private void drawApoapse(Graphics g, Orbit orbit)
{
float x, y;
Tuple <double, double> XY = getXYfromTheta(Helper.deg2rad(180) + thetaZero, orbit);
x = (float)XY.Item1;
y = (float)XY.Item2;
g.FillEllipse(apoBrush, x - 5, y - 5, 10, 10);
g.DrawString(Math.Round(orbit.ApoapsisAltitude).ToString(), font, textBrush, x, y);
}
private void drawAscDescNodes(Graphics g, Orbit orbit)
{
float x, y;
Tuple <double, double> XY = getXYfromTheta(alphaZero, orbit);
x = (float)XY.Item1;
y = (float)XY.Item2;
g.FillEllipse(NodeBrush, x - 5, y - 5, 10, 10);
XY = getXYfromTheta(Helper.deg2rad(180) + alphaZero, orbit);
x = (float)XY.Item1;
y = (float)XY.Item2;
g.FillEllipse(NodeBrush, x - 5, y - 5, 10, 10);
}
private PointF[] screwInfillPoints(float x, float y, float size)
{
PointF[] path = new PointF[6];
float s = (float)((size / 2f) * Math.Sin(Helper.deg2rad(30)));
float l = (float)((size / 2f) * Math.Cos(Helper.deg2rad(30)));
path[0] = new PointF(x, y + (size / 2f));
path[1] = new PointF(x + s, y + (size / 2f) - l);
path[2] = new PointF(x + size - s, y + (size / 2f) - l);
path[3] = new PointF(x + size, y + (size / 2f));
path[4] = new PointF(x + size - s, y + (size / 2f) + l);
path[5] = new PointF(x + s, y + (size / 2f) + l);
return(path);
}
private void drawSinglePointer(Graphics g)
{
// Pointer
double scaler = (Height - 20) / (double)Math.Abs(scale1max - scale1min);
float y = (float)((Height - 10) - (value1 * scaler));
float x = 3;
float w = Width / 3;
float a = 50; // Angle at "pointy" end
PointF[] points = new PointF[4];
points[0] = new PointF(x + w, y);
points[1] = new PointF(x, (float)(y + (w * Math.Sin(Helper.deg2rad(a / 2)))));
points[2] = new PointF(x, (float)(y - (w * Math.Sin(Helper.deg2rad(a / 2)))));
points[3] = new PointF(x + w, y);
g.FillPolygon(pointerBrush, points);
RectangleF Rect = new RectangleF(0, y - 1, 4, 2);
g.FillRectangle(pointerBrush, Rect);
}
public override void updateLocalElements(object sender, EventArgs e)
{
// Re-usable data variable for graph data
List <List <KeyValuePair <double, double?> > > data = new List <List <KeyValuePair <double, double?> > >();
List <Plot.Type> types = new List <Plot.Type>();
int steps = 200;
string tgtapo = form.dataStorage.getData("TGTAPO");
if (tgtapo == "")
{
tgtapo = "120000";
form.dataStorage.setData("TGTAPO", "120000");
}
int.TryParse(tgtapo, out int apo);
double mass = form.streamCollection.GetData(DataType.body_mass);
if (mass == 0)
{
mass = 5.2915158e22;
}
double bodyrad = form.streamCollection.GetData(DataType.body_radius);
if (bodyrad == 0)
{
bodyrad = 600000;
}
double distance = bodyrad + apo;
double speed = Math.Sqrt((6.67408e-11 * mass) / distance);
// Find inertial speed at the pad
float rotPeriod = form.streamCollection.GetData(DataType.body_rotPeriod);
if (rotPeriod == 0)
{
rotPeriod = 21600;
} // If no period found, set to Kerbin-period
double lat = 0; // TODO: Set to 0 now, add button to calibrate later
// MAKE GUIDE(S)
// TODO: THIS SHOULD MAYBE BE CALCULATED BY SOME METHOD
double StaticSpeed = (2 * Math.PI * bodyrad * Math.Cos(Helper.deg2rad(lat))) / rotPeriod;
double speedStep = (speed - StaticSpeed) / steps;
double maxAngle = 40;
double maxAnglePosition = 0.1; // position on the velocity axis of max angle. 0.0 - 1.0
double maxAngleSpeed = ((speed - StaticSpeed) * maxAnglePosition) + StaticSpeed;
double a = (speed - StaticSpeed) * maxAnglePosition; // X-axis length
double b = maxAngle; // Y-axis height
double c = 0; // Y-axis offset
double d = maxAngleSpeed; // X-axis offset
List <KeyValuePair <double, double?> > middle = new List <KeyValuePair <double, double?> >();
List <KeyValuePair <double, double?> > middle2 = new List <KeyValuePair <double, double?> >();
List <KeyValuePair <double, double?> > tgt = new List <KeyValuePair <double, double?> >();
List <KeyValuePair <double, double?> > low = new List <KeyValuePair <double, double?> >();
List <KeyValuePair <double, double?> > low2 = new List <KeyValuePair <double, double?> >();
List <KeyValuePair <double, double?> > high = new List <KeyValuePair <double, double?> >();
List <KeyValuePair <double, double?> > high2 = new List <KeyValuePair <double, double?> >();
for (int i = 0; i <= steps; i++)
{
// ELLIPTIC CURVE
int x = (int)(Math.Round(i * ((maxAngleSpeed - StaticSpeed) / steps)) + StaticSpeed);
double?y = Math.Sqrt(Math.Pow(b, 2) * (1 - (Math.Pow(x - d, 2) / Math.Pow(a, 2)))) + c;
if (i == 0)
{
y = 0;
}
middle.Add(new KeyValuePair <double, double?>(x, y));
low.Add(new KeyValuePair <double, double?>(x, y * 0.8));
high.Add(new KeyValuePair <double, double?>(x, y * 1.2));
// SMOOTHSTEP DOWN
x = (int)(speed - (i * ((speed - maxAngleSpeed) / steps)));
double t = (x - maxAngleSpeed) / (speed - maxAngleSpeed);
double m0 = 1.5;
double m1 = 0.5;
double sx = ((Math.Pow(t, 3) - (2 * Math.Pow(t, 2)) + t) * m0)
+
((-2 * Math.Pow(t, 3)) + (3 * Math.Pow(t, 2)))
+
((Math.Pow(t, 3) - Math.Pow(t, 2)) * m1);
double sy = (-2 * Math.Pow(t, 3)) + (3 * Math.Pow(t, 2));
x = (int)(speed - Math.Round(sx * (speed - maxAngleSpeed)));
y = sy * maxAngle;
middle2.Add(new KeyValuePair <double, double?>(x, y));
low2.Add(new KeyValuePair <double, double?>(x, y * 0.8));
high2.Add(new KeyValuePair <double, double?>(x, y * 1.2));
}
// TARGET LINE
tgt.Add(new KeyValuePair <double, double?>(speed, -2));
tgt.Add(new KeyValuePair <double, double?>(speed, 2));
data.Add(middle);
types.Add(Plot.Type.LINE);
data.Add(middle2);
types.Add(Plot.Type.LINE);
if (form.form.connected && form.form.krpc.CurrentGameScene == GameScene.Flight)
{
data.Add(chartData["FlightangleVelocity"]);
types.Add(Plot.Type.CROSS);
}
else
{
// ADD EMPTY DATA
data.Add(new List <KeyValuePair <double, double?> >());
types.Add(Plot.Type.CROSS);
}
data.Add(tgt);
types.Add(Plot.Type.LINE);
data.Add(low);
types.Add(Plot.Type.LINE);
data.Add(low2);
types.Add(Plot.Type.LINE);
data.Add(high);
types.Add(Plot.Type.LINE);
data.Add(high2);
types.Add(Plot.Type.LINE);
screenCharts[0].setData(data, types, false);
screenCharts[0].maxX = (int)Math.Round(speed * 1.1f);
}
private void MakeOrbitConstants(Graphics g, Orbit orbit, bool relativeToParent, double time, string debugstr, bool relativeREF)
{
float x, y;
double alpha;
double r;
double REF = 0; // Degress from x-right
double bodyInc;
if (orbit.Body.Name == "Sun")
{
bodyInc = 0;
}
else
{
bodyInc = orbit.Body.Orbit.Inclination;
if (relativeREF)
{
if (time != -1)
{
if (bodyInc > Helper.deg2rad(90) && bodyInc <= Helper.deg2rad(270))
{
REF = 0 - orbit.Body.Orbit.LongitudeOfAscendingNode + orbit.Body.Orbit.ArgumentOfPeriapsis + orbit.Body.Orbit.TrueAnomalyAtUT(time);
}
else
{
REF = 0 - orbit.Body.Orbit.LongitudeOfAscendingNode - orbit.Body.Orbit.ArgumentOfPeriapsis - orbit.Body.Orbit.TrueAnomalyAtUT(time);
}
}
else
{
if (bodyInc > Helper.deg2rad(90) && bodyInc <= Helper.deg2rad(270))
{
REF = 0 - orbit.Body.Orbit.LongitudeOfAscendingNode + orbit.Body.Orbit.ArgumentOfPeriapsis + orbit.Body.Orbit.TrueAnomaly;
}
else
{
REF = 0 - orbit.Body.Orbit.LongitudeOfAscendingNode - orbit.Body.Orbit.ArgumentOfPeriapsis - orbit.Body.Orbit.TrueAnomaly;
}
}
}
}
eccentricity = orbit.Eccentricity;
inclination = orbit.Inclination;
trueAnomaly = orbit.TrueAnomaly;
bodyOrbit = orbit.Body.Orbit;
if (eccentricity <= 0.00001)
{
// SET EVERYTHING TO 0
thetaZero = 0;
thetaZeroNoREF = 0;
alphaZero = 0;
directrix = orbit.Periapsis;
x = (float)((orbit.Periapsis * scaler) + graphCenterX);
P1 = new PointF(x, (float)(graphCenterY + satY));
P2 = new PointF(-x, (float)(graphCenterY - satY));
}
else
{
if (inclination > Helper.deg2rad(90) && inclination <= Helper.deg2rad(270))
{
thetaZeroNoREF = 0 - orbit.LongitudeOfAscendingNode + orbit.ArgumentOfPeriapsis; // Rotation clockwise from x-direction (Right) of Apoapse
thetaZero = REF + thetaZeroNoREF;
alphaZero = REF - orbit.LongitudeOfAscendingNode; // Decending Node
}
else
{
thetaZeroNoREF = 0 - orbit.LongitudeOfAscendingNode - orbit.ArgumentOfPeriapsis; // Rotation counterclockwise from x-direction (Right) of Apoapse
thetaZero = REF + thetaZeroNoREF;
alphaZero = REF - orbit.LongitudeOfAscendingNode; // Decending Node
}
directrix = (orbit.Periapsis / eccentricity) + orbit.Periapsis;
//Inclination point 1
alpha = alphaZero;
r = (eccentricity * directrix) / (1 + (eccentricity * Math.Cos(alpha - thetaZero)));
x = (float)((r * Math.Cos(alpha) * scaler) + graphCenterX + satX);
y = (float)((r * Math.Sin(alpha) * scaler) + graphCenterY - satY);
P1 = new PointF(x, y);
//g.FillEllipse(burnBrush, x - 5, y - 5, 10, 10);
//Inclination point 2
alpha = Helper.deg2rad(180) + alphaZero;
r = (eccentricity * directrix) / (1 + (eccentricity * Math.Cos(alpha - thetaZero)));
x = (float)((r * Math.Cos(alpha) * scaler) + graphCenterX + satX);
y = (float)((r * Math.Sin(alpha) * scaler) + graphCenterY - satY);
P2 = new PointF(x, y);
//g.FillEllipse(burnBrush, x - 5, y - 5, 10, 10);
}
// DEBUG LINES
if (debug)
{
PointF center = new PointF((float)(graphCenterX + satX), (float)(graphCenterY - satY));
x = (float)((200 * Math.Cos(thetaZero)) + center.X);
y = (float)((200 * Math.Sin(thetaZero)) + center.Y);
g.DrawLine(burnPen, center, new PointF(x, y));
g.DrawString("ThetaZero " + debugstr, font, textBrush, x, y);
x = (float)((200 * Math.Cos(alphaZero)) + center.X);
y = (float)((200 * Math.Sin(alphaZero)) + center.Y);
g.DrawLine(burnPen, center, new PointF(x, y));
g.DrawString("AlphaZero " + debugstr, font, textBrush, x, y);
x = (float)((200 * Math.Cos(REF)) + center.X);
y = (float)((200 * Math.Sin(REF)) + center.Y);
g.DrawLine(burnPen, center, new PointF(x, y));
g.DrawString("REF " + debugstr, font, textBrush, x, y);
g.DrawArc(burnPen, center.X - 180, center.Y - 180, 360, 360, (float)Helper.rad2deg(REF), (float)Helper.rad2deg(alphaZero - REF));
g.DrawArc(burnPen, center.X - 160, center.Y - 160, 320, 320, (float)Helper.rad2deg(alphaZero), (float)Helper.rad2deg(thetaZero - alphaZero));
}
}
private void drawPatchedConic(Graphics g, Orbit orbit, double thetaStart, double thetaEnd, Color orbitColor, bool relativeToParent)
{
int steps = 60; // Number of line segments
double totTheta = thetaEnd - thetaStart;
double thetaStep = totTheta / steps;
double theta;
PointF?lastPoint = null;
PointF?point = null;
PointF center;
Pen localPen = new Pen(orbitColor, 2f);
Brush localBrush = new SolidBrush(orbitColor);
for (int i = 0; i <= steps; i++)
{
// IF relativeToParent, recalculate satX/Y and thetaZero each time.
if (relativeToParent)
{
theta = Helper.deg2rad(180 - ((i * thetaStep) + thetaStart)) + thetaZeroNoREF;
double time = orbit.UTAtTrueAnomaly(theta - thetaZeroNoREF);
Tuple <double, double, double> pos = bodyOrbit.PositionAt(time, bodyNonRotFrame);
satX = pos.Item1 * scaler;
satY = pos.Item3 * scaler;
if (pos.Item3 <= 0)
{
thetaZero = Math.Acos(pos.Item1 / Math.Sqrt(Math.Pow(pos.Item1, 2) + Math.Pow(pos.Item3, 2))) + thetaZeroNoREF;
}
else
{
thetaZero = (Helper.deg2rad(360) - Math.Acos(pos.Item1 / Math.Sqrt(Math.Pow(pos.Item1, 2) + Math.Pow(pos.Item3, 2)))) + thetaZeroNoREF;
}
}
theta = Helper.deg2rad(180 - ((i * thetaStep) + thetaStart)) + thetaZero;
Tuple <double, double> XY = getXYfromTheta(theta, orbit, relativeToParent);
point = new PointF((float)XY.Item1, (float)XY.Item2);
if (lastPoint != null)
{
g.DrawLine(localPen, (PointF)lastPoint, (PointF)point);
g.DrawLine(orbitPen3, (PointF)lastPoint, (PointF)point);
lastPoint = point;
}
else
{
lastPoint = point;
}
if (i % 10 == 0 && debug)
{
center = new PointF((float)(graphCenterX + satX), (float)(graphCenterY - satY));
g.DrawLine(orbitPen, (PointF)point, center);
float x = (float)((300 * Math.Cos(thetaZero)) + center.X);
float y = (float)((300 * Math.Sin(thetaZero)) + center.Y);
g.DrawLine(burnPen, center, new PointF(x, y));
g.DrawString("ThetaZero ", font, textBrush, x, y);
}
if (i == 0 && eccentricity >= 1)
{
float size = 10;
center = (PointF)point;
PointF[] shape = new PointF[3];
shape[0] = new PointF(center.X + (size * -1f), center.Y + (size * -1.0f));
shape[1] = new PointF(center.X + (size * 1f), center.Y + (size * -1.0f));
shape[2] = new PointF(center.X + (size * 0f), center.Y + (size * 0f));
//g.FillPolygon(EnterSoiBrush, shape);
g.FillEllipse(EnterSoiBrush, center.X - (size / 2), center.Y - (size / 2), size, size);
}
else if (i == steps && !double.IsNaN(orbit.TimeToSOIChange))
{
float size = 10;
center = (PointF)point;
PointF[] shape = new PointF[3];
shape[0] = new PointF(center.X + (size * -1f), center.Y + (size * 1f));
shape[1] = new PointF(center.X + (size * 1f), center.Y + (size * 1f));
shape[2] = new PointF(center.X + (size * 0f), center.Y + (size * 0f));
//g.FillPolygon(ExitSoiBrush, shape);
g.FillEllipse(ExitSoiBrush, center.X - (size / 2), center.Y - (size / 2), size, size);
}
}
}
protected override void OnPaint(PaintEventArgs e)
{
Graphics g = e.Graphics;
g.SmoothingMode = SmoothingMode.HighQuality;
g.TextRenderingHint = TextRenderingHint.ClearTypeGridFit;
// DEBUG TEST
//g.FillRectangle(new SolidBrush(Color.Maroon), 0, 0, this.Width, this.Height);
// Check for body and orbitset
if (currentOrbit != null)
{
// Determine scaler
int maxSizePx;
if (this.Width < this.Height)
{
maxSizePx = this.Width;
}
else
{
maxSizePx = this.Height;
}
// Get biggest apopapsis of satellites
double satMaxApo = 0;
// Check of vessel orbit is biggest
if (currentOrbit.Apoapsis > satMaxApo)
{
double maxDist = (currentOrbit.Apoapsis * 2.25) / zoom; // The .25 is to have some margin to the edges of the graph
scaler = maxSizePx / maxDist;
}
else
{
scaler = maxSizePx / ((satMaxApo * 2.25) / zoom);
}
// Set Center of graph
graphCenterX = (Width / 2);
graphCenterY = (Height / 2);
// Add manual offset
graphCenterX += (float)(slideX + slideXtmp);
graphCenterY += (float)(slideY + slideYtmp);
// Draw Body
float left = graphCenterX - (float)(currentOrbit.Body.EquatorialRadius * scaler);
float top = graphCenterY - (float)(currentOrbit.Body.EquatorialRadius * scaler);
float width = (float)(currentOrbit.Body.EquatorialRadius * 2 * scaler);
float height = (float)(currentOrbit.Body.EquatorialRadius * 2 * scaler);
RectangleF rect = new RectangleF(left, top, width, height);
g.FillEllipse(bodyBrush, rect);
// Draw satellites
foreach (CelestialBody sat in bodySatellites)
{
Orbit orbit = sat.Orbit;
MakeOrbitConstants(g, orbit);
drawPatchedConic(g, orbit, 0, 360, orbitColor);
drawCurrentPosition(g, orbit);
}
MakeOrbitConstants(g, currentOrbit, false, "CurrentOrbit");
drawPatchedConic(g, currentOrbit, 0, 360, orbitColor);
drawPeriapse(g, currentOrbit);
drawApoapse(g, currentOrbit);
drawAscDescNodes(g, currentOrbit);
drawCurrentPosition(g, currentOrbit);
if (burnNodes != null)
{
int s = 0;
for (int i = 0; i < burnNodes.Count; i++)
{
Node burnNode = burnNodes[i];
drawBurnPoint(g, burnNode);
if (!double.IsNaN(burnNode.Orbit.TimeToSOIChange))
{
double SOIUT = burnNode.Orbit.TimeToSOIChange + UT;
double TAatSOI = burnNode.Orbit.TrueAnomalyAtUT(SOIUT);
double burnTA = burnNode.Orbit.TrueAnomalyAtUT(burnNode.UT);
// Swap thetaStart and thetaEnd is orbit is retrograde
if (burnNode.Orbit.Inclination > Helper.deg2rad(90) && burnNode.Orbit.Inclination <= Helper.deg2rad(275))
{
double tmp = burnTA;
burnTA = TAatSOI;
TAatSOI = tmp;
}
MakeOrbitConstants(g, burnNode.Orbit, false, "Node " + i.ToString());
drawPatchedConic(g, burnNode.Orbit, Helper.rad2deg(burnTA) + 180, Helper.rad2deg(TAatSOI) + 180, burnOrbitColor[i + s % 3]);
Orbit SOIorbit = burnNode.Orbit.NextOrbit;
while (SOIorbit != null)
{
s++;
double entryTA = SOIorbit.TrueAnomalyAtUT(SOIUT);
SOIUT = SOIorbit.TimeToSOIChange + UT;
if (!double.IsNaN(SOIUT))
{
TAatSOI = SOIorbit.TrueAnomalyAtUT(SOIUT);
}
else
{
TAatSOI = Helper.deg2rad(360);
entryTA = 0;
}
// Swap thetaStart and thetaEnd is orbit is retrograde
if (SOIorbit.Inclination > Helper.deg2rad(90) && SOIorbit.Inclination <= Helper.deg2rad(275))
{
double tmp = entryTA;
entryTA = TAatSOI;
TAatSOI = tmp;
}
satX = 0;
satY = 0;
if (SOIorbit.Body.Name != body.Name && SOIorbit.Body.Name != "Sun")
{
// ORBIT AROUND ANTOHER BODY
double CloseTime = SOIorbit.TimeToPeriapsis + burnNode.Orbit.TimeToSOIChange + UT;
MakeOrbitConstants(g, SOIorbit.Body.Orbit, false, "SOI Orbit Blob");
drawBlob(g, SOIorbit.Body.Orbit, CloseTime); // This need to be done with satX/Y at 0, becouse it is relative to main body
satX = SOIorbit.Body.Orbit.PositionAt(UT, bodyNonRotFrame).Item1 *scaler;
satY = SOIorbit.Body.Orbit.PositionAt(UT, bodyNonRotFrame).Item3 *scaler;
MakeOrbitConstants(g, SOIorbit, false, -1, "SOI Orbit local", true);
drawPatchedConic(g, SOIorbit, Helper.rad2deg(entryTA) + 180, Helper.rad2deg(TAatSOI) + 180, burnOrbitColor[(i + s) % 3]);
drawPeriapse(g, SOIorbit);
// Main body relative orbit
satX = SOIorbit.Body.Orbit.PositionAt(CloseTime, bodyNonRotFrame).Item1 *scaler;
satY = SOIorbit.Body.Orbit.PositionAt(CloseTime, bodyNonRotFrame).Item3 *scaler;
relPeriapse = -1;
MakeOrbitConstants(g, SOIorbit, true, CloseTime, "SOI Orbit Relative", true);
drawPatchedConic(g, SOIorbit, Helper.rad2deg(entryTA) + 180, Helper.rad2deg(TAatSOI) + 180, burnOrbitColor[(i + s) % 3], true);
drawPeriapse(g, relPeriapseX, relPeriapseY);
}
else
{
MakeOrbitConstants(g, SOIorbit, false, "SOI Orbit " + s.ToString());
drawPatchedConic(g, SOIorbit, Helper.rad2deg(entryTA) + 180, Helper.rad2deg(TAatSOI) + 180, burnOrbitColor[(i + s) % 3]);
drawPeriapse(g, SOIorbit);
}
if (SOIorbit.Eccentricity < 1 && double.IsNaN(SOIorbit.TimeToSOIChange))
{
drawApoapse(g, SOIorbit);
drawAscDescNodes(g, SOIorbit);
}
SOIorbit = SOIorbit.NextOrbit;
}
}
else
{
satX = 0;
satY = 0;
MakeOrbitConstants(g, burnNode.Orbit, false, "Burn Orbit");
drawPatchedConic(g, burnNode.Orbit, 0, 360, burnOrbitColor[(i + s) % 3]);
drawPeriapse(g, burnNode.Orbit);
drawApoapse(g, burnNode.Orbit);
drawAscDescNodes(g, burnNode.Orbit);
}
}
}
}
}
public void updateChartData(object sender, EventArgs e)
{
if (connected && krpc.CurrentGameScene == KRPC.Client.Services.KRPC.GameScene.Flight && graphStreams != null)
{
double altitude = graphStreams.GetData(DataType.flight_meanAltitude);
double apoapsis = graphStreams.GetData(DataType.orbit_apoapsisAltitude);
double periapsis = graphStreams.GetData(DataType.orbit_periapsisAltitude);
double speed = graphStreams.GetData(DataType.orbit_speed);
double MET = graphStreams.GetData(DataType.vessel_MET);
double elevation = graphStreams.GetData(DataType.flight_elevation);
float gee = graphStreams.GetData(DataType.flight_gForce);
float dynPress = graphStreams.GetData(DataType.flight_dynamicPressure);
float roll = graphStreams.GetData(DataType.flight_inertial_roll);
float pitch = graphStreams.GetData(DataType.flight_inertial_pitch);
Tuple <double, double, double> prograde = graphStreams.GetData(DataType.flight_prograde);
float aoa = graphStreams.GetData(DataType.flight_angleOfAttack);
float yaw = graphStreams.GetData(DataType.flight_inertial_yaw);
double tapo = graphStreams.GetData(DataType.orbit_timeToApoapsis);
double lat = graphStreams.GetData(DataType.flight_map_latitude);
double lon = graphStreams.GetData(DataType.flight_map_longitude);
// Limit taop to 120 minutes
if (tapo > 120 * 60)
{
tapo = 120 * 60;
}
// Calculate Range
double RANGE = 0;
if (originLat != null)
{
float R = graphStreams.GetData(DataType.body_radius); // body radius in metres
double lat1 = (double)originLat;
double lon1 = originLon;
double rad1 = Helper.deg2rad(lat);
double rad2 = Helper.deg2rad(lat1);
double deltaRad = Helper.deg2rad((lat1 - lat));
double deltaLambda = Helper.deg2rad((lon1 - lon));
double a = Math.Sin(deltaRad / 2) * Math.Sin(deltaRad / 2) +
Math.Cos(rad1) * Math.Cos(rad2) *
Math.Sin(deltaLambda / 2) * Math.Sin(deltaLambda / 2);
double c = 2 * Math.Atan2(Math.Sqrt(a), Math.Sqrt(1 - a));
RANGE = R * c;
}
addValueToChart(chartData["lat"], MET, lat, 10000);
addValueToChart(chartData["lon"], MET, lon, 10000);
// HDOT
if (prevAlt.Key != 0)
{
double HDOT = (double)((altitude - prevAlt.Value) / (MET - prevAlt.Key));
addValueToChart(chartData["hdot"], MET, HDOT, 3000);
addValueToChart(chartData["hhdot"], HDOT, altitude, 3000);
}
prevAlt = new KeyValuePair <double, double?>(MET, altitude);
// FLIGHT PATH ANGLE
// Flight path angle is the angle between the velocity vector (prograde), and the local horizon.
// Surface direction unit length
double surf = Math.Sqrt(Math.Pow(prograde.Item2, 2) + Math.Pow(prograde.Item3, 2));
// Flight path angle
double fpa;
if (surf < 0.00001)
{
fpa = 90;
}
else
{
fpa = Helper.rad2deg(Math.Atan(prograde.Item1 / surf));
}
addValueToChart(chartData["FlightangleVelocity"], speed, fpa, 3000);
addValueToChart(chartData["geeVel"], speed, gee, 3000);
addValueToChart(chartData["altitudeTime"], MET, altitude);
addValueToChart(chartData["apoapsisTime"], MET, apoapsis);
addValueToChart(chartData["periapsisTime"], (int)MET, periapsis);
addValueToChart(chartData["geeTime"], (int)MET, gee);
addValueToChart(chartData["terrainTime"], (int)MET, elevation);
addValueToChart(chartData["dynPresTime"], (int)MET, dynPress);
addValueToChart(chartData["rollTime"], (int)MET, roll);
addValueToChart(chartData["pitchTime"], (int)MET, pitch);
addValueToChart(chartData["yawTime"], (int)MET, yaw);
addValueToChart(chartData["altitudeSpeed"], (int)speed, altitude, 3000);
addValueToChart(chartData["timeToApoSpeed"], (int)speed, tapo, 3000);
addValueToChart(chartData["altitudeRange"], (int)RANGE, altitude, 3000);
}
}
