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Updated of SGP4.cpp exceptions

feature/19
Daniel Warner 2012-01-04 22:23:10 +00:00
parent 0294aa43d7
commit daf729f8f4
1 changed files with 38 additions and 10 deletions
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48
libsgp4/SGP4.cpp
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@ -282,9 +282,25 @@ Eci SGP4::FindPositionSDP4(const Julian& dt, double tsince) const
xl = xmam + omgadf + xnode;
omega = omgadf;
if (e < 0.0 || e > 1.0)
if (a < 1.0)
{
throw SatelliteException("Error: #3 (e < 0.0 || e > 1.0)");
throw SatelliteException("Error: (a < 1.0)");
}
/*
* fix tolerance for error recognition
*/
if (e <= -0.001)
{
throw SatelliteException("Error: (e <= -0.001)");
}
else if (e < 1.0e-6)
{
e = 1.0e-6;
}
else if (e > (1.0 - 1.0e-6))
{
e = 1.0 - 1.0e-6;
}
/*
@ -372,20 +388,26 @@ Eci SGP4::FindPositionSGP4(const Julian& dt, double tsince) const
e = elements_.Eccentricity() - tempe;
xl = xmp + omega + xnode + elements_.RecoveredMeanMotion() * templ;
if (a < 1.0)
{
throw SatelliteException("Error: (a < 1.0)");
}
/*
* fix tolerance for error recognition
*/
if (e >= 1.0 || e < -0.001)
if (e <= -0.001)
{
throw SatelliteException("Error: #1 (e >= 1.0 || e < -0.001)");
throw SatelliteException("Error: (e <= -0.001)");
}
/*
* fix tolerance to avoid a divide by zero
*/
if (e < 1.0e-6)
else if (e < 1.0e-6)
{
e = 1.0e-6;
}
else if (e > (1.0 - 1.0e-6))
{
e = 1.0 - 1.0e-6;
}
/*
* using calculated values, find position and velocity
@ -418,6 +440,11 @@ Eci SGP4::CalculateFinalPositionVelocity(const Julian& dt, const double& e,
const double ayn = e * sin(omega) + aynl;
const double elsq = axn * axn + ayn * ayn;
if (elsq >= 1.0)
{
throw SatelliteException("Error: (elsq >= 1.0)");
}
/*
* solve keplers equation
* - solve using Newton-Raphson root solving
@ -496,7 +523,8 @@ Eci SGP4::CalculateFinalPositionVelocity(const Julian& dt, const double& e,
if (pl < 0.0)
{
throw SatelliteException("Error: #4 (pl < 0.0)");
//TODO:
throw SatelliteException("Error: (pl < 0.0)");
}
const double r = a * (1.0 - ecose);
@ -528,7 +556,7 @@ Eci SGP4::CalculateFinalPositionVelocity(const Julian& dt, const double& e,
if (rk < 1.0)
{
throw SatelliteException("Error: #6 Satellite decayed (rk < 1.0)");
throw SatelliteException("Error: Satellite decayed (rk < 1.0)");
}
/*