Class which represents the CPACS trajectory XML block.
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#include <cpacsAcftXML.h>
Class which represents the CPACS trajectory XML block.
◆ cpacsTrajectory()
cpacsAcft::cpacsTrajectory::cpacsTrajectory |
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◆ ~cpacsTrajectory()
cpacsAcft::cpacsTrajectory::~cpacsTrajectory |
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◆ altitude
std::vector<double> cpacsAcft::cpacsTrajectory::altitude |
Vector which contains current altitude [m]
◆ angleOfAttack
std::vector<double> cpacsAcft::cpacsTrajectory::angleOfAttack |
Vector which contains the current angle of attack [deg]
◆ angleOfRoll
std::vector<double> cpacsAcft::cpacsTrajectory::angleOfRoll |
Vector which contains the current angle of roll [deg]
◆ angleOfYaw
std::vector<double> cpacsAcft::cpacsTrajectory::angleOfYaw |
Vector which contains the current angle of yaw [deg]
◆ cAS
std::vector<double> cpacsAcft::cpacsTrajectory::cAS |
Vector which contains calibrated air speed [m/s]
◆ cO2Flow
std::vector<double> cpacsAcft::cpacsTrajectory::cO2Flow |
Vector which contains current CO2 flow [kg/s]
◆ cO2Mass
double cpacsAcft::cpacsTrajectory::cO2Mass |
CO2 mass emitted during mission step [kg]
◆ cOFlow
std::vector<double> cpacsAcft::cpacsTrajectory::cOFlow |
Vector which contains current CO flow [kg/s]
◆ cOMass
double cpacsAcft::cpacsTrajectory::cOMass |
CO mass emitted during mission step [kg]
◆ currentLocation
std::vector<Vec3> cpacsAcft::cpacsTrajectory::currentLocation |
Vector which contains the current location
◆ deltaTemperature
◆ distance
double cpacsAcft::cpacsTrajectory::distance |
Distance flown during mission step [m]
◆ flightDistance
std::vector<double> cpacsAcft::cpacsTrajectory::flightDistance |
Vector which contains flown flight distance [m]
◆ flightTime
std::vector<double> cpacsAcft::cpacsTrajectory::flightTime |
Vector which contains the elapsed flight times [s]
◆ fuelFlow
std::vector<double> cpacsAcft::cpacsTrajectory::fuelFlow |
Vector which contains current fuel flow [kg/s]
◆ fuelMass
double cpacsAcft::cpacsTrajectory::fuelMass |
Fuel mass consumed during mission step [kg]
◆ groundDistance
std::vector<double> cpacsAcft::cpacsTrajectory::groundDistance |
Vector which contains the distance to the ground [m]
◆ h2OMass
double cpacsAcft::cpacsTrajectory::h2OMass |
H2O mass emitted during mission step [kg]
◆ hCFlow
std::vector<double> cpacsAcft::cpacsTrajectory::hCFlow |
Vector which contains current HC (carbon hydride) flow [kg/s]
◆ hCMass
double cpacsAcft::cpacsTrajectory::hCMass |
HC (carbon hydride) mass emitted during mission step [kg]
◆ index
std::vector<int> cpacsAcft::cpacsTrajectory::index |
Vector which contains index variables
◆ info
Object of the information class that provides the CPACS trajectory infos like uID and description
◆ latitude
std::vector<double> cpacsAcft::cpacsTrajectory::latitude |
Vector which contains current latitude [coordinate 0-360]
◆ longitude
std::vector<double> cpacsAcft::cpacsTrajectory::longitude |
Vector which contains current longitude [coordinate 0-360]
◆ mass
std::vector<double> cpacsAcft::cpacsTrajectory::mass |
Vector which contains the current aircraft's total mass [kg]
◆ missionUID
std::string cpacsAcft::cpacsTrajectory::missionUID |
◆ nOXFlow
std::vector<double> cpacsAcft::cpacsTrajectory::nOXFlow |
Vector which contains current NOx flow [kg/s]
◆ nOXMass
double cpacsAcft::cpacsTrajectory::nOXMass |
NOx mass emitted during mission step [kg]
◆ nOXMassHumid
double cpacsAcft::cpacsTrajectory::nOXMassHumid |
Humid NOx mass emitted during mission step [kg]
◆ radiativeForcing
◆ refLocation
std::vector<Vec3> cpacsAcft::cpacsTrajectory::refLocation |
Vector which contains the reference location
◆ segmentUID
std::vector<std::string> cpacsAcft::cpacsTrajectory::segmentUID |
Vector which contains the segment's CPACS uID
◆ sO2Flow
std::vector<double> cpacsAcft::cpacsTrajectory::sO2Flow |
Vector which contains current SO2 flow [kg/s]
◆ sO2Mass
double cpacsAcft::cpacsTrajectory::sO2Mass |
SO2 mass emitted during mission step [kg]
◆ sootFlow
std::vector<double> cpacsAcft::cpacsTrajectory::sootFlow |
Vector which contains current soot flow [kg/s]
◆ sootMass
double cpacsAcft::cpacsTrajectory::sootMass |
Soot mass emitted during mission step [kg]
◆ staticPressure
std::vector<double> cpacsAcft::cpacsTrajectory::staticPressure |
Vector which contains the static pressure [Pa]
◆ tAS
std::vector<double> cpacsAcft::cpacsTrajectory::tAS |
Vector which contains the true air speed [m/s]
◆ theControlSurfaceDeflections
◆ theGearDeflections
◆ thrust
std::vector<double> cpacsAcft::cpacsTrajectory::thrust |
Vector which contains current thrust [N]
◆ time
double cpacsAcft::cpacsTrajectory::time |
Time elapsed during mission step [s]
The documentation for this class was generated from the following files: