//------------------------------------------------------------------------------
// int main(int argc, char *argv[])
//------------------------------------------------------------------------------
int main(int argc, char *argv[])
{
cout << "=-=-=-=-=-=-= TEST coordinate system ....." << endl;
cout << " ------ number of objects instantiated = " << GmatBase::GetInstanceCount() << endl;
cout.setf(ios::fixed);
cout.precision(16);
std::string eopFileName = "/GMAT/dev/datafiles/EOPFiles/eopc04.62-now";
std::string nutFileName = "/GMAT/dev/datafiles/ITRF/NUTATION.DAT";
std::string planFileName = "/GMAT/dev/datafiles/ITRF/NUT85.DAT";
std::string SLPFileName = "/GMAT/dev/datafiles/mac/DBS_mn2000.dat";
std::string DEFileName = "/GMAT/dev/datafiles/DEascii/macp1941.405";
std::string LeapFileName = "/GMAT/dev/datafiles/tai-utcFiles/tai-utc.dat";
cout << "\n==> First, test the AxisSystemFactory <==" << endl;
AxisSystemFactory *asf = new AxisSystemFactory();
cout << "AxisSystemFactory created .........." << endl;
cout << " ------ number of objects instantiated = " << GmatBase::GetInstanceCount() << endl;
std::string
AXES_TYPE[13] =
{
"MJ2000Eq",
"MJ2000Ec",
"TOEEq",
"TOEEc",
"MOEEq",
"MOEEc",
"TODEq",
"TODEc",
"MODEq",
"MODEc",
"ObjectReferenced",
"Equator",
"BodyFixed",
};
AxisSystem *as;
MJ2000EqAxes* mj;
MJ2000EqAxes* mj2;
//MJ2000EcAxes* mj2;
std::string tmpStr = "";
//for (int i = 0; i < 13 ; i++)
for (int i = 0; i < 2 ; i++) // only do the first one, for now
{
tmpStr = AXES_TYPE[i] + "1";
as = asf->CreateAxisSystem(AXES_TYPE[i], tmpStr);
if (as)
{
cout << "AxisSystem of type " << AXES_TYPE[i] <<
" was created with name " << tmpStr << endl;
if (i > 1) delete as;
else if (i == 0) mj = (MJ2000EqAxes*) as;
//else mj2 = (MJ2000EcAxes*) as;
}
else cout << "NO " << AXES_TYPE[i] << " AxisSystem created." << endl;
}
cout << " ------ number of objects instantiated = " << GmatBase::GetInstanceCount() << endl;
if (mj)
{
cout << "MJ2000EqAxes object exists with name " << mj->GetName() <<
" and type " << mj->GetTypeName() << endl;
}
mj2 = (MJ2000EqAxes*)(asf->CreateAxisSystem("MJ2000Eq","MJ2000Eq2"));
if (mj2)
{
cout << "MJ20002 object exists with name " << mj2->GetName() <<
" and type " << mj2->GetTypeName() << endl;
}
try
{
LeapSecsFileReader* ls = new LeapSecsFileReader(LeapFileName);
ls->Initialize();
EopFile *eop = new EopFile(eopFileName);
eop->Initialize();
ItrfCoefficientsFile* itrf = new ItrfCoefficientsFile(nutFileName, planFileName);
itrf->Initialize();
//bf->SetEopFile(eop);
//bf->SetCoefficientsFile(itrf);
TimeConverterUtil::SetLeapSecsFileReader(ls);
TimeConverterUtil::SetEopFile(eop);
}
catch (BaseException &bbee)
{
cout << "ERROR !!!!! " << bbee.GetMessage() << endl;
}
SolarSystem* ss;
Star* sol;
Planet* earth;
Planet* mars;
Planet* jupiter;
Moon* luna;
std::string j2000BN = "";
SpacePoint* j2000B = NULL;
try
{
cout << "\n==> Create the solar system <==" << endl;
ss = new SolarSystem("TheSS");
cout << "solar system name = " << ss->GetName() << endl;
cout << " ------ number of objects instantiated = " << GmatBase::GetInstanceCount() << endl;
earth = (Planet*) ss->GetBody(SolarSystem::EARTH_NAME);
cout << "earth name = " << earth->GetName() << endl;
cout << "earth's type name is " << earth->GetTypeName() << endl;
sol = (Star*) ss->GetBody(SolarSystem::SUN_NAME);
cout << "sol name = " << sol->GetName() << endl;
cout << "sol's type name is " << sol->GetTypeName() << endl;
cout << " ------ number of objects instantiated = " << GmatBase::GetInstanceCount() << endl;
luna = (Moon*) ss->GetBody(SolarSystem::MOON_NAME);
cout << "luna name = " << luna->GetName() << endl;
cout << "luna's type name is " << luna->GetTypeName() << endl;
mars = (Planet*) ss->GetBody(SolarSystem::MARS_NAME);
cout << "mars name = " << mars->GetName() << endl;
cout << "mars's type name is " << mars->GetTypeName() << endl;
jupiter = (Planet*) ss->GetBody(SolarSystem::JUPITER_NAME);
cout << "jupiter name = " << jupiter->GetName() << endl;
cout << "jupiter's type name is " << jupiter->GetTypeName() << endl;
SlpFile* anSLP;
DeFile* aDE;
try
{
std::string SLPFileName = "/GMAT/dev/datafiles/mac/DBS_mn2000.dat";
std::string DEFileName = "/GMAT/dev/datafiles/DEascii/macp1941.405";
anSLP = new SlpFile(SLPFileName);
aDE = new DeFile(Gmat::DE405,DEFileName);
cout << "the SLP file is : " << anSLP->GetName() << endl;
cout << "the DE file is : " << aDE->GetName() << endl;
}
catch (BaseException &be1)
{
cout << "ERROR with ephem file -> " << be1.GetMessage() << endl;
}
ss->SetSource(Gmat::SLP);
ss->SetSourceFile(anSLP);
//ss->SetSource(Gmat::DE_405);
//ss->SetSourceFile(aDE);
// set the j2000Body
j2000BN = "Earth";
j2000B = earth;
sol->SetJ2000BodyName(j2000BN);
sol->SetJ2000Body(j2000B);
earth->SetJ2000BodyName(j2000BN);
earth->SetJ2000Body(j2000B);
luna->SetJ2000BodyName(j2000BN);
luna->SetJ2000Body(j2000B);
mars->SetJ2000BodyName(j2000BN);
mars->SetJ2000Body(j2000B);
jupiter->SetJ2000BodyName(j2000BN);
jupiter->SetJ2000Body(j2000B);
}
catch (GmatBaseException &ex)
{
cout << "Some kind of error ..........." << endl;
}
bool isOK = false;
cout << "\n==> Now creating CoordinateSystems <==" << endl;
CoordinateSystem* mj2000 = new CoordinateSystem("", "CoordSystemMJ2000");
cout << " ------ number of objects instantiated = " << GmatBase::GetInstanceCount() << endl;
mj2000->SetSolarSystem(ss);
mj2000->SetStringParameter("OriginName","Earth");
mj2000->SetStringParameter("J2000BodyName",j2000BN);
isOK = mj2000->SetRefObject(earth,Gmat::SPACE_POINT,"Earth");
isOK = mj2000->SetRefObject(j2000B,Gmat::SPACE_POINT,j2000BN);
isOK = mj2000->SetRefObject(mj, Gmat::AXIS_SYSTEM, mj->GetName());
if (isOK) cout << "It seems to have been set OK!!!!!!!!!!!" << endl;
else cout << "ERROR setting axis system for coordinate system!!!!!" << endl;
mj2000->Initialize();
CoordinateSystem* mj20002 = new CoordinateSystem("", "CoordSystemMJ2000eq");
cout << " ------ number of objects instantiated = " << GmatBase::GetInstanceCount() << endl;
mj20002->SetSolarSystem(ss);
mj20002->SetStringParameter("OriginName",SolarSystem::SUN_NAME);
mj20002->SetStringParameter("J2000BodyName",j2000BN);
isOK = mj20002->SetRefObject(sol,Gmat::SPACE_POINT,SolarSystem::SUN_NAME);
//isOK = mj20002->SetRefObject(mars,Gmat::SPACE_POINT,"Earth");
isOK = mj20002->SetRefObject(j2000B,Gmat::SPACE_POINT,j2000BN);
isOK = mj20002->SetRefObject(mj2, Gmat::AXIS_SYSTEM, mj2->GetName());
if (isOK) cout << "It seems to have been set OK!!!!!!!!!!!" << endl;
else cout << "ERROR setting axis system for coordinate system!!!!!" << endl;
mj20002->Initialize();
try
{
cout << "Now checking CoordinateSystems' AxisSystems ..." << endl;
GmatBase *mjObj = mj2000->GetRefObject(Gmat::AXIS_SYSTEM, mj->GetName());
if (mjObj)
{
cout << "mj2000 has a pointer to the axis system " << mjObj->GetName() <<
" of type " << mjObj->GetTypeName() << endl;
}
else cout << "ERROR - no pointer to the axis system ????????" << endl;
GmatBase *mjObj2 = mj20002->GetRefObject(Gmat::AXIS_SYSTEM, mj2->GetName());
if (mjObj2)
{
cout << "mj2000ec has a pointer to the axis system " << mjObj2->GetName() <<
" of type " << mjObj2->GetTypeName() << endl;
}
else cout << "ERROR - no pointer to the axis system ????????" << endl;
}
catch (BaseException &be)
{
cout << "ERROR ------------- : " << be.GetMessage() << endl;
}
CoordinateConverter *cc = new CoordinateConverter();
//cc->SetJ2000BodyName("Earth");
//cc->SetJ2000Body(earth);
//Rvector6 theState(15999.99999999998,0.0,0.0,
// 0.0, 3.8662018270519716, 3.8662018270519711);
Rvector6 theState(18407337.2437560,146717552.364272,2436998.6080801622,
-29.85775713588113, 3.7988731566283533, -0.0883535323140749);
Rvector6 outState;
A1Mjd atTime1;
Real ut1_utc = 0.456647;
Real atTime = atTime1.UtcMjdToA1Mjd(ModifiedJulianDate(2012,1,1,0,0,ut1_utc));
A1Mjd testTime(atTime);
cout << "The test time is " << testTime.Get() << endl;
cout << "The test Rvector6 is " << theState << endl;
cout << "About to try to convert!!!!!" << endl;
try
{
cc->Convert(testTime,theState, mj2000, outState, mj20002);
cout << "The output state is : " << outState << endl;
}
catch (BaseException &cse)
{
cout << "ERROR: " << cse.GetMessage() << endl;
}
cout << "Now delete SolarSystem ............." << endl;
delete ss;
cout << "Now delete CoordinateConverter ............." << endl;
delete cc;
cout << "Now delete CoordinateSystem (and its AxisSystem) ............." << endl;
delete mj2000;
cout << "Now delete other CoordinateSystem (and its AxisSystem) ............." << endl;
delete mj20002;
//cout << "Now delete AxisSystem ............." << endl;
//delete mj;
cout << " ------ number of objects instantiated = " << GmatBase::GetInstanceCount() << endl;
cout << "Now delete everything else ............." << endl;
delete asf;
cout << " ------ number of objects instantiated = " << GmatBase::GetInstanceCount() << endl;
cout << "=-=-=-=-=-=-= END TEST coordinate system ....." << endl;
}
//------------------------------------------------------------------------------
// int main(int argc, char *argv[])
//------------------------------------------------------------------------------
int main(int argc, char *argv[])
{
std::string eopFileName = "/GMAT/dev/datafiles/EOPFiles/eopc04.62-now";
std::string nutFileName = "/GMAT/dev/datafiles/ITRF/NUTATION.DAT";
std::string planFileName = "/GMAT/dev/datafiles/ITRF/NUT85.DAT";
std::string SLPFileName = "/GMAT/dev/datafiles/mac/DBS_mn2000.dat";
std::string DEFileName = "/GMAT/dev/datafiles/DEascii/macp1941.405";
std::string LeapFileName = "/GMAT/dev/datafiles/tai-utcFiles/tai-utc.dat";
//std::string eopFileName = "/Users/wendyshoan/WORKONLY/dev/build3/bin/files/eop/eopc04.62-now";
//std::string nutFileName = "/Users/wendyshoan/WORKONLY/dev/build3/bin/files/itrf/NUTATION.DAT";
//std::string planFileName = "/Users/wendyshoan/WORKONLY/dev/build3/bin/files/itrf//NUT85.DAT";
//std::string SLPFileName = "/Users/wendyshoan/WORKONLY/dev/build3/bin/files/planetary_ephem/slp/DBS_mn2000.dat";
//std::string DEFileName = "/Users/wendyshoan/WORKONLY/dev/build3/bin/files/planetary_ephem/de/macp1941.405";
//std::string LeapFileName = "/Users/wendyshoan/WORKONLY/dev/build3/bin/files/time/tai-utc.dat";
cout << "=-=-=-=-=-=-= TEST CalculatedPoint/Barycenter ....." << endl;
cout << " ------ number of objects instantiated = " << GmatBase::GetInstanceCount() << endl;
cout.setf(ios::fixed);
cout.precision(30);
cout << "\n==> First, test the CalculatedPointFactory <==" << endl;
CalculatedPointFactory *cpf = new CalculatedPointFactory();
cout << "CalculatedPointFactory created .........." << endl;
cout << " ------ number of objects instantiated = " << GmatBase::GetInstanceCount() << endl;
LeapSecsFileReader* ls;
EopFile *eop;
ItrfCoefficientsFile* itrf;
try
{
ls = new LeapSecsFileReader(LeapFileName);
ls->Initialize();
eop = new EopFile(eopFileName);
eop->Initialize();
itrf = new ItrfCoefficientsFile(nutFileName, planFileName);
itrf->Initialize();
TimeConverterUtil::SetLeapSecsFileReader(ls);
TimeConverterUtil::SetEopFile(eop);
}
catch (BaseException &bbee)
{
cout << "ERROR !!!!! " << bbee.GetMessage() << endl;
}
SolarSystem* ss;
Star* sol;
Planet* earth;
Planet* mars;
Planet* jupiter;
Moon* luna;
std::string j2000BN = "";
SpacePoint* j2000B = NULL;
try
{
cout << "\n==> Create the solar system <==" << endl;
ss = new SolarSystem("TheSS");
cout << "solar system name = " << ss->GetName() << endl;
cout << " ------ number of objects instantiated = " << GmatBase::GetInstanceCount() << endl;
earth = (Planet*) ss->GetBody(SolarSystem::EARTH_NAME);
cout << "earth name = " << earth->GetName() << endl;
cout << "earth's type name is " << earth->GetTypeName() << endl;
sol = (Star*) ss->GetBody(SolarSystem::SUN_NAME);
cout << "sol name = " << sol->GetName() << endl;
cout << "sol's type name is " << sol->GetTypeName() << endl;
cout << " ------ number of objects instantiated = " << GmatBase::GetInstanceCount() << endl;
luna = (Moon*) ss->GetBody(SolarSystem::MOON_NAME);
cout << "luna name = " << luna->GetName() << endl;
cout << "luna's type name is " << luna->GetTypeName() << endl;
mars = (Planet*) ss->GetBody(SolarSystem::MARS_NAME);
cout << "mars name = " << mars->GetName() << endl;
cout << "mars's type name is " << mars->GetTypeName() << endl;
jupiter = (Planet*) ss->GetBody(SolarSystem::JUPITER_NAME);
cout << "jupiter name = " << jupiter->GetName() << endl;
cout << "jupiter's type name is " << jupiter->GetTypeName() << endl;
SlpFile* anSLP;
DeFile* aDE;
try
{
anSLP = new SlpFile(SLPFileName);
aDE = new DeFile(Gmat::DE405,DEFileName);
cout << "the SLP file is : " << anSLP->GetName() << endl;
cout << "the DE file is : " << aDE->GetName() << endl;
}
catch (BaseException &be1)
{
cout << "ERROR with ephem file -> " << be1.GetMessage() << endl;
}
//ss->SetSource(Gmat::SLP);
//ss->SetSourceFile(anSLP);
ss->SetSource(Gmat::DE_405);
ss->SetSourceFile(aDE);
// set the j2000Body
j2000BN = "Earth";
j2000B = earth;
sol->SetJ2000BodyName(j2000BN);
sol->SetJ2000Body(j2000B);
earth->SetJ2000BodyName(j2000BN);
earth->SetJ2000Body(j2000B);
luna->SetJ2000BodyName(j2000BN);
luna->SetJ2000Body(j2000B);
mars->SetJ2000BodyName(j2000BN);
mars->SetJ2000Body(j2000B);
jupiter->SetJ2000BodyName(j2000BN);
jupiter->SetJ2000Body(j2000B);
}
catch (GmatBaseException &ex)
{
cout << "Some kind of error ..........." << endl;
}
bool OK = false;
cout << "Now creating Barycenter1" << endl;
Barycenter *bary1 = (Barycenter*) cpf->CreateCalculatedPoint("Barycenter", "Bary1");
cout << "Now setting bddies for Bary1 .........." << endl;
bary1->SetStringParameter("BodyNames","Earth",0);
bary1->SetStringParameter("BodyNames","Sun",1);
bary1->SetStringParameter("BodyNames","Luna",2);
OK = bary1->SetRefObject(earth, Gmat::SPACE_POINT, "Earth");
if (!OK) cout << "ERROR setting barycenter with body Earth" << endl;
OK = bary1->SetRefObject(sol, Gmat::SPACE_POINT, "Sun");
if (!OK) cout << "ERROR setting barycenter with body Sun" << endl;
OK = bary1->SetRefObject(luna, Gmat::SPACE_POINT, "Luna");
if (!OK) cout << "ERROR setting barycenter with body Luna" << endl;
Integer num = 0;
StringArray names;
cout << "Check out bary1 data ---------------------" << endl;
num = bary1->GetIntegerParameter("NumberOfBodies");
cout << "bary1 number of bodies = " << num << endl;
cout << "bary1 body names are: " << endl;
names = bary1->GetStringArrayParameter(bary1->GetParameterID("BodyNames"));
for (unsigned int i = 0; i < names.size(); i++)
cout << " .... " << names.at(i) << endl;
cout << "bary1 bodies (their names) are: " << endl;
for (Integer i = 0; i < num; i++)
{
cout << " .... " << (bary1->GetRefObject(Gmat::SPACE_POINT, names.at(i), i))->GetName() << endl;
}
cout << "Now try to clone bary1 " << endl;
Barycenter* bary2 = (Barycenter*) bary1->Clone();
cout << "Check out bary2 data ---------------------" << endl;
num = bary2->GetIntegerParameter("NumberOfBodies");
cout << "bary2 number of bodies = " << num << endl;
cout << "bary2 body names are: " << endl;
names = bary2->GetStringArrayParameter(bary1->GetParameterID("BodyNames"));
for (unsigned int i = 0; i < names.size(); i++)
cout << " .... " << names.at(i) << endl;
cout << "bary2 bodies (their names) are: " << endl;
for (Integer i = 0; i < num; i++)
{
cout << " .... " << (bary2->GetRefObject(Gmat::SPACE_POINT, names.at(i), i))->GetName() << endl;
}
cout << "NOW try to clear the body list .........." << endl;
bary2->TakeAction("ClearBodies");
num = bary2->GetIntegerParameter("NumberOfBodies");
cout << "bary2 number of bodies = " << num << endl;
cout << "bary2 body names are: " << endl;
names = bary2->GetStringArrayParameter(bary1->GetParameterID("BodyNames"));
for (unsigned int i = 0; i < names.size(); i++)
cout << " .... " << names.at(i) << endl;
cout << "bary2 bodies (their names) are: " << endl;
for (Integer i = 0; i < num; i++)
{
cout << " .... " << (bary2->GetRefObject(Gmat::SPACE_POINT, names.at(i), i))->GetName() << endl;
}
A1Mjd atTime1;
// Real ut1_utc = -0.5036517; // 2005/01/01
Real atTime = atTime1.UtcMjdToA1Mjd(ModifiedJulianDate(1991,4,6,7,51,28.39));
A1Mjd testTime(atTime);
cout << "The test time is " << testTime.Get() << endl;
cout << "*** NOW try to do bary1 calculations ........." << endl;
cout.setf(ios::scientific);
cout << "Earth's mass = " << earth->GetMass() << endl;
//cout.setf(ios::fixed);
//cout.precision(30);
cout << "Earth's position and velocity at test time are : " << earth->GetMJ2000State(atTime) << endl;
//cout.setf(ios::scientific);
cout << "Sun's mass = " << sol->GetMass() << endl;
//cout.setf(ios::fixed);
//cout.precision(30);
cout << "Sun's position and velocity at test time are : " << sol->GetMJ2000State(atTime) << endl;
//cout.setf(ios::scientific);
cout << "Luna's mass = " << luna->GetMass() << endl;
//cout.setf(ios::fixed);
//cout.precision(30);
cout << "Luna's position and velocity at test time are : " << luna->GetMJ2000State(atTime) << endl;
cout << "bary1's position and velocity at test time = " << bary1->GetMJ2000State(atTime) << endl;
cout << "Now delete SolarSystem ............." << endl;
delete ss;
cout << " ------ number of objects instantiated = " << GmatBase::GetInstanceCount() << endl;
cout << "Now delete Barycenter 1 ............." << endl;
delete bary1;
cout << "........ bary1 deleted ............." << endl;
cout << "Now delete Barycenter 2 ............." << endl;
delete bary2;
cout << "........ bary2 deleted ............." << endl;
cout << "Now delete everything else ............." << endl;
delete cpf;
cout << "........ cpf deleted ............." << endl;
delete ls;
cout << "........ ls deleted ............." << endl;
delete eop;
cout << "........ eop deleted ............." << endl;
delete itrf;
cout << "........ itrf deleted ............." << endl;
cout << " ------ number of objects instantiated = " << GmatBase::GetInstanceCount() << endl;
cout << "=-=-=-=-=-=-= END TEST CalculatedPoint/Barycenter ....." << endl;
}