void interplanetaryDialog::on_buttonBox_accepted()
{
// Create a new scenario
SpaceScenario* scenario = new SpaceScenario();
scenario->setName("This is a demo");
ScenarioSC* sc = new ScenarioSC();
sc->setName("my satellite demo");
sc->ElementIdentifier()->setName("my satellite demo");
// Create the initial position (Keplerian elements)
ScenarioKeplerianElementsType* elements = new ScenarioKeplerianElementsType();
elements->setSemiMajorAxis(87000.0);
elements->setEccentricity(0.0045);
elements->setInclination(27.456);
elements->setRAAN(132.34);
elements->setArgumentOfPeriapsis(231.34);
elements->setTrueAnomaly(45.32);
// Create the initial attitude (Euler elements)
ScenarioEulerType* initAtt = new ScenarioEulerType();
initAtt->setPhi(0.00000);
initAtt->setTheta(0.00000);
initAtt->setPsi(0.00000);
initAtt->setPhiDot(0.00000);
initAtt->setThetaDot(0.00000);
initAtt->setPsiDot(0.00000);
// Create the trajectory arc
ScenarioLoiteringType* loitering = new ScenarioLoiteringType();
loitering->ElementIdentifier()->setName("loitering");
loitering->ElementIdentifier()->setColorName("Yellow");
loitering->Environment()->CentralBody()->setName("Earth");
loitering->InitialPosition()->setCoordinateSystem("INERTIAL J2000");
loitering->PropagationPosition()->setTimeStep(60.0);
loitering->PropagationPosition()->setPropagator("TWO BODY");
loitering->PropagationPosition()->setIntegrator("RK4");
loitering->InitialAttitude()->setCoordinateSystem("EULER 123");
loitering->PropagationAttitude()->setIntegrator(""); // Not defined in STA yet
loitering->PropagationAttitude()->setTimeStep(60.0);
// Time-line
QDateTime TheCurrentDateAndTime = QDateTime::currentDateTime(); // Get the current epoch
loitering->TimeLine()->setStartTime(TheCurrentDateAndTime);
loitering->TimeLine()->setEndTime(TheCurrentDateAndTime.addDays(1));
loitering->TimeLine()->setStepTime(60.0);
loitering->InitialPosition()->setAbstract6DOFPosition(QSharedPointer<ScenarioAbstract6DOFPositionType>(elements));
//loitering->InitialAttitude()->setAbstract6DOFAttitude(initAtt);
loitering->InitialAttitude()->setAbstract6DOFAttitude(QSharedPointer<ScenarioAbstract6DOFAttitudeType>(initAtt));
// Create the spacecraft
sc->SCMission()->TrajectoryPlan()->AbstractTrajectory().append(QSharedPointer<ScenarioAbstractTrajectoryType>(loitering));
// Add it to the scenario
scenario->AbstractParticipant().append(QSharedPointer<ScenarioParticipantType>(sc));
mainwindow->setScenario(scenario);
return;
}
/* This slot is signalled when an inline edit is performed on an item
* in the scenario tree.
*/
void ScenarioTree::editItemInline(QTreeWidgetItem* item, int column)
{
ScenarioObject* object = objectForItem(item);
if (object == NULL)
return;
// TODO: If we allow more objects to be editing in the scenario
// tree view, we need to add an edit method.
if (dynamic_cast<ScenarioParticipant*>(object) && column == 1)
{
// Change the name of a participant
ScenarioParticipant* participant = dynamic_cast<ScenarioParticipant*>(object);
participant->setName(item->text(1));
}
else if (dynamic_cast<SpaceScenario*>(object) && column == 1)
{
SpaceScenario* scenario = dynamic_cast<SpaceScenario*>(object);
scenario->setName(item->text(1));
}
}
/** Load an OEM file and convert it to an STA Space Scenario.
*
* Not all features of the OEM format are supported by the OemImporter
* class. An oem file that uses an unsupported feature will fail to load;
* details of the problem are available via the errorMessage() method.
*
* The current implementation has the following limitations:
* - TIME_STANDARD must be TDB
* - REF_FRAME must be EME2000 or ECLIP2000
* - CENTER_NAME must be an object with an ephemeris
*
* \return a pointer to a complete space scenario, or NULL if
* there was an error loading the scenario.
*/
SpaceScenario*
OemImporter::loadScenario()
{
readHeader();
SpaceScenario* scenario = new SpaceScenario();
scenario->setName("New scenario");
QSharedPointer<ScenarioSC> sc(new ScenarioSC());
scenario->AbstractParticipant().append(sc);
ScenarioExternalType* trajectory;
bool skip = false;
QString line;
QString objectName;
StaBody* center = NULL;
sta::CoordinateSystemType coordSys = sta::COORDSYS_INVALID;
QRegExp whiteSpaceRegExp("\\s+");
// This is the state machine for parsing OEM files. Roughly, the structure
// of an OEM file is:
// Header
//
// Metadata
// Ephemeris data
// Metadata
// Ephemeris data
// ...
//
// Where the metadata and ephemeris data blocks alternate; any number
// of metadata/ephemeris data pairs may appear in the file. For full
// details see Recommended Standard CCSDS 502.0-B-2.
while (m_parserState != Oem_End && m_parserState != Oem_Error)
{
if (skip)
{
skip = false;
}
else
{
line = m_stream->readLine().trimmed();
m_lineNumber++;
}
if (m_stream->atEnd())
{
m_parserState = Oem_End;
}
else if (line.isEmpty())
{
// Nothing to do
}
else
{
switch (m_parserState)
{
case Oem_Begin:
{
OemKeyValue kv = ParseKeyValue(line);
if (kv.key == "CCSDS_OEM_VERS")
{
m_parserState = Oem_AfterVersion;
}
else
{
raiseError("Version expected in header");
}
}
break;
case Oem_AfterVersion:
if (line.startsWith("COMMENT"))
{
// Skip and do nothing
}
else
{
OemKeyValue kv = ParseKeyValue(line);
if (kv.key == "CREATION_DATE")
{
m_parserState = Oem_AfterCreationDate;
}
else
{
raiseError("Creation date expected in header");
}
}
break;
case Oem_AfterCreationDate:
{
OemKeyValue kv = ParseKeyValue(line);
if (kv.key == "ORIGINATOR")
{
m_parserState = Oem_AfterHeader;
}
else
{
raiseError("Creation date expected in header");
}
}
break;
case Oem_AfterHeader:
if (line.startsWith("COMMENT"))
{
// Skip and do nothing
}
else if (line == "META_START")
{
m_parserState = Oem_MetaStart;
}
else
{
raiseError("Metadata block expected");
}
break;
case Oem_MetaStart:
{
OemKeyValue kv = ParseKeyValue(line);
if (kv.key == "OBJECT_NAME")
{
m_parserState = Oem_AfterObjectName;
objectName = kv.value;
}
else
{
raiseError("Object name expected");
}
}
break;
case Oem_AfterObjectName:
{
OemKeyValue kv = ParseKeyValue(line);
if (kv.key == "OBJECT_ID")
{
m_parserState = Oem_AfterObjectId;
}
else
{
raiseError("Object ID expected");
}
}
break;
case Oem_AfterObjectId:
{
OemKeyValue kv = ParseKeyValue(line);
if (kv.key == "CENTER_NAME")
{
m_parserState = Oem_AfterCenterName;
center = STA_SOLAR_SYSTEM->lookup(kv.value);
if (!center)
{
raiseError("Unknown central body " + kv.value);
}
}
else
{
raiseError("Center name expected");
}
}
break;
case Oem_AfterCenterName:
{
OemKeyValue kv = ParseKeyValue(line);
if (kv.key == "REF_FRAME")
{
m_parserState = Oem_AfterRefFrame;
if (kv.value == "EME2000")
{
coordSys = sta::COORDSYS_EME_J2000;
}
else if (kv.value == "ECLIP2000")
{
coordSys = sta::COORDSYS_ECLIPTIC_J2000;
}
else
{
raiseError("Unsupported reference frame " + kv.value);
}
}
else
{
raiseError("Reference frame expected");
}
}
break;
case Oem_AfterRefFrame:
{
OemKeyValue kv = ParseKeyValue(line);
if (kv.key == "REF_FRAME_EPOCH")
{
}
else
{
skip = true;
}
m_parserState = Oem_AfterRefFrameEpoch;
}
break;
case Oem_AfterRefFrameEpoch:
{
OemKeyValue kv = ParseKeyValue(line);
if (kv.key == "TIME_SYSTEM")
{
m_parserState = Oem_AfterTimeSystem;
if (kv.value != "TDB")
{
raiseError("Unsupported time system " + kv.value);
}
}
else
{
raiseError("Time system expected");
}
}
break;
case Oem_AfterTimeSystem:
{
OemKeyValue kv = ParseKeyValue(line);
if (kv.key == "START_TIME")
{
m_parserState = Oem_AfterStartTime;
}
else
{
raiseError("Start time expected");
}
}
break;
case Oem_AfterStartTime:
{
OemKeyValue kv = ParseKeyValue(line);
if (kv.key == "USEABLE_START_TIME")
{
}
else
{
skip = true;
}
m_parserState = Oem_AfterUseableStartTime;
}
break;
case Oem_AfterUseableStartTime:
{
OemKeyValue kv = ParseKeyValue(line);
if (kv.key == "USEABLE_STOP_TIME")
{
}
else
{
skip = true;
}
m_parserState = Oem_AfterUseableStopTime;
}
break;
case Oem_AfterUseableStopTime:
{
OemKeyValue kv = ParseKeyValue(line);
if (kv.key == "STOP_TIME")
{
m_parserState = Oem_AfterStopTime;
}
else
{
raiseError("Stop time expected");
}
}
break;
case Oem_AfterStopTime:
{
OemKeyValue kv = ParseKeyValue(line);
if (kv.key == "INTERPOLATION")
{
}
else
{
skip = true;
}
m_parserState = Oem_AfterInterpolation;
}
break;
case Oem_AfterInterpolation:
{
OemKeyValue kv = ParseKeyValue(line);
if (kv.key == "INTERPOLATION_DEGREE")
{
}
else
{
skip = true;
}
m_parserState = Oem_AfterInterpolationDegree;
}
break;
case Oem_AfterInterpolationDegree:
if (line == "META_STOP")
{
m_parserState = Oem_AfterMetaStop;
trajectory = new ScenarioExternalType();
int trajectoryIndex = sc->SCMission()->TrajectoryPlan()->AbstractTrajectory().size();
trajectory->CentralBody()->setName(center->name());
trajectory->setCoordinateSystem(sta::CoordinateSystem(coordSys).name());
trajectory->ElementIdentifier()->setName(QString("%1 - %2").arg(objectName).arg(trajectoryIndex + 1));
trajectory->ElementIdentifier()->setColorName("Yellow");
sc->SCMission()->TrajectoryPlan()->AbstractTrajectory().append(QSharedPointer<ScenarioAbstractTrajectoryType>(trajectory));
}
else
{
raiseError("End of metadata (META_STOP) expected");
}
break;
case Oem_AfterMetaStop:
if (line.startsWith("COMMENT"))
{
// Ignore the comment
}
else
{
skip = true;
m_parserState = Oem_EphemerisData;
}
break;
case Oem_EphemerisData:
if (line == "META_START")
{
m_parserState = Oem_MetaStart;
}
else
{
// Parse the ephemeris line
QStringList values = line.split(whiteSpaceRegExp);
if (values.size() != 7)
{
raiseError("Bad or unsupported ephemeris data record");
}
else
{
QDateTime dateTime;
int secondsDecimal = values[0].lastIndexOf('.');
if (secondsDecimal > 0)
{
bool msecOk = false;
double sec = values[0].right(values[0].length() - secondsDecimal).toDouble(&msecOk);
if (msecOk)
{
dateTime = QDateTime::fromString(values[0].left(secondsDecimal), Qt::ISODate);
dateTime.setTimeSpec(Qt::UTC);
int msec = (int) (sec * 1000.0);
dateTime = dateTime.addMSecs((int) (sec * 1000.0));
}
}
else
{
dateTime = QDateTime::fromString(values[0], Qt::ISODate);
}
if (!dateTime.isValid())
{
raiseError(QString("Bad time value in ephemeris data (%1)").arg(values[0]));
}
else
{
bool stateValid = true;
double state[6];
for (int i = 0; i < 6; ++i)
{
bool ok = false;
state[i] = values[i + 1].toDouble(&ok);
if (!ok)
{
stateValid = false;
}
}
if (!stateValid)
{
raiseError("Non-number in ephemeris data");
}
else
{
trajectory->TimeTags().append(dateTime);
for (int i = 0; i < 6; ++i)
{
trajectory->States() << state[i];
}
}
}
}
}
break;
default:
m_parserState = Oem_Error;
break;
}
}
}
// Validate trajectory by making sure that there are no overlapping segments or gaps
if (sc)
{
for (int i = 1; i < sc->SCMission()->TrajectoryPlan()->AbstractTrajectory().size(); ++i)
{
ScenarioExternalType* prev = dynamic_cast<ScenarioExternalType*>(sc->SCMission()->TrajectoryPlan()->AbstractTrajectory().at(i - 1).data());
ScenarioExternalType* curr = dynamic_cast<ScenarioExternalType*>(sc->SCMission()->TrajectoryPlan()->AbstractTrajectory().at(i).data());
if (prev && curr && !prev->TimeTags().isEmpty() && !curr->TimeTags().isEmpty())
{
QDateTime prevEnd = prev->TimeTags().last();
QDateTime currStart = curr->TimeTags().first();
if (currStart < prevEnd)
{
raiseError(QString("Ephemeris segments %1 and %2 overlap.").arg(i - 1).arg(i));
}
else if (currStart > prevEnd)
{
raiseError(QString("Gap between ephemeris segments %1 and %2.").arg(i - 1).arg(i));
}
}
}
}
if (m_parserState == Oem_Error)
{
qDebug() << "Error while importing OEM file: " << errorMessage();
delete scenario;
scenario = NULL;
}
else
{
scenario->setName(objectName);
sc->setName(objectName);
sc->ElementIdentifier()->setName(objectName);
}
return scenario;
}