private void DoSimulation(SimData simData, double fTimeDelta)
{
simData.ElapsedSeconds += fTimeDelta * simData.SimulationSpeed;
double time = simData.ElapsedSeconds;
simData.CurrentEarthRotation = (float)(time % simData.RealEarthPeriode / simData.RealEarthPeriode * 2 * Math.PI);
for (int i = 0; i < simData.Satellites.Length; i++)
{
var satellite = simData.Satellites[i];
if (satellite.IsVisible)
{
CalculateSatelitePosition(satellite, time);
}
}
}
//
// simulation stuff
//
private void InitSimulationData(SimData simData)
{
simData.CurrentEarthRotation = 0;
simData.SimulationSpeed = 1000.0f;
simData.SimulationSizeScalar = 0.001f;
var satelites = new List <SatelliteSimData>();
var satDataStream = Utils.OpenEmbeddedResource("vissatellite.simdata.UCS_Satellite_Database_9-1-2017.txt");
var streamReader = new System.IO.StreamReader(satDataStream);
streamReader.ReadLine();
string line;
var rand = new Random();
while ((line = streamReader.ReadLine()) != null)
{
string[] elements = line.Split('\t');
var satelite = new SatelliteSimData();
satelite.IsVisible = true;
satelite.IsSelected = false;
satelite.Name = elements[0];
switch (elements[4])
{
case "Civil":
satelite.Users = SatelliteUsers.CIVIL;
break;
case "Military":
satelite.Users = SatelliteUsers.MILITARY;
break;
case "Government":
satelite.Users = SatelliteUsers.GOVERNMENT;
break;
case "Commercial":
satelite.Users = SatelliteUsers.COMMERCIAL;
break;
default:
satelite.Users = SatelliteUsers.MIXED;
break;
}
switch (elements[7])
{
case "LEO":
satelite.ClassOfOrbit = OrbitType.LEO;
break;
case "MEO":
satelite.ClassOfOrbit = OrbitType.MEO;
break;
case "GEO":
satelite.ClassOfOrbit = OrbitType.GEO;
break;
case "Elliptical":
satelite.ClassOfOrbit = OrbitType.ELLIPTICAL;
break;
}
//Read all the data we have
if (!elements[9].Equals(""))
{
satelite.LongitudeOfGeo = float.Parse(elements[9], CultureInfo.InvariantCulture);
}
satelite.Perigee = float.Parse(elements[10].Replace("\"", "").Replace(",", ""));
satelite.Apogee = float.Parse(elements[11].Replace("\"", "").Replace(",", ""));
satelite.Eccentricity = float.Parse(elements[12], CultureInfo.InvariantCulture);
satelite.Inclenation = float.Parse(elements[13], CultureInfo.InvariantCulture) * (float)Math.PI / 180;
satelite.Periode = float.Parse(elements[14].Replace("\"", ""), CultureInfo.InvariantCulture) * 60;
//Calculated what we need
satelite.SemiMajorAxis = (float)(satelite.Apogee + satelite.Perigee + simData.RealEarthDiameter) / 2;
//Generate random values for needed object elements that are not in the dataset
satelite.LongitudeOfAscendingNode = (float)(rand.NextDouble() * Math.PI * 2);
satelite.ArgumentOfPeriapsis = (float)(rand.NextDouble() * Math.PI * 2);
satelite.Position = new Vector3(0, 0, 0);
satelites.Add(satelite);
}
simData.Satellites = satelites.ToArray();
}
