private async Task <List <Pixel> > GetListAsync(Group group, int dx, int dy, int viceVersa, int width, int height, Bgr24Bitmap bitmap)
{
return(await Task.Run(() =>
{
List <Pixel> pixels = new List <Pixel>();
int count = 0;
ZBuffer zBuf = new ZBuffer(width, height);
Parallel.ForEach(group.Faces, face =>
{
if (IsFaceVisible(group.Vertices, face))
{
List <Pixel> pixelsForSide = new List <Pixel>();
List <Pixel> pixelsInSide = new List <Pixel>();
Vertex vertex0, vertex1;
int index0, index1;
Vector3 lightingVector = new Vector3(0, 0, 1);
int ind0 = (face.FaceElements.ElementAt(0).VertexNormalIndex != null) ? (int)face.FaceElements.ElementAt(0).VertexNormalIndex : 1;
Vector3 point0Normal = new Vector3(group.VertexNormals[ind0 - 1].X, group.VertexNormals[ind0 - 1].Y, group.VertexNormals[ind0 - 1].Z);
int ind1 = (face.FaceElements.ElementAt(1).VertexNormalIndex != null) ? (int)face.FaceElements.ElementAt(1).VertexNormalIndex : 1;
Vector3 point1Normal = new Vector3(group.VertexNormals[ind1 - 1].X, group.VertexNormals[ind1 - 1].Y, group.VertexNormals[ind1 - 1].Z);
int ind2 = (face.FaceElements.ElementAt(2).VertexNormalIndex != null) ? (int)face.FaceElements.ElementAt(2).VertexNormalIndex : 1;
Vector3 point2Normal = new Vector3(group.VertexNormals[ind2 - 1].X, group.VertexNormals[ind2 - 1].Y, group.VertexNormals[ind2 - 1].Z);
Color color = Color.FromArgb(255, 255, 0, 0);
Color point1Color = Lambert.GetPointColor(point0Normal, lightingVector, color);
Color point2Color = Lambert.GetPointColor(point1Normal, lightingVector, color);
Color point3Color = Lambert.GetPointColor(point2Normal, lightingVector, color);
Color faceColor = PlaneShading.GetAverageColor(point1Color, point2Color, point3Color);
for (int i = 0; i < face.FaceElements.Count - 1; i++)
{
index0 = (face.FaceElements.ElementAt(i).VertexIndex != -2) ? face.FaceElements.ElementAt(i).VertexIndex : (group.Vertices.Count - 1);
index1 = (face.FaceElements.ElementAt(i + 1).VertexIndex != -2) ? face.FaceElements.ElementAt(i + 1).VertexIndex : (group.Vertices.Count - 1);
vertex0 = group.Vertices.ElementAt(index0);
vertex1 = group.Vertices.ElementAt(index1);
pixelsForSide.AddRange(Bresenham.GetPixels((int)(vertex0.X + dx), (int)(vertex0.Y * viceVersa + dy), (int)(vertex0.Z), (int)(vertex1.X + dx), (int)(vertex1.Y * viceVersa + dy), (int)(vertex1.Z), windowWidth, windowHeight, bitmap, zBuf, faceColor));
}
index0 = (face.FaceElements.ElementAt(0).VertexIndex != -2) ? face.FaceElements.ElementAt(0).VertexIndex : (group.Vertices.Count - 1);
index1 = (face.FaceElements.ElementAt(face.FaceElements.Count - 1).VertexIndex != -2) ? face.FaceElements.ElementAt(face.FaceElements.Count - 1).VertexIndex : (group.Vertices.Count - 1);
vertex0 = group.Vertices.ElementAt(index0);
vertex1 = group.Vertices.ElementAt(index1);
pixelsForSide.AddRange(Bresenham.GetPixels((int)(vertex0.X + dx), (int)(vertex0.Y *viceVersa + dy), vertex0.Z, (int)(vertex1.X + dx), (int)(vertex1.Y *viceVersa + dy), vertex1.Z, windowWidth, windowHeight, bitmap, zBuf, faceColor));
RastAlgorithm.DrawPixelForRasterization(pixelsForSide, bitmap, zBuf, faceColor);
//pixels.AddRange(pixelsForSide);
//pixelsInSide.AddRange(RastAlgorithm.DrawPixelForRasterization(pixelsForSide, bitmap, zBuf));
//pixels.AddRange(pixelsInSide);
count++;
}
});
return pixels;
}));
}
private static void test02()
//****************************************************************************80
//
// Purpose:
//
// TEST02 tests WEW_B
//
// Licensing:
//
// This code is distributed under the GNU LGPL license.
//
// Modified:
//
// 11 June 2014
//
// Author:
//
// John Burkardt
//
{
double en = 0;
double w1 = 0;
double x = 0;
Console.WriteLine("");
Console.WriteLine("TEST02");
Console.WriteLine(" Test WEW_B to evaluate");
Console.WriteLine(" Lambert's W function.");
Console.WriteLine("");
Console.WriteLine(" X Exact Computed Error");
Console.WriteLine("");
int n_data = 0;
for (;;)
{
Burkardt.Values.Lambert.lambert_w_values(ref n_data, ref x, ref w1);
if (n_data <= 0)
{
break;
}
double w2 = x switch
{
0.0 => 0.0,
_ => Lambert.wew_b(x, ref en)
};
Console.WriteLine(x.ToString(CultureInfo.InvariantCulture).PadLeft(14) + " "
+ w1.ToString(CultureInfo.InvariantCulture).PadLeft(16) + " "
+ w2.ToString(CultureInfo.InvariantCulture).PadLeft(16) + " "
+ Math.Abs(w1 - w2).ToString(CultureInfo.InvariantCulture).PadLeft(10) + "");
}
}
}
bool LambertSolutionExists()
{
// Make local copies of departure and arrival orbits.
OrbitData earthCopy = null;
OrbitData asteroidCopy = null;
foreach (Body body in Bodies)
{
if (body.tag == "Earth")
{
earthCopy = new OrbitData(body.Orbit);
}
else if (body.tag == "Asteroid")
{
asteroidCopy = new OrbitData(body.Orbit);
}
}
// Advance orbits to epoch of impact for Lambert solver
earthCopy.Epoch = ImpactEpoch;
asteroidCopy.Epoch = ImpactEpoch;
// Get the transfer orbit and C3 from the Lambert solution
LambertSolution lambertSolution = Lambert.GetTransferOrbit(earthCopy, asteroidCopy, TimeOfDeflection, TransferTime, -1);
if (lambertSolution == null)
{
Debug.Log("No Lambert solution found\nTry different mission values.");
ShowInfeasibleLaunchWindow();
return(false);
}
if (lambertSolution.C3 <= 0.0)
{
Debug.Log("Lambert solution requires negative C3");
ShowInfeasibleLaunchWindow();
return(false);
}
double deliverableMass = LaunchVehicleType.ComputeDeliverableMass(lambertSolution.C3, NumLaunches * EffectMultiplier);
if (deliverableMass <= 0.0)
{
Debug.LogFormat("Launch C3 = {0:F4}\nLaunch Vehicle unable to obtain required launch energy",
lambertSolution.C3);
ShowInfeasibleLaunchWindow();
return(false);
}
Debug.LogFormat("Launch C3 = {0:F4}Impact Mass = {1:F4}; Impact Vel. = {2:E4}",
lambertSolution.C3, MassKI, lambertSolution.arrDV.magnitude);
SetMissionValuesText(deliverableMass, lambertSolution.C3, lambertSolution.arrDV.magnitude);
return(true);
}
//兰伯特投影
public static List <PointF[]> inverseCompute(List <PointF[]> mapPoints)
{
List <PointF[]> outList = new List <PointF[]>();
for (int i = 0; i < mapPoints.Count; i++)
{
PointF[] points = new PointF[mapPoints[i].Length];
for (int j = 0; j < mapPoints[i].Length; j++)
{
points[j] = Lambert.blToXY(mapPoints[i][j]);
}
outList.Add(points);
Lambert.blToXY
}
return(outList);
}
public void LambertTest()
{
/*
* Vector3 EarthRad = Earth.Heliocentric(2457239 - 2451545);
* Vector3 MarsRad = Mars.Heliocentric(2457239 - 2451545 + 150);
* double time = 150;
*/
Vector3 EarthRad = new Vector3(4.440778960961146E+07, -1.454625135657227E+08, 7.039903338298202E+03);
Vector3 MarsRad = new Vector3(8.550441288420311E+07, 2.098123095830674E+08, 2.299312316831380E+06);
double time = 2459219 - 2459039;
Vector3 Vout = new Lambert().Solver(EarthRad, MarsRad, time, "pro", "V1");
double LambertIs = Vout.Magnitude();
double ShouldBe = 32.9054;
Assert.AreEqual(LambertIs, ShouldBe, .05);
}
public static void lambert_w_values_test()
//****************************************************************************80
//
// Purpose:
//
// LAMBERT_W_VALUES_TEST tests LAMBERT_W_VALUES.
//
// Licensing:
//
// This code is distributed under the GNU LGPL license.
//
// Modified:
//
// 12 June 2007
//
// Author:
//
// John Burkardt
//
{
double fx = 0;
double x = 0;
Console.WriteLine("");
Console.WriteLine("LAMBERT_W_VALUES_TEST:");
Console.WriteLine(" LAMBERT_W_VALUES stores values of ");
Console.WriteLine(" the Lambert W function.");
Console.WriteLine("");
Console.WriteLine(" X W(X)");
Console.WriteLine("");
int n_data = 0;
for (;;)
{
Lambert.lambert_w_values(ref n_data, ref x, ref fx);
if (n_data == 0)
{
break;
}
Console.WriteLine(" "
+ x.ToString("0.################").PadLeft(24) + " "
+ fx.ToString("0.################").PadLeft(24) + "");
}
}
/// <summary>
/// Launches a spacecraft from Earth to intercept/deflect the asteroid.
/// </summary>
public void LaunchSpacecraft()
{
// Make local copies of departure and arrival orbits.
OrbitData earth = null;
OrbitData asteroid = null;
foreach (Body body in Bodies)
{
if (body.tag == "Earth")
{
earth = new OrbitData(body.Orbit);
}
else if (body.tag == "Asteroid")
{
asteroid = new OrbitData(body.Orbit);
}
}
if (earth == null || asteroid == null)
{
Debug.LogError("Error finding departure/arrival orbits from bodies list by tag");
return;
}
// Advance orbits to epoch of impact for Lambert solver
earth.Epoch = ImpactEpoch;
asteroid.Epoch = ImpactEpoch;
// Get the transfer orbit and C3 from the Lambert solution
LambertSolution lambertSolution = Lambert.GetTransferOrbit(earth, asteroid, TimeOfDeflection, TransferTime, -1);
if (lambertSolution == null || lambertSolution.C3 <= 0.0)
{
DisplayTextWithFadeEffect(MessageText, "No Lambert solution found");
return;
}
// MassKI calculated here will be used in ProcessCollisionEnter
MassKI = LaunchVehicleType.ComputeDeliverableMass(lambertSolution.C3, NumLaunches * EffectMultiplier);
if (MassKI <= 0.0)
{
DisplayTextWithFadeEffect(MessageText, string.Format("Launch vehicle unable to achieve C3 {0:E3} (km/s)^2", lambertSolution.C3));
return;
}
// TODO: Initialize spacecraft from prefab here
//GameObject prefab = Instantiate(Resources.Load("Spacecraft.prefab", typeof(GameObject)) as GameObject);
Body spacecraft = spacecraftObject.GetComponent <Body>();
if (spacecraft == null)
{
Debug.LogError("Instantiated spacecraft prefab does not have Body component");
}
spacecraft.InitOrbit(lambertSolution.TransferOrbit);
spacecraft.SetImpactEpoch(ImpactEpoch - TimeOfDeflection);
spacecraft.gameObject.SetActive(true);
Bodies = FindObjectsOfType <Body>(); // Update bodies list
string message = string.Format("Launch successful!\nC3 = {0:F3} (km/s)^2\nMass = {1:F1} kg", lambertSolution.C3, MassKI);
DisplayTextWithFadeEffect(MessageText, message);
}
public Technique(string sid, Lambert item)
: this(sid)
{ this.item = item; }