public SimulationState(CelestialBody planet, double departureAltitude, Vector3d forward)
{
this.planet = planet;
this.forward = forward;
x = 0;
y = planet.Radius + departureAltitude;
vx = planet.rotates ? (y * 2 * Math.PI / planet.rotationPeriod) : 0;
vy = 0;
throttle = 1.0f;
activeEngines = new List <EngineWrapper>();
availableNodes = new Dictionary <Part, Node>();
ascentPath = new DefaultAscentPath(planet);
}
public SimulationState(CelestialBody planet, double departureAltitude, Vector3d forward)
{
this.planet = planet;
this.forward = forward;
x = 0;
y = planet.Radius + departureAltitude;
vx = planet.rotates ? (y * 2 * Math.PI / planet.rotationPeriod) : 0;
vy = 0;
throttle = 1.0f;
activeEngines = new List<EngineWrapper>();
availableNodes = new Dictionary<Part, Node>();
ascentPath = new DefaultAscentPath(planet);
}
