public static List <object> CSE(Vector3d r0, Vector3d v0, double tgo)
{
Connection conn = Globals.Connection.Connection;
double mu = conn.SpaceCenter().ActiveVessel.Orbit.Body.GravitationalParameter;
return(CSER.CSE(r0, v0, tgo, mu, 0, 0.000000005));
}
public static List <object> Iterate(Vehicle vehicle, Target target, VesselState state, VesselState previous)
{
var gamma = target.Angle;
var iy = target.Normal;
var rdval = target.Radius;
var vdval = target.Velocity;
var t = state.Time;
var m = state.Mass.Value;
var r = state.Radius;
var v = state.Velocity;
var cser = previous.Cse;
var rbias = previous.Rbias;
var rd = previous.Rd;
var rgrav = previous.Rgrav;
var tp = previous.Time;
var vprev = previous.Velocity;
var vgo = previous.Vgo;
var n = vehicle.Stages.Count;
var SM = new List <double>();
var aL = new List <double>();
var md = new List <double>();
var ve = new List <double>();
var fT = new List <double>();
var aT = new List <double>();
var tu = new List <double>();
var tb = new List <double>();
for (int i = 0; i < n; i++)
{
Stage stg = vehicle.Stages[i];
var pack = stg.GetThrust();
SM.Add(stg.Mode);
aL.Add(stg.GLim * Constants.G0);
fT.Add(pack[0]);
md.Add(pack[1]);
ve.Add(pack[2] * Constants.G0);
aT.Add(fT[i] / stg.MassTotal);
tu.Add(ve[i] / aT[i]);
tb.Add(stg.MaxT);
}
var dt = t - tp;
var dvsensed = Vector3d.Subtract(v, vprev);
vgo = Vector3d.Subtract(vgo, dvsensed);
tb[0] = tb[0] - previous.Tb;
if (SM[0] == 1)
{
aT[0] = fT[0] / m;
}
else if (SM[0] == 2)
{
aT[0] = aL[0];
}
tu[0] = ve[0] / aT[0];
var L = 0d;
var Li = new List <double>();
for (int i = 0; i < n - 1; i++)
{
if (SM[i] == 1)
{
Li.Add(ve[i] * Math.Log(tu[i] / (tu[i] - tb[i])));
}
else if (SM[i] == 2)
{
Li.Add(aL[i] * tb[i]);
}
else
{
Li.Add(0);
}
L = Li[i];
if (L > vgo.Magnitude())
{
var veh = vehicle;
veh.Stages.RemoveAt(veh.Stages.Count - 1);
return(UPFG.Iterate(veh, target, state, previous));
}
}
Li.Add(vgo.Magnitude() - L);
var tgoi = new List <double>();
for (int i = 0; i < n; i++)
{
if (SM[i] == 1)
{
tb[i] = tu[i] * (1 - Math.Pow(Math.E, (-Li[i] / ve[i])));
}
else if (SM[i] == 2)
{
tb[i] = Li[i] / aL[i];
}
if (i == 0)
{
tgoi.Add(tb[i]);
}
else
{
tgoi.Add(tgoi[i - 1] + tb[i]);
}
}
var L1 = Li[0];
var tgo = tgoi[n - 1];
L = 0d;
var J = 0d;
var S = 0d;
var Q = 0d;
var H = 0d;
var P = 0d;
var Ji = new List <double>();
var Si = new List <double>();
var Qi = new List <double>();
var Pi = new List <double>();
var tgoi1 = 0d;
for (int i = 0; i < n; i++)
{
if (i > 0)
{
tgoi1 = tgoi[i - 1];
}
if (SM[i] == 1)
{
Ji.Add(tu[i] * Li[i] - ve[i] * tb[i]);
Si.Add(-Ji[i] + tb[i] * Li[i]);
Qi.Add(Si[i] * (tu[i] + tgoi1) - 0.5 * ve[i] * Math.Pow(tb[i], 2));
Pi.Add(Qi[i] * (tu[i] + tgoi1) - 0.5 * ve[i] * Math.Pow(tb[i], 2) * (tb[i] / 3 + tgoi1));
}
else if (SM[i] == 2)
{
Ji.Add(0.5 * Li[i] * tb[i]);
Si.Add(Ji[i]);
Qi.Add(Si[i] * (tb[i] / 3 + tgoi1));
Pi.Add((1 / 6) * Si[i] * (Math.Pow(tgoi[i], 2) + 2 * tgoi[i] * tgoi1 + 3 * Math.Pow(tgoi1, 2)));
}
Ji[i] = Ji[i] + Li[i] * tgoi1;
Si[i] = Si[i] + L * tb[i];
Qi[i] = Qi[i] + J * tb[i];
Pi[i] = Pi[i] + H * tb[i];
L += Li[i];
J += Ji[i];
S += Si[i];
Q += Qi[i];
P += Pi[i];
H = J * tgoi[i] - Q;
}
var lambda = Vector3d.Normalize(vgo);
if (previous.Tgo > 0)
{
rgrav = Vector3d.Multiply(rgrav, Math.Pow((tgo / previous.Tgo), 2));
}
var rgo = Vector3d.Subtract(
rd,
Vector3d.Add(
Vector3d.Multiply(
Vector3d.Add(r, v),
tgo
),
rgrav
)
);
var iz = Vector3d.Normalize(Vector3d.Cross(rd, iy));
var rgoxy = Vector3d.Dot(Vector3d.Subtract(rgo, Vector3d.Dot(iz, rgo)), iz);
var rgoz = Vector3d.Divide(Vector3d.Subtract(Vector3d.Multiply(lambda, rgoxy), S),
Vector3d.Dot(lambda, iz));
rgo = Vector3d.Add(Vector3d.Add(rgoz, rgoxy), Vector3d.Add(iz, rbias));
var lambdade = Q - S * J / L;
var lambdadot = Vector3d.Divide(Vector3d.Subtract(rgo, Vector3d.Multiply(lambda, S)), lambdade);
var iF_ = Vector3d.Subtract(lambda, Vector3d.Multiply(lambdadot, J / L));
iF_ = Vector3d.Normalize(iF_);
var phi = Math.Acos(Vector3d.Dot(iF_, lambda) / (iF_.Magnitude() * lambda.Magnitude()));
var phidot = -phi * L / J;
var vthrust = Vector3d.Multiply(lambda,
L - 0.5 * L * Math.Pow(phi, 2) - J * phi * phidot - 0.5 * Math.Pow(phidot, 2));
var rthrst = S - 0.5 * S * Math.Pow(phi, 2) - Q * phi * phidot - 0.5 * P * Math.Pow(phidot, 2);
var rthrust = Vector3d.Subtract(
Vector3d.Multiply(lambda, rthrst),
Vector3d.Multiply(
Vector3d.Normalize(lambda),
(S * phi + Q * phidot)
)
);
var vbias = Vector3d.Subtract(vgo, vthrust);
var rbs = Vector3d.Subtract(rgo, rthrst);
var _up = Vector3d.Normalize(r);
var _east = Vector3d.Normalize(Vector3d.Cross(
new Vector3d(0, 0, 1),
_up
));
var pitch = Math.Acos(Vector3d.Dot(iF_, _up) / (iF_.Magnitude() * _up.Magnitude()));
var inplane = Vector3d.Subtract(
iF_,
Vector3d.Multiply(_up,
Vector3d.Dot(iF_, _up) / Vector3d.Dot(_up, _up)
));
var yaw = Math.Acos(Vector3d.Dot(inplane, _east) / (inplane.Magnitude() * _east.Magnitude()));
var tangent = Vector3d.Cross(_up, _east);
if (Vector3d.Dot(inplane, tangent) < 0)
{
yaw = -yaw;
}
var rc1 = Vector3d.Subtract(Vector3d.Subtract(
r,
Vector3d.Multiply(rthrust, 0.1)
),
Vector3d.Multiply(
vthrust,
tgo / 30
));
var vc1 = Vector3d.Subtract(Vector3d.Add(
Vector3d.Divide(Vector3d.Multiply(rthrust, 1.2), tgo),
v
),
Vector3d.Multiply(vthrust, 0.1));
var pck = CSER.CSE(rc1, vc1, tgo);
cser = (Dictionary <string, object>)pck[2];
var rgrv = Vector3d.Subtract(
(Vector3d)pck[0],
Vector3d.Subtract(
rc1,
Vector3d.Multiply(vc1, tgo)
)
);
var vgrv = Vector3d.Subtract(
(Vector3d)pck[1],
vc1
);
var rp = Vector3d.Add(
r,
Vector3d.Add(
Vector3d.Multiply(v, tgo),
Vector3d.Add(rgrv, rthrust)
)
);
rp = Vector3d.Subtract(
rp,
Vector3d.Multiply(
iy,
Vector3d.Dot(rp, iy)
)
);
rd = Vector3d.Multiply(
Vector3d.Normalize(rp),
rdval
);
var ix = Vector3d.Normalize(rd);
iz = Vector3d.Cross(ix, iy);
var vv1 = new Vector3d(ix.X, iy.X, iz.Z);
var vv2 = new Vector3d(ix.Y, iy.Y, iz.Y);
var vv3 = new Vector3d(ix.Z, iy.Z, iz.Z);
var vop = new Vector3d(Math.Sin(gamma), 0, Math.Cos(gamma));
var vd = new Vector3d(
Vector3d.Dot(vv1, vop),
Vector3d.Dot(vv2, vop),
Vector3d.Dot(vv3, vop)
);
vgo = Vector3d.Add(Vector3d.Subtract(
vd,
Vector3d.Subtract(
vgrv,
v
)
),
vbias
);
// var current = new VesselState(cser);
var current = new VesselState(t, null, null, v, cser, rbias, rd, rgrv, vgo, previous.Tb + dt, tgo);
var guidance = new Guidance(iF_, pitch, yaw, 0, 0, tgo);
return(new List <object>
{
current,
guidance,
dt
});
}
