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Clean up

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This commit is contained in:
Nick 2022-04-18 00:11:26 -04:00
parent 860ffd2c95
commit 6156255cf5
1 changed files with 3 additions and 39 deletions
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42
NewHorizons/Components/Orbital/OrbitalParameters.cs
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@ -61,6 +61,8 @@ namespace NewHorizons.Components.Orbital
var r_a = semiMajorAxis * (1 + eccentricity);
float v;
// For linear
if(primaryGravity.Power == 1)
{
// Have to deal with a limit
@ -76,6 +78,7 @@ namespace NewHorizons.Components.Orbital
v = Mathf.Sqrt(v2);
}
}
// For inverseSquare
else
{
v = Mathf.Sqrt(G * primaryMass * ((2f / r) - (1f / semiMajorAxis)));
@ -100,45 +103,6 @@ namespace NewHorizons.Components.Orbital
orbitalParameters.InitialPosition = R1 * R2 * R3 * pos;
orbitalParameters.InitialVelocity = R1 * R2 * R3 * vel;
Logger.Log($"POSITION: {orbitalParameters.InitialPosition}, {orbitalParameters.InitialVelocity}, {n_p}, {n_v}, {primaryMass}");
/*
var x = r * (Mathf.Cos(la) * Mathf.Cos(ap + f) - Mathf.Sin(la) * Mathf.Sin(ap + f) * Mathf.Cos(i));
var y = r * (Mathf.Sin(la) * Mathf.Cos(ap + f) + Mathf.Cos(la) * Mathf.Sin(ap + f) * Mathf.Cos(i));
var z = r * (Mathf.Sin(i) * Mathf.Sin(ap + f));
orbitalParameters.InitialPosition = new Vector3(x, y, z);
// Velocity
var coefficient = h * eccentricity * Mathf.Sin(f) / (r * p);
var vx = x * coefficient - (h / r) * (Mathf.Cos(la) * Mathf.Sin(ap + f) + Mathf.Sin(la) * Mathf.Cos(ap + f) * Mathf.Cos(i));
var vy = y * coefficient - (h / r) * (Mathf.Sin(la) * Mathf.Sin(ap + f) - Mathf.Cos(la) * Mathf.Cos(ap + f) * Mathf.Cos(i));
var vz = z * coefficient + (h / r) * (Mathf.Sin(i) * Mathf.Cos(ap + f));
orbitalParameters.InitialVelocity = new Vector3(vx, vy, vz);
*/
/*
// Where x points towards the periapsis
var ox = semiMajorAxis * Mathf.Cos(f);
var oy = semiMinorAxis * Mathf.Sin(f);
var o = new Vector3(ox, 0, oy);
var mu = GravityVolume.GRAVITATIONAL_CONSTANT * primaryMass;
var r = o.magnitude;
var o_dot_coeff = Mathf.Sqrt(mu * ((2/r) - (1/semiMajorAxis)));
var ox_dot = o_dot_coeff * -Mathf.Sin(eccentricAnomaly);
var oy_dot = o_dot_coeff * Mathf.Cos(eccentricAnomaly);
var o_dot = new Vector3(ox_dot, 0, oy_dot);
// Do some rotations
var R1 = Quaternion.AngleAxis(Mathf.Rad2Deg * -longitudeOfAscendingNode, Vector3.up);
var R2 = Quaternion.AngleAxis(Mathf.Rad2Deg * -inclination, Vector3.forward);
var R3 = Quaternion.AngleAxis(Mathf.Rad2Deg * -argumentOfPeriapsis, Vector3.up);
orbitalParameters.InitialPosition = R1 * R2 * R3 * o;
orbitalParameters.InitialVelocity = R1 * R2 * R3 * o_dot;
*/
return orbitalParameters;
}
}