private void LoadSolarSystem()
{
_sun = new Sun();
var mercury = new Mercury();
var venus = new Venus();
var earth = new Earth();
var moon = new Moon(earth.Position, earth.Velocity);
var mars = new Mars();
var jupiter = new Jupiter();
var europa = new Europa(jupiter.Position, jupiter.Velocity);
var saturn = new Saturn();
_massiveBodies = new List <IMassiveBody>
{
_sun, mercury, venus, earth, moon, mars, jupiter, europa, saturn
};
ResolveMassiveBodyParents();
_spaceCrafts = new List <ISpaceCraft>();
_structures = new List <StructureBase>();
MissionConfig primaryMission = MissionConfig.Load(ProfilePaths[0]);
_originTime = primaryMission.GetLaunchDate();
OrbitHelper.SimulateToTime(_massiveBodies, _originTime, 300);
// Load missions
for (int i = 0; i < ProfilePaths.Count; i++)
{
MissionConfig missionConfig = MissionConfig.Load(ProfilePaths[i]);
IMassiveBody targetPlanet = LocatePlanet(missionConfig.ParentPlanet);
double launchAngle = targetPlanet.GetSurfaceAngle(_originTime, _sun);
_spaceCrafts.AddRange(SpacecraftFactory.BuildSpaceCraft(targetPlanet, launchAngle, missionConfig, ProfilePaths[i]));
_structures.AddRange(StructureFactory.Load(targetPlanet, launchAngle, ProfilePaths[i]));
}
// Initialize the spacecraft controllers
foreach (ISpaceCraft spaceCraft in _spaceCrafts)
{
spaceCraft.InitializeController(_eventManager);
}
_gravitationalBodies = new List <IGravitationalBody>
{
_sun, mercury, venus, earth, moon, mars, jupiter, europa, saturn
};
foreach (ISpaceCraft spaceCraft in _spaceCrafts)
{
_gravitationalBodies.Add(spaceCraft);
}
// Target the spacecraft
_targetIndex = _gravitationalBodies.IndexOf(_spaceCrafts.FirstOrDefault());
ResolveSpaceCraftParents();
}
private void LoadSolarSystem()
{
_sun = new Sun();
var mercury = new Mercury();
var venus = new Venus();
var earth = new Earth();
var moon = new Moon(earth.Position, earth.Velocity);
var mars = new Mars();
var jupiter = new Jupiter();
var callisto = new Callisto(jupiter.Position, jupiter.Velocity);
var europa = new Europa(jupiter.Position, jupiter.Velocity);
var ganymede = new Ganymede(jupiter.Position, jupiter.Velocity);
var io = new Io(jupiter.Position, jupiter.Velocity);
var saturn = new Saturn();
_massiveBodies = new List <IMassiveBody>
{
_sun, mercury, venus, earth, moon, mars, jupiter, callisto, europa, ganymede, io, saturn
};
ResolveMassiveBodyParents();
_gravitationalBodies = new List <IGravitationalBody>
{
_sun, mercury, venus, earth, moon, mars, jupiter, callisto, europa, ganymede, io, saturn
};
_spaceCraftManager = new SpaceCraftManager(_gravitationalBodies);
_structures = new List <StructureBase>();
MissionConfig primaryMission = MissionConfig.Load(ProfilePaths[0]);
_originTime = primaryMission.GetLaunchDate();
UpdateLoadingPercentage(20);
OrbitHelper.SimulateToTime(_massiveBodies, _originTime, 300, UpdateLoadingPercentage);
UpdateLoadingPercentage(80);
// Load missions
for (int i = 0; i < ProfilePaths.Count; i++)
{
MissionConfig missionConfig = MissionConfig.Load(ProfilePaths[i]);
if (missionConfig.ClockDelay > _clockDelay)
{
_clockDelay = missionConfig.ClockDelay;
}
IMassiveBody targetPlanet = LocatePlanet(missionConfig.ParentPlanet);
// Get the launch angle relative to the sun for the given time at the origin
// and offset each vehicle by a certain amount on the surface
double launchAngle = targetPlanet.GetSurfaceAngle(_originTime, _sun) + i * 0.00002;
_spaceCraftManager.Add(SpacecraftFactory.BuildSpaceCraft(targetPlanet, launchAngle, missionConfig, ProfilePaths[i]));
_structures.AddRange(StructureFactory.Load(targetPlanet, launchAngle, ProfilePaths[i]));
}
_spaceCraftManager.Initialize(_eventManager, _clockDelay);
// Target the spacecraft
_targetIndex = _gravitationalBodies.IndexOf(_spaceCraftManager.First);
_spaceCraftManager.ResolveGravitionalParents(_massiveBodies);
UpdateLoadingPercentage(90);
}
