| CcabinDeck | Describes cabin deck of aircraft |
| CconvertUNICADO2CPACS | Class for the control of all reading functions from UNICADO |
| CconvertUNICADO2CPACSOutput | Class for creation and management of program output |
| CconvertUNICADO2CPACSSettings | Global class for the program settings, which are accessed throughout the program |
| ▼CcpacsAcft | Class that represents the CPACS Aircrafts XML Structure |
| CcomponentSegment | Class which represents the CPACS componentSegment-XML-Block |
| ►CcontrolSurface | Class that represents the CPACS Control Surface XML Block. Definition of the outer shape, structure and deflection of all control surfaces (flaps, slats, spoiler, ailerons...) of the wing |
| Cborder | Class which contains the borders around the control surface |
| ChingePoint | Gathers the parameters which describe a hinge in CPACS |
| CintermediateAirfoil | Class which describes the airfoil definition of a control surface between inner and outer border |
| CcpacsAccommodation | Class only used for conversion to UNICADO to include accommodations |
| CcpacsAeroPerformanceMap | Class which contains the aerodynamic performance data |
| CcpacsDeck | Class which represents the CPACS deck element XML block |
| ►CcpacsDesignSpecs | Class only used for conversion to UNICADO to include design specifications |
| CcargoDeck | Class which gathers the data for the cargo deck |
| CpaxDeck | Class which gathers the data for the pax deck |
| ►CcpacsEcologicalValues | Represents the CPACS ecological values block |
| CEmissions | Represents the CPACS emissions block |
| ►CcpacsEngine | Class which contains geometry and performance parameters of the engine |
| CenginePerformanceMap | Class which contains performance parameters of one engine deck |
| CJetEngine | Class which gathers the parameters of a jet engine |
| CScaledPerformanceCharacteristics | Class that gathers the following performance characteristics: thrust, fuel flow, TSFC and N1 |
| CTurbopropEngine | Class which gathers the parameters of a turboprop engine |
| CcpacsFuselage | Class which represents the CPACS fuselage XML block |
| ►CcpacsGear | Class which represents the CPACS gear XML block |
| Caxle | Class contains main information about the gears axle |
| ►Cbogie | Class which defines the landing gear's bogie |
| CbogieAxle | Class which contains axleuID an the relative position of the axle |
| CfuseAttachment | |
| CmainStrut | Class contains length and radius of the main strut |
| Cwheel | Class which contains the rough geometry of the wheel (cylinder) |
| CwingAttachment | Class which represents the CPACS wing attachment block |
| CcpacsIsotropicProperties | Class which represents the CPACS isotropic properties block |
| ►CcpacsMassBreakdown | |
| CmapElements | Structure for mass map elements (key + mass [kg]) |
| CmassElement | Class that represents a mass element |
| CmassMapElement | Class that represents a mass element, every mass element has a map of mass elements, you can access subelements with .at("name of the mass element") |
| CcpacsMaterial | Class which represents the CPACS material XML block |
| CcpacsMaterialProperties | Class which represents the CPACS MaterialProperties |
| CcpacsMaterials | Class which represents the CPACS materials XML block |
| ►CcpacsMission | Class which represents the CPACS missions XML Block |
| ►CmissionSegment | Class which represents the mission segment in the CPACS file |
| CExitConditions | Structure which describes the exit conditions of the mission segment in the CPACS file |
| Ctrajectory | Class which contains the relevant trajectory data |
| ►CcpacsMonetaryValues | Class which represents the CPACS monetary values block |
| ►CcostElement | Class which represents a cost element, where every cost element has a map of cost elements |
| CcostDescription | Class which represents the cost's description and amount |
| CmapElements | Structure for mapElements (key + a costElement value) |
| CcpacsProfile | Class which represents the CPACS profile XML block (fuselage and wing) |
| CcpacsProfiles | Class which represents the CPACS profiles XML block (fuselage and wing) |
| CcpacsPylon | Class which represents the CPACS pylon XML block |
| CcpacsReference | Class that represents the CPACS reference block |
| CcpacsRequirements | Represents the CPACS requirements block |
| CcpacsSeatElement | Class which represents the CPACS seat element XML block |
| ►CcpacsSystem | Class which contains the performance parameters of the system |
| ►CATA | Class which contains the system's pre-design definitions according to the Air Transport Association (ATA) |
| CChapter | Class which contains ATA chapters of the respective pre-design definition |
| CmapElements | Structure for ATA (key + an ATA value) |
| ►CcpacsTrajectory | Class which represents the CPACS trajectory XML block |
| CcomponentDeflection | Class which represents deflection angle of a component |
| CEmissionValues | Class which represents the CPACS emissions XML block |
| CcpacsWing | Class which represents the CPACS wing XML block |
| Celement | Class that represents the generalized CPACS Elements-Block, that is used for all components such as wing, fuselage, etc |
| CfuelTank | Class which describes the different volumes of the fuel tank |
| CfuselageFuelTank | Class which describes the different volumes of the fuselage fuel tank including its position |
| Cinformation | Class that represents the CPACS Info which is used for all components |
| Cpositioning | Class that represents the generalized CPACS Positionings Block, that is used for all components such as wing, fuselage, etc |
| Csection | Class that represents the generalized CPACS Section Block, that is used for all components such as wing, fuselage, etc |
| Csegment | Class that represents the generalized CPACS Segments Block, that is used for all components such as wing, fuselage, etc |
| ►Cspars | Class which defines the spars in CPACS |
| CsparPosition | Class which defines the spars' position in CPACS |
| ►CsparSegments | Class which defines the CPACS spar segments block |
| CsparPositionUID | Class which defines the CPACS spar position's uID |
| Ctransformation | Class that represents the CPACS Transformation Block, that is used for all components such as wing, fuselage, etc |
| CwingFuelTank | Class which describes the different volumes of the wing fuel tank including its position |
| CcpacsMassBreakDown | Class that represents the CPACS MassBreakdown Block |
| CcruiseSteps | Class contains relative length and flight level of cruise steps |
| CFurnishing | Class represents costs for furnishing |
| Coutput | |
| Csettings | |
| ▼CunicadoAcft | Class that represents the UNICADO XML Structure |
| CcentreOfGravityRangeStruct | Structure for center of gravity range |
| ►CunicadoAccommodation | Represents the unicado Accommodations Values-XML-Block |
| ►Ccabin | Describes cabin of aircraft |
| ►CcabinDeck | Describes cabin deck of aircraft |
| CCabinClass | |
| ►Ccargo | Describes cargo of aircraft |
| ►CcargoDeck | Describes cargo decks of aircraft |
| CCargoCompartment | Describes cargo compartments of aircraft |
| Cgalley | Describes galleys of aircraft |
| Clavatory | Describes the lavatories of aircaft |
| ►Cseat | Describes seats of aircraft |
| CseatConfiguration | Describes configuration of seats |
| ►CunicadoAerodynamics | Represents the unicado Aerodynamics Values XML-Block |
| CaerodynamicRefValues | Describes the aerodynamic reference values of aircraft |
| ►CdragCoefficients | Describes drag coefficients of aircraft |
| CviscousDrag | Describes viscous drag of aircraft |
| CwaveDrag | Describes wave drag coefficients of aircraft |
| CliftCoefficients | Describes the lift coefficients of aircraft |
| CmomentCoefficients | Describes moment coefficients of aircraft(trimmed, with maximum L/D in cruise) |
| ►CpolarAerodynamics | Describes polar aerodynamics of aircraft |
| Cconfiguration | Describes configurations in polar file |
| ►CunicadoDesignSpecs | Represents the unicado design specification XML-Block |
| ►Caccommodation | Describes specifications regarding passenger decks and classes |
| ►CpaxDeck | Describes passenger deck |
| CcabinClass | Describes characteristics of cabin classes |
| ►Ccargo | Describes specifications regarding cargo decks and ULDs |
| ►CcargoDeck | Describes characteristics of cargo deck |
| ►Ccompartment | Describes characteristics of compartment |
| CunitLoadDevice | Class defines container group (ULD) |
| ClaminarFlowTechnology | Class describes application of laminar flow controlling on different components |
| Cpropulsion | Class describes specifications for the propulsion system |
| ►CunicadoEcologicalValues | Represents the unicado EcologicalValues-XML-Block |
| ►CairQuality | Class describes Air quality impact due to Aircraft Operation |
| CtoleranceFactors | Class describes Tolerance Factors of Emissions emitted during LTO |
| ►Cced | Class describes Cumulative Energy Demand |
| CcedComponents | Class describes components of Cumulative Energy Demand |
| CclimateImpact | Class describes Climate Impact due to Aircraft Operation |
| ►CcommunityNoiseLevels | Class describes community noise level for take off, approach and cumulative |
| CEPNLArea | Class describes areas of defined effective percieved noise level |
| CloudnessArea | Class describes areas of defined Zwickers loudness |
| CPNLArea | Class describes areas of defined percieved noise level |
| CPNLTArea | Class describes areas of defined Tone Corrected Perceived Noise Level |
| CSELArea | Class describes areas of defined sound exposure level |
| CsharpnessArea | Class describes areas of defined sharpness level |
| CSPLArea | Class describes areas of defined sound pressure level |
| CtonalityArea | Class describes areas of defined tonality level |
| CEmissions | Class describes mass of different emissions |
| ►CnoiseCertLevels | Describes acoustic parameters and noise evaluation measures |
| CcertificationPoint | Class describes noise parameter in certification points |
| CnoisePathFile | Class describes departure and approach path |
| ►COperations | Class describes operation emissions |
| ►COperationComponents | Class describes components of operation emissions |
| CEngineEmissons | Class describes engine emissions |
| ►CMission | Class describes Environmental analysis of one study mission |
| CLTOTimes | Class describes segments of landing and take off, all phases under 3000 ft |
| ►CunicadoGeometry | Represents the unicado Geometry-XML-Block |
| CusedComponents | Represents the unicado UsedComponents-XML-Block |
| ►CunicadoMassesAndLoadings | Class represents the UNICADO MassesAndLoadings-Block |
| ►CmassBreakdown | Class represents the unicado MassBreakdown-Block |
| CmapElements | Structure for mass map elements (key + mass [kg]) |
| CmassElement | Class represents a mass element, every mass element has a map of mass elements, you can access subelements with .at("name of the mass element") |
| ►CunicadoMonetaryValues | Represents the unicado Monetary Values-XML-Block |
| ►CLCC | Nested Class LCC represents life cycle costs |
| ►CendOfLifeCosts | Class describes End-of-life-Costs |
| CeOLCTotalComponents | Class describes components of end of life costs |
| ►CNRC | Class represents Non recurring costs |
| ►CNRCComponents | Class represents components of non recurring cost |
| ►CFlightTestAC | Class represents costs for Aircraft flight tests |
| CFlightTestACComponents | Class represents components of flight test costs |
| ►CoperatingCosts | Class describes operating costs |
| ►CDOC | Class describes the direct operating costs |
| ►CdocComponents | Class describes components of direct operating costs in 100ASK |
| CdocCharge | Class describes charge per 100ASK |
| ►CdocMaintenance | Class describes maintenance costs |
| ►CMaintenanceComponents | Class describes components of maintenance costs |
| ►CmaintenanceAirframe | Class describes airframe maintenance costs |
| ►CATAChapter | Class describes maintenance costs for ATA chapter |
| CCostComponents | Class describes components of costs for ATA chapter |
| CCostComponents | Class describes costs for a components containing labour and material costs |
| CoperatingScenario | Class describes operating scenario containing number of flights and seat load factor |
| CtotalCosts | Class describes total costs |
| ►CRC | Class represents recurring costs |
| ►CRCComponents | Class represents components of recurring costs |
| ►CFurnishings | |
| CFurnishingsComponents | Class describes components of furnishing costs |
| ►CPowerUnit | Class represents costs for all installed engines with systems without pylons |
| CPowerUnitComponents | Class represents components of power unit costs |
| ►CSystems | Class Represents Costs for Systems |
| CSystemsComponents | Class represents components of system costs |
| CMonetaryScenario | Describes the monetary scenario containing engineering hours and production volume |
| ►CunicadoPerformance | Represents the unicado Performance Values-XML-Block |
| Caltitude | Describes different flight altitudes of aircraft |
| Cclimb | Describes characteristics of climb |
| CenginePerformanceMap | The class contains the parameters and values of an engine deck (csv file) |
| ►CmissionAnalysis | The class contains general mission data, predefined mission steps and the resulting trajectory |
| CcruiseStep | |
| CmissionSegment | The class contains the main aircraft parameters at each mission step |
| Ctrajectory | Class contains trajectory data at different time steps |
| Crange | Describes reachable range |
| ►CrequirementChecks | Class describes the fulfillment of requirements |
| Ccertification | Class represents fulfillment of certification specifications; fulfilled:1, not fulfilled:0 |
| CTLARs | Represents fulfillment of top level aircraft requirements; fulfilled:1, not fulfilled 0 |
| Cspeed | Describes different speeds |
| CtakeOff | Describes characteristics of take-off |
| ►CvnDiagram | Describes velocity-loadFactor-diagram |
| CvnConfigurations | Class describes different configurations for vn diagram |
| ►CunicadoPropulsion | Represents the unicado Propulsion Values-XML-Block |
| CengineDimensions | Describes geometrical data of scaled engine, core engine |
| CjetEngineData | Describes jet engine specific data |
| ►CnacellePositioning | Describes positioning of nacelle |
| CnacelleLocationType | Describes rescaling of nacelle |
| CscaledPerformanceCharacteristics | Describes performance characteristic of one scaled engine |
| CturbopropEngineData | Describes prob specific engine data |
| ►CunicadoRequirements | |
| CdesignMissionRequirements | Inherited class of missionRequirements |
| CmissionRequirements | Class describes parameter of mission requirement |
| CstudyMissionRequirements | Inherited class of missionRequirements |
| ►CunicadoStabilityAndControlCharacteristics | Represents the unicado StabilityAndControlCharacteristics Values-XML-Block |
| Cstabilizer | Describes the stabilizer characteristics |
| CverticalTail | Describes characteristics of vertical tail |
| ►CunicadoSystems | Represents the unicado Systems Values-XML-Block |
| ►CataChapter | Represents the ata chapter in XML file |
| CspecificValues | Describes specific values in ATA chapter |
| CfuelTank | Represents the unicado fuel tank Values-XML-Block |
| CusedElements | Represents the unicado UsedElements-XML-Block |
1.9.4