int main (void)
{
int dir, oppDir;
die[CURR] = 0;
die[NORTH] = 3;
die[SOUTH] = 2;
die[EAST] = 1;
die[WEST] = 4;
die[CURR] = 2;
die[NORTH] = 0;
die[SOUTH] = 5;
die[EAST] = 4;
die[WEST] = 1;
dir = NORTH;
oppDir = SOUTH;
outState();
die[dir] = die[CURR];
die[CURR] = die[oppDir];
die[oppDir] = 5 - die[dir];
outState();
die[dir] = die[CURR];
die[CURR] = die[oppDir];
die[oppDir] = 5 - die[dir];
outState();
die[dir] = die[CURR];
die[CURR] = die[oppDir];
die[oppDir] = 5 - die[dir];
outState();
die[dir] = die[CURR];
die[CURR] = die[oppDir];
die[oppDir] = 5 - die[dir];
outState();
/*
curr = $80 ;
dir = $85 ;
ldx CURR ;
lda curr, x ;
ldx dir ; die[dir] = die[CURR];
sta curr, x ;
ldx oppDir ;
lda arrayaddr, x ;
ldx curr ; die[curr] = die[oppdir]
sta arrayaddr, x ;
ldx dir
lda #5
sec
sbc curr,x
ldx oppDir
sta curr, x
*/
return 0;
}
RealArray PhysicalMeasurement::IonosphereCorrection(Real freq, Rvector3 r1, Rvector3 r2, Real epoch)
{
RealArray ionoCorrection;
if (ionosphere != NULL)
{
// 1. Set wave length:
Real wavelength = GmatPhysicalConstants::SPEED_OF_LIGHT_VACUUM / (freq*1.0e6); // unit: meter
ionosphere->SetWaveLength(wavelength);
// 2. Set time:
ionosphere->SetTime(epoch); // unit: Julian day
// 3. Set station and spacecraft positions:
GroundstationInterface* gs = (GroundstationInterface*)participants[0];
CoordinateSystem* cs = gs->GetBodyFixedCoordinateSystem();
Rvector inState(6, 1.0, 2.0, 3.0, 4.0, 5.0, 6.0);
Rvector outState(6, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0);
// Rvector bogusOut = cs->FromMJ2000Eq(epoch, bogusIn, true);
// Rmatrix33 R_g_j2k = cs->GetLastRotationMatrix().Transpose();
CoordinateConverter* cv = new CoordinateConverter();
A1Mjd time(epoch);
CoordinateSystem* fk5cs = Moderator::Instance()->GetCoordinateSystem("EarthMJ2000Eq");
cv->Convert(time, inState, cs, outState, fk5cs); // convert EarthFK5 coordinate system to EarthBodyFixed coordinate system
Rmatrix33 R_g_j2k = cv->GetLastRotationMatrix().Transpose();
// MessageInterface::ShowMessage("[ %f %f %f\n", R_g_j2k.GetElement(0,0), R_g_j2k.GetElement(0,1), R_g_j2k.GetElement(0,2));
// MessageInterface::ShowMessage(" %f %f %f\n", R_g_j2k.GetElement(1,0), R_g_j2k.GetElement(1,1), R_g_j2k.GetElement(1,2));
// MessageInterface::ShowMessage(" %f %f %f]\n", R_g_j2k.GetElement(2,0), R_g_j2k.GetElement(2,1), R_g_j2k.GetElement(2,2));
ionosphere->SetStationPosition(R_g_j2k*r1); // unit: km
ionosphere->SetSpacecraftPosition(R_g_j2k*r2); // unit: km
// 4. Set earth radius:
SpacePoint* earth = (SpacePoint*)gs->GetRefObject(Gmat::SPACE_POINT, "Earth");
Real earthRadius = earth->GetRealParameter("EquatorialRadius");
ionosphere->SetEarthRadius(earthRadius); // unit: km
#ifdef DEBUG_IONOSPHERE_MEDIA_CORRECTION
MessageInterface::ShowMessage(" *Run Ionosphere media correction for:\n");
MessageInterface::ShowMessage(" +Earth radius = %lf km\n", earthRadius);
MessageInterface::ShowMessage(" +Wave length = %.12lf m\n", wavelength);
MessageInterface::ShowMessage(" +Time = %.12lf\n", epoch);
MessageInterface::ShowMessage(" +Station location in Earth body fixed coordinate system (km):\n"
" (%s)", (R_g_j2k*r1).ToString().c_str());
MessageInterface::ShowMessage(" +Spacecraft location in Earth body fixed coordinate system (km):\n"
" (%s)", (R_g_j2k*r2).ToString().c_str());
#endif
// 5. Run ionosphere correction:
ionoCorrection = ionosphere->Correction();
Real rangeCorrection = ionoCorrection[0]*GmatMathConstants::M_TO_KM; // unit: meter
#ifdef DEBUG_IONOSPHERE_MEDIA_CORRECTION
MessageInterface::ShowMessage(" *Ionosphere media correction result:\n");
MessageInterface::ShowMessage(" +Range correction = %.12lf m\n", rangeCorrection*GmatMathConstants::KM_TO_M);
#endif
}
else
{
ionoCorrection.push_back(0.0);
ionoCorrection.push_back(0.0);
ionoCorrection.push_back(0.0);
}
return ionoCorrection;
}