tigl::CTiglStandardizer Class Reference

#include <CTiglStandardizer.h>

Static Public Member Functions
static void	StandardizeAircraft (CCPACSConfiguration &config, bool useSimpleDecomposition=false)
static void	StandardizeFuselage (CCPACSFuselage &fuselage, bool useSimpleDecomposition=false)
static void	StandardizeWing (CCPACSWing &wing, bool useSimpleDecomposition=false)

Static Private Member Functions
static std::vector< CTiglTransformation >	GetTotalTransformations (std::vector< tigl::CTiglSectionElement * > elements)
static void	SetTotalTransformations (std::vector< CTiglSectionElement * > elements, std::vector< CTiglTransformation >, bool useSimpleDecomposition=false)
static void	StdandardizePositioningsStructure (CCPACSPositionings &positionings, std::vector< CTiglSectionElement * > elements)

Member Function Documentation

GetTotalTransformations()

static std::vector<CTiglTransformation> tigl::CTiglStandardizer::GetTotalTransformations ( std::vector< tigl::CTiglSectionElement * >  elements )

staticprivate

SetTotalTransformations()

static void tigl::CTiglStandardizer::SetTotalTransformations ( std::vector< CTiglSectionElement * >  elements, std::vector< CTiglTransformation >  , bool  useSimpleDecomposition = false  )

staticprivate

StandardizeAircraft()

static void tigl::CTiglStandardizer::StandardizeAircraft ( CCPACSConfiguration &  config, bool  useSimpleDecomposition = false  )

static

Standardize the all the wings and the fuselage of the aircraft.

Parameters

config
useSimpleDecomposition

StandardizeFuselage()

static void tigl::CTiglStandardizer::StandardizeFuselage ( CCPACSFuselage &  fuselage, bool  useSimpleDecomposition = false  )

static

Standardize the fuselage using the CPACSCreator standard. This mean: 1) The fuselage transformation store the nose position. 2) The translation of sections are set using positionings. 3) Each positioning correspond to a segment, except for the nose section that has a positioning from the fuselage origin (with a length of 0, if the origin of the profile correspond to its center).

Parameters

fuselage
useSimpleDecomposition,if	set to true the standardization use only polar decomposition. This mean that the cpacs file is more readable but there can be some simplification that change the global shape of the fuselage.

StandardizeWing()

static void tigl::CTiglStandardizer::StandardizeWing ( CCPACSWing &  wing, bool  useSimpleDecomposition = false  )

static

Standardize the wing using the CPACSCreator standard. This mean: 1) The wing transformation store the root leading point translation. 2) The translation of sections are set using positionings. 3) Each positioning correspond to a segment, except for the root section that has a positioning from the wing origin (with a length of 0, if the origin of the airfoil correspond to its leading edge).

Parameters

wing
useSimpleDecomposition,if	set to true the standardization use only polar decomposition. This mean that the cpacs file is more readable but there can be some simplification that change the global shape of the wing.

StdandardizePositioningsStructure()

static void tigl::CTiglStandardizer::StdandardizePositioningsStructure ( CCPACSPositionings &  positionings, std::vector< CTiglSectionElement * >  elements  )

staticprivate

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The documentation for this class was generated from the following file:

• CTiglStandardizer.h