public double execute(double in) throws DMLRuntimeException {
switch (bFunc) {
case SIN:
return FASTMATH ? FastMath.sin(in) : Math.sin(in);
case COS:
return FASTMATH ? FastMath.cos(in) : Math.cos(in);
case TAN:
return FASTMATH ? FastMath.tan(in) : Math.tan(in);
case ASIN:
return FASTMATH ? FastMath.asin(in) : Math.asin(in);
case ACOS:
return FASTMATH ? FastMath.acos(in) : Math.acos(in);
case ATAN:
return Math.atan(in); // faster in Math
case CEIL:
return FASTMATH ? FastMath.ceil(in) : Math.ceil(in);
case FLOOR:
return FASTMATH ? FastMath.floor(in) : Math.floor(in);
case LOG:
return FASTMATH ? FastMath.log(in) : Math.log(in);
case LOG_NZ:
return (in == 0) ? 0 : FASTMATH ? FastMath.log(in) : Math.log(in);
case ABS:
return Math.abs(in); // no need for FastMath
case SIGN:
return FASTMATH ? FastMath.signum(in) : Math.signum(in);
case SQRT:
return Math.sqrt(in); // faster in Math
case EXP:
return FASTMATH ? FastMath.exp(in) : Math.exp(in);
case ROUND:
return Math.round(in); // no need for FastMath
case PLOGP:
if (in == 0.0) return 0.0;
else if (in < 0) return Double.NaN;
else return (in * (FASTMATH ? FastMath.log(in) : Math.log(in)));
case SPROP:
// sample proportion: P*(1-P)
return in * (1 - in);
case SIGMOID:
// sigmoid: 1/(1+exp(-x))
return FASTMATH ? 1 / (1 + FastMath.exp(-in)) : 1 / (1 + Math.exp(-in));
case SELP:
// select positive: x*(x>0)
return (in > 0) ? in : 0;
default:
throw new DMLRuntimeException("Builtin.execute(): Unknown operation: " + bFunc);
}
}
/**
* Get the useful angles for eclipse computation.
*
* @param position the satellite's position in the selected frame.
* @param frame in which is defined the position
* @param date the date
* @return the 3 angles {(satCentral, satSun), Central body apparent radius, Sun apparent radius}
* @exception OrekitException if the trajectory is inside the Earth
*/
private double[] getEclipseAngles(
final Vector3D position, final Frame frame, final AbsoluteDate date) throws OrekitException {
final double[] angle = new double[3];
final Vector3D satSunVector =
sun.getPVCoordinates(date, frame).getPosition().subtract(position);
// Sat-Sun / Sat-CentralBody angle
angle[0] = Vector3D.angle(satSunVector, position.negate());
// Central body apparent radius
final double r = position.getNorm();
if (r <= equatorialRadius) {
throw new OrekitException(OrekitMessages.TRAJECTORY_INSIDE_BRILLOUIN_SPHERE, r);
}
angle[1] = FastMath.asin(equatorialRadius / r);
// Sun apparent radius
angle[2] = FastMath.asin(Constants.SUN_RADIUS / satSunVector.getNorm());
return angle;
}