 1; lr_0++)
{
elevator[i, lr_0] = new ControlPlane();
}
}
for (i = 0; i < 1; i++)
{
for (int lr_1 = 0; lr_1 <= 1; lr_1++)
{
aileron[i, lr_1] = new ControlPlane();
}
}
for (i = 0; i < 1; i++)
{
for (int lr_2 = 0; lr_2 <= 1; lr_2++)
{
rudder[i, lr_2] = new ControlPlane();
}
}
for (i = 0; i < 1; i++)
{
for (int lr_3 = 0; lr_3 <= 1; lr_3++)
{
t_flap[i, lr_3] = new ControlPlane();
}
}
for (i = 0; i < 1; i++)
{
for (int lr_4 = 0; lr_4 <= 1; lr_4++)
{
l_flap[i, lr_4] = new ControlPlane();
}
}
for (i = 0; i < 1; i++)
{
for (int lr_5 = 0; lr_5 <= 1; lr_5++)
{
canard_elevator[i, lr_5] = new ControlPlane();
}
}
for (i = 0; i < 3; i++)
{
for (int lr_6 = 0; lr_6 <= 1; lr_6++)
{
landing_gear[i, lr_6] = new LandingGear();
}
}
}
public Led(ControlPlane control, byte index)
{
this.control = control;
this.Index = index;
}
public void DrawInstrument(Graphics g, AirPlane ap, SimulatorInterface simif, double dt)
{
Matrix44 tmat = new Matrix44();
Matrix44 smat = new Matrix44();
Matrix44 rmat = new Matrix44();
Matrix44 rzmat = new Matrix44();
Matrix44 rxmat = new Matrix44();
Matrix44 mat = new Matrix44();
Scine scine = new Scine();
//g.SetColor(informationColor);
//g.SetFont(stdFont);
SolidBrush informationBrush = new SolidBrush(informationColor);
Pen informationPen = new Pen(informationColor);
g.DrawString(ap.plane.name, stdFont, informationBrush, 300 - ap.plane.name.Length * 3, 365);
if (simif.dispInformationSw == 1)
{
double x = ap.pMotion.ov.Length();
//g.DrawString("V: " + Jp.Maker1.Util.DispFormat.DoubleFormat(x, 3, 1) + " m/s", v_true_x, v_true_y);
//g.DrawString("V: " + Jp.Maker1.Util.DispFormat.DoubleFormat(Jp.Maker1.Sim.Tools.UnitConvert.Mps2kmph(x), 3, 1) + " km/h", v_true_x, v_true_y + 12);
//g.DrawString("V: " + Jp.Maker1.Util.DispFormat.DoubleFormat(Jp.Maker1.Sim.Tools.UnitConvert.Mps2kt(x), 3, 1) + " kt", v_true_x, v_true_y + 24);
x = ap.pMotion.wpos.y;
//g.DrawString("ALT: " + Jp.Maker1.Util.DispFormat.DoubleFormat(x, 5, 1) + " m", alt_x, alt_y);
//g.DrawString("ALT: " + Jp.Maker1.Util.DispFormat.DoubleFormat(Jp.Maker1.Sim.Tools.UnitConvert.M2ft(x), 5, 1) + " ft", alt_x, alt_y + 12);
}
double pitch = ap.pMotion.pitch.GetValue();
double roll = ap.pMotion.roll.GetValue();
g.DrawString("PIT: " + DispFormat.DoubleFormat(MathTool.RadToDeg(pitch), 5, 1) + " deg", stdFont, informationBrush, 515, 12);
g.DrawString("ROL: " + DispFormat.DoubleFormat(MathTool.RadToDeg(roll), 5, 1) + " deg", stdFont, informationBrush, 512, 89);
tmat.SetTMat(550.0D, 45.0D, 0.0D);
smat.SetSMat(30.0D, -30.0D, 0.0D);
if ((roll > 1.570796326794897D) || (roll < -1.570796326794897D))
{
rmat.SetRzMat(Math.PI - pitch);
}
else
{
rmat.SetRzMat(pitch);
}
mat = smat.MultMat(rmat).MultMat(tmat);
scine.Add(pitch_miniature_aircraft.Transform(mat));
g.DrawEllipse(informationPen, 520, 15, 60, 60);
tmat.SetTMat(550.0D, 121.0D, 0.0D);
smat.SetSMat(30.0D, -30.0D, 0.0D);
rmat.SetRzMat(-roll);
mat = smat.MultMat(rmat).MultMat(tmat);
scine.Add(roll_miniature_aircraft.Transform(mat));
g.DrawEllipse(informationPen, 520, 91, 60, 60);
if (simif.dispInformationSw == 1)
{
double x_0 = ap.atmos.h;
//g.DrawString("H': " + Jp.Maker1.Util.DispFormat.DoubleFormat(x_0, 5, 1) + " m'", atmo_x, atmo_y);
x_0 = ap.atmos.tc;
//g.DrawString("t: " + Jp.Maker1.Util.DispFormat.DoubleFormat(x_0, 4, 1) + " ��", atmo_x, atmo_y + 12);
x_0 = ap.atmos.t;
//g.DrawString("T: " + Jp.Maker1.Util.DispFormat.DoubleFormat(x_0, 4, 1) + " K", atmo_x, atmo_y + 24);
x_0 = ap.atmos.p;
//g.DrawString("p: " + Jp.Maker1.Util.DispFormat.DoubleFormat(x_0 / 100.0D, 4, 1) + " hPa", atmo_x + 90, atmo_y);
x_0 = ap.atmos.rho;
//g.DrawString("��: " + Jp.Maker1.Util.DispFormat.DoubleFormat(x_0, 1, 3) + " kg/m3", atmo_x + 90, atmo_y + 12);
x_0 = ap.atmos.a;
// g.DrawString("a: " + Jp.Maker1.Util.DispFormat.DoubleFormat(x_0, 3, 1) + " m/sec", atmo_x + 90, atmo_y + 24);
}
double alpha = ap.pMotion.alpha;
double beta = ap.pMotion.beta;
if (simif.dispInformationSw == 1)
{
//g.DrawString("��: " + Jp.Maker1.Util.DispFormat.DoubleFormat(Jp.Maker1.Util.MathTool.RadToDeg(alpha), 3, 1) + " deg", 2, 60);
// g.DrawString("��: " + Jp.Maker1.Util.DispFormat.DoubleFormat(Jp.Maker1.Util.MathTool.RadToDeg(beta), 3, 1) + " deg", 2, 72);
}
Vector3D vec = ap.pMotion.ov.SclProd(60000000.0D).MultMat(ap.pilot.ViewMatrix());
if ((vec != null) && (vec.z > 0.0D))
{
vec = proj.Project(vec);
tmat.SetTMat(vec.x, vec.y, vec.z);
scine.Add(velocity_vector.Transform(tmat));
}
vec.SetVec(0.0D, 0.0D, 60000000.0D);
vec = vec.MultMat(ap.pilot.ViewMatrix());
if ((vec != null) && (vec.z > 0.0D))
{
vec = proj.Project(vec);
tmat.SetTMat(vec.x, vec.y, vec.z);
scine.Add(front_point.Transform(tmat));
}
vec = ap.pMotion.force.R2l().SclProd(-1.0D / ap.inp.m);
vec.z = 0.0D;
double x_1 = vec.Length();
Vector3D vec2 = vec.NmlVec().SclProd(50.0D);
vec = vec.NmlVec().SclProd(100.0D);
Vector3D vec3 = vec.NmlVec().SclProd(113.0D);
Jp.Maker1.Util.Symbol.DrawArrow(g, 300 + (int)vec2.x, 200 - (int)vec2.y, 300 + (int)vec.x, 200 - (int)vec.y, 50.0D, x_1 * 4.0D);
//g.DrawString(Jp.Maker1.Util.DispFormat.DoubleFormat(x_1 / 9.80655D, 2) + "G", 286 + (int)vec3.x, 200 - (int)vec3.y);
vec = ap.pMotion.force.R2l().SclProd(-1.0D / ap.inp.m);
x_1 = vec.z;
// g.DrawString(Jp.Maker1.Util.DispFormat.DoubleFormat(x_1 / 9.80655D, 2) + "G", 120, 192);
if (Math.Abs((int)(x_1 * 10.0D)) >= 1)
{
Jp.Maker1.Util.Symbol.DrawArrow(g, 150, 200, 150 + (int)(x_1 * 10.0D), 200, (int)(Math.Abs(x_1) * 10.0D), 10.0D);
Jp.Maker1.Util.Symbol.DrawArrow(g, 450, 200, 450 - (int)(x_1 * 10.0D), 200, (int)(Math.Abs(x_1) * 10.0D), 10.0D);
}
int xx = 2;
int yy = 100;
vec = ap.pMotion.force.SclProd(-1.0D / ap.inp.m / 9.80655D);
if (simif.dispInformationSw == 1)
{
//g.DrawString("Gx: " + Jp.Maker1.Util.DispFormat.DoubleFormat(vec.x, 2, 4) + " [G]", xx, yy);
yy += 11;
// g.DrawString("Gy: " + Jp.Maker1.Util.DispFormat.DoubleFormat(vec.y, 2, 4) + " [G]", xx, yy);
yy += 11;
//g.DrawString("Gz: " + Jp.Maker1.Util.DispFormat.DoubleFormat(vec.z, 2, 4) + " [G]", xx, yy);
yy += 11;
}
if (ap.max_k_stall_wing > 1.0D)
{
//g.DrawString("STALL", stallAlert_x + 25, stallAlert_y);
}
else if (ap.max_k_stall_wing > 0.95D)
{
//g.DrawString("STALL WARNING", stallAlert_x, stallAlert_y);
}
//g.SetColor(instrumentColor);
double yaw = ap.pMotion.yaw.GetValue();
//g.DrawString("HDG: " + Jp.Maker1.Util.DispFormat.DoubleFormat(Jp.Maker1.Util.MathTool.RadToDeg(yaw), 5, 1) + " deg", 512, 165);
tmat.SetTMat(550.0D, 197.0D, 0.0D);
smat.SetSMat(30.0D, 30.0D, 0.0D);
rmat.SetRzMat(yaw);
mat = smat.MultMat(rmat).MultMat(tmat);
scine.Add(heading_miniature_aircraft.Transform(mat));
// g.DrawOval(520, 167, 60, 60);
rzmat.SetRzMat(-ap.pMotion.roll.GetValue());
rxmat.SetRxMat(-ap.pMotion.pitch.GetValue());
mat = rxmat.MultMat(rzmat);
Scine scine2 = new Scine();
scine2.Add(artificial_horizon.Transform(mat.MultMat(ap.pilot.ViewMatrix())));
Scine view = new Scine();
view = scine2.MakeView(clip, proj, false);
view.Draw(g);
// g.SetFont(bigFont);
x_1 = ap.pMotion.vc.Length() * Math.Sqrt(ap.atmos.rho / 1.225D);
// g.DrawString("ASI: " + Jp.Maker1.Util.DispFormat.DoubleFormat(Jp.Maker1.Sim.Tools.UnitConvert.Mps2kt(x_1), 3, 0) + " kt", 190, 380);
x_1 = ap.pMotion.wpos.y;
//g.DrawString("ALT: " + Jp.Maker1.Util.DispFormat.DoubleFormat(Jp.Maker1.Sim.Tools.UnitConvert.M2ft(x_1), 5, 0) + " ft", 190, 396);
x_1 = ap.pMotion.wv.y;
//g.DrawString("VSI: " + Jp.Maker1.Util.DispFormat.DoubleFormat(Jp.Maker1.Sim.Tools.UnitConvert.M2ft(x_1) * 60.0D, 5, 0) + " fpm", 305, 380);
x_1 = ap.pMotion.omega.z;
// g.DrawString("YRT: " + Jp.Maker1.Util.DispFormat.DoubleFormat(Jp.Maker1.Util.MathTool.RadToDeg(x_1) * 60.0D, 3, 0) + " deg/m", 305, 396);
for (int i = 0; i < ap.n_LandingGear; i++)
{
if (ap.landing_gear[i, 1].flag == 1)
{
xx = gear_x;
}
else
{
xx = gear_x - gear_box_maegine / 2;
}
yy = gear_y + i * gear_box_maegine * 3;
for (int lr = 0; lr <= 1; lr++)
{
if (ap.landing_gear[i, lr].flag == 1)
{
int xx1;
if (lr == 0)
{
xx1 = xx + gear_box_maegine;
}
else
{
xx1 = xx;
}
x_1 = ap.landing_gear[i, lr].delta;
if (x_1 == 0.0D)
{
//g.SetColor(instrumentRed);
//g.FillRect(xx1 + 2, yy + 2, gear_box_size - 3, gear_box_size - 3);
}
else if (x_1 == 1.0D)
{
//g.SetColor(instrumentGreen);
//g.FillRect(xx1 + 2, yy + 2 + gear_box_maegine * 2, gear_box_size - 3, gear_box_size - 3);
}
else
{
// g.SetColor(instrumentYellow);
// g.FillRect(xx1 + 2, yy + 2 + gear_box_maegine, gear_box_size - 3, gear_box_size - 3);
}
//g.SetColor(instrumentColor);
//g.DrawRect(xx1, yy, gear_box_size, gear_box_size);
//g.DrawRect(xx1, yy + gear_box_maegine, gear_box_size, gear_box_size);
//g.DrawRect(xx1, yy + gear_box_maegine * 2, gear_box_size, gear_box_size);
}
}
}
//g.SetFont(smallFont);
ControlPlane flap = ap.t_flap[0, 0];
if (ap.t_flap[0, 0].type != 0)
{
xx = flap_x;
yy = flap_y;
// g.DrawRect(xx, yy - flap_width, 10, flap_width);
for (double ang = 0.0D; ang < MathTool.RadToDeg(flap.delta_max) + 0.1D; ang += 10.0D)
{
x_1 = (MathTool.DegToRad(ang) - flap.delta_min) / (flap.delta_max - flap.delta_min);
int yy1 = yy - flap_width + (int)(flap_width * x_1 + 0.5D);
// g.DrawLine(xx + 10, yy1, xx + 13, yy1);
// g.DrawString("" + (int)ang, xx + 14, yy1);
}
x_1 = (flap.delta - flap.delta_min) / (flap.delta_max - flap.delta_min);
int yy1_2 = (int)(flap_width * x_1 + 0.5D);
// g.FillRect(xx + 2, yy - flap_width, 7, yy1_2);
}
//g.SetFont(stdFont);
scine.Draw(g);
//g.SetFont(stdFont);
}
internal void Calc_dynamics(int lr, ControlPlane cw, AirPlane ap, Vector3D dv, double k_q, double k_S)
{
Matrix44 ma = new Matrix44();
Matrix44 mtemp = new Matrix44();
Vector3D vtemp = new Vector3D();
fv.SetVec(0.0D, 0.0D, 0.0D);
tv.SetVec(0.0D, 0.0D, 0.0D);
ac = AirPlane.Get_point(ac_base, lr).Sub(ap.inp.cg);
dvv = ap.pMotion.omega.CrsProd(ac);
vd = ap.pMotion.vc.Add(dvv);
vd = vd.Add(dv);
v = vd.Length();
vd = vd.NmlVec().SclProd(v * k_q);
v = vd.Length();
s2_dash = (s2 * k_S);
m = (v / ap.atmos.a);
q = (0.5D * v * v * ap.atmos.rho);
Vector3D kdd = new Vector3D();
Vector3D idd = new Vector3D();
Vector3D jdd = new Vector3D();
if ((cw != null) && (cw.type == 2))
{
ma.SetRyMat(cw.delta);
mtemp.SetRzMat(cw.lamda_h);
ma = ma.MultMat(mtemp);
if (lr == 1)
{
mtemp.SetRxMat(-cw.gamma_h);
}
else
{
mtemp.SetRxMat(-cw.gamma_h);
}
ma = ma.MultMat(mtemp);
idd = id.MultMat(ma);
kdd = kd.MultMat(ma);
}
else
{
idd = new Vector3D(id);
jdd = new Vector3D(jd);
kdd = new Vector3D(kd);
}
mtemp.Set3ColVec(idd, jdd, kdd);
vdw = vd.MultMat(mtemp);
alpha = Jp.Maker1.Sim.Tools.Tool.CalcAlpha(vdw);
beta = Jp.Maker1.Sim.Tools.Tool.CalcBeta(vdw);
ar = wing.AspectRatio(beta);
are = (ar * wing.K_ground_effect(beta,
ap.pMotion.wpos.y));
lamda_dash = SweepbackAngle(wing.hv_arrangement, lr,
beta);
Calc_cla();
delta_cl_flap = 0.0D;
delta_cd_flap = 0.0D;
delta_cmac_flap = 0.0D;
delta_alpha = 0.0D;
k_a = 1.0D;
if ((cw != null) && ((cw.type == 1) || (cw.type == 1)))
{
cw.beta_f = Flap.Beta_f(lr, wing.hv_arrangement, cw.lamda_h, beta);
cw.delta_dash = Flap.Delta_dash(cw.delta, cw.beta_f);
if (Math.Abs(cw.beta_f) < 1.570796326794897D)
{
delta_alpha = (cw.f_lamda1 * cw.delta_dash);
delta_cmac_flap = cw.f_cmac;
}
else
{
delta_alpha = (cw.b_lamda1 * cw.delta_dash);
delta_cmac_flap = cw.b_cmac;
}
k_a = Flap.K_cla(cw.delta_dash, cw.cf_c);
delta_cl_flap = (k_a * cla * delta_alpha);
delta_cmac_flap *= (alpha + delta_alpha - alpha0);
}
vtemp.SetVec(0.0D, 0.0D, -1.0D);
ma.SetRyMat(-alpha);
mtemp.SetRzMat(beta);
ma = ma.MultMat(mtemp);
mtemp.Set3RowVec(idd, jdd, kdd);
ma = ma.MultMat(mtemp);
lu = vtemp.MultMat(ma);
du = vd.SclProd(-1.0D).NmlVec();
alpha += delta_alpha;
cla *= k_a;
Calc_cl_cd();
l = (q * cl * s2_dash);
cdi = (cl * cl / (Math.PI * are * ew));
cd += cdi;
cd += delta_cd_flap;
d = (q * cd * s2_dash);
lf = Dynamics.Force(l, lu);
lt = Dynamics.Torque(ac, lf);
df = Dynamics.Force(d, du);
dt = Dynamics.Torque(ac, df);
cmac = cmac0;
cmac += delta_cmac_flap;
mac = (q * s2_dash * cmac);
Vector3D mt_0 = new Vector3D(0.0D, mac, 0.0D);
fv = lf.Add(df);
tv = lt.Add(dt).Add(mt_0);
}
