Derived class quaternionSixDOF

quaternionSixDOF provides the same functionality as the old sixDOFqODE, the only
difference being the addition of run-time selectable class hieararchy (i.e.
quaternionSixDOF is derived from sixDOFODE instead of being stand-alone class).

Note: sixDofqODE is left for backward compatibility.
This commit is contained in:
Vuko Vukcevic 2017-02-24 15:42:26 +01:00 committed by Hrvoje Jasak
parent 6436f1a496
commit fd575d39b1
7 changed files with 1094 additions and 5 deletions

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@ -16,5 +16,6 @@ $(sixDOF)/sixDOFbodies/sixDOFbodies.C
$(sixDOF)/sixDOFODE/sixDOFODE.C $(sixDOF)/sixDOFODE/sixDOFODE.C
$(sixDOF)/sixDOFODE/newSixDOFODE.C $(sixDOF)/sixDOFODE/newSixDOFODE.C
$(sixDOF)/quaternionSixDOF/quaternionSixDOF.C
LIB = $(FOAM_LIBBIN)/libODE LIB = $(FOAM_LIBBIN)/libODE

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@ -0,0 +1,678 @@
/*---------------------------------------------------------------------------*\
========= |
\\ / F ield | foam-extend: Open Source CFD
\\ / O peration | Version: 4.0
\\ / A nd | Web: http://www.foam-extend.org
\\/ M anipulation | For copyright notice see file Copyright
-------------------------------------------------------------------------------
License
This file is part of foam-extend.
foam-extend is free software: you can redistribute it and/or modify it
under the terms of the GNU General Public License as published by the
Free Software Foundation, either version 3 of the License, or (at your
option) any later version.
foam-extend is distributed in the hope that it will be useful, but
WITHOUT ANY WARRANTY; without even the implied warranty of
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
General Public License for more details.
You should have received a copy of the GNU General Public License
along with foam-extend. If not, see <http://www.gnu.org/licenses/>.
Class
quaternionSixDOF
Description
6-DOF solver using quaternions
Author
Dubravko Matijasevic, FSB Zagreb. All rights reserved.
Hrvoje Jasak, FSB Zagreb. All rights reserved.
Vuko Vukcevic, FSB Zagreb. All rights reserved.
SourceFiles
quaternionSixDOF.C
\*---------------------------------------------------------------------------*/
#include "quaternionSixDOF.H"
#include "addToRunTimeSelectionTable.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
namespace Foam
{
defineTypeNameAndDebug(quaternionSixDOF, 0);
addToRunTimeSelectionTable(sixDOFODE, quaternionSixDOF, dictionary);
}
// * * * * * * * * * * * * * Private Member Functions * * * * * * * * * * * //
Foam::dimensionedVector Foam::quaternionSixDOF::A
(
const dimensionedVector& xR,
const dimensionedVector& uR,
const HamiltonRodriguezRot& rotation
) const
{
// Fix the global force for global rotation constraints
dimensionedVector fAbs = this->force();
// Constrain translation
constrainTranslation(fAbs.value());
return
(
- (linSpringCoeffs() & xR) // spring
- (linDampingCoeffs() & uR) // damping
+ fAbs
// To absolute
+ (rotation.invR() & forceRelative())
)/mass();
}
Foam::dimensionedVector Foam::quaternionSixDOF::OmegaDot
(
const HamiltonRodriguezRot& rotation,
const dimensionedVector& omega
) const
{
// Fix the global moment for global rotation constraints
dimensionedVector mAbs = moment();
// Constrain rotation
constrainRotation(mAbs.value());
return
inv(momentOfInertia())
& (
E(omega)
// To relative
+ (rotation.R() & mAbs)
+ momentRelative()
);
}
Foam::dimensionedVector Foam::quaternionSixDOF::E
(
const dimensionedVector& omega
) const
{
return (*(momentOfInertia() & omega) & omega);
}
void Foam::quaternionSixDOF::constrainRotation(vector& vec) const
{
// Constrain the vector with respect to referent or global coordinate system
if (referentMotionConstraints_)
{
vector consVec(referentRotation_.R() & vec);
if (fixedRoll_)
{
consVec.x() = 0;
}
if (fixedPitch_)
{
consVec.y() = 0;
}
if (fixedYaw_)
{
consVec.z() = 0;
}
vec = referentRotation_.invR() & consVec;
}
else
{
if (fixedRoll_)
{
vec.x() = 0;
}
if (fixedPitch_)
{
vec.y() = 0;
}
if (fixedYaw_)
{
vec.z() = 0;
}
}
}
void Foam::quaternionSixDOF::constrainTranslation(vector& vec) const
{
// Constrain the vector in respect to referent or global coordinate system
if (referentMotionConstraints_)
{
vector consVec(referentRotation_.R() & vec);
if (fixedSurge_)
{
consVec.x() = 0;
}
if (fixedSway_)
{
consVec.y() = 0;
}
if (fixedHeave_)
{
consVec.z() = 0;
}
vec = referentRotation_.invR() & consVec;
}
else
{
if (fixedSurge_)
{
vec.x() = 0;
}
if (fixedSway_)
{
vec.y() = 0;
}
if (fixedHeave_)
{
vec.z() = 0;
}
}
}
// * * * * * * * * * * * * Protected Member Functions * * * * * * * * * * * //
void Foam::quaternionSixDOF::setCoeffs()
{
// Set ODE coefficients from position and rotation
// Linear displacement relative to spring equilibrium
const vector& Xval = Xrel_.value();
coeffs_[0] = Xval.x();
coeffs_[1] = Xval.y();
coeffs_[2] = Xval.z();
// Linear velocity
const vector& Uval = U_.value();
coeffs_[3] = Uval.x();
coeffs_[4] = Uval.y();
coeffs_[5] = Uval.z();
// Rotational velocity in non - inertial coordinate system
const vector& omegaVal = omega_.value();
coeffs_[6] = omegaVal.x();
coeffs_[7] = omegaVal.y();
coeffs_[8] = omegaVal.z();
// Quaternions
coeffs_[9] = rotation_.eInitial().e0();
coeffs_[10] = rotation_.eInitial().e1();
coeffs_[11] = rotation_.eInitial().e2();
coeffs_[12] = rotation_.eInitial().e3();
}
// * * * * * * * * * * * * * * * * Constructors * * * * * * * * * * * * * * //
Foam::quaternionSixDOF::quaternionSixDOF(const IOobject& io)
:
sixDOFODE(io),
Xrel_(lookup("Xrel")),
U_(lookup("U")),
Uaverage_(U_),
rotation_
(
vector(lookup("rotationVector")),
dimensionedScalar(lookup("rotationAngle")).value()
),
omega_(lookup("omega")),
omegaAverage_(omega_),
omegaAverageAbsolute_(omega_),
coeffs_(13, 0.0),
fixedSurge_(lookup("fixedSurge")),
fixedSway_(lookup("fixedSway")),
fixedHeave_(lookup("fixedHeave")),
fixedRoll_(lookup("fixedRoll")),
fixedPitch_(lookup("fixedPitch")),
fixedYaw_(lookup("fixedYaw")),
referentMotionConstraints_
(
lookupOrDefault<Switch>
(
"referentMotionConstraints",
false
)
),
referentRotation_(vector(1, 0, 0), 0)
{
setCoeffs();
}
Foam::quaternionSixDOF::quaternionSixDOF
(
const word& name,
const quaternionSixDOF& qsd
)
:
sixDOFODE
(
IOobject
(
name,
qsd.instance(),
qsd.local(),
qsd.db(),
IOobject::NO_READ,
IOobject::NO_WRITE
)
),
Xrel_(qsd.Xrel_.name(), qsd.Xrel_),
U_(qsd.U_.name(), qsd.U_),
Uaverage_(qsd.Uaverage_.name(), qsd.Uaverage_),
rotation_(qsd.rotation_),
omega_(qsd.omega_.name(), qsd.omega_),
omegaAverage_(qsd.omegaAverage_.name(), qsd.omegaAverage_),
omegaAverageAbsolute_
(
qsd.omegaAverageAbsolute_.name(),
qsd.omegaAverageAbsolute_
),
coeffs_(qsd.coeffs_),
fixedSurge_(qsd.fixedSurge_),
fixedSway_(qsd.fixedSway_),
fixedHeave_(qsd.fixedHeave_),
fixedRoll_(qsd.fixedRoll_),
fixedPitch_(qsd.fixedPitch_),
fixedYaw_(qsd.fixedYaw_),
referentMotionConstraints_(qsd.referentMotionConstraints_),
referentRotation_(qsd.referentRotation_)
{}
Foam::autoPtr<Foam::sixDOFODE> Foam::quaternionSixDOF::clone
(
const word& name
) const
{
// Create and return an autoPtr to the new quaternionSixDOF object with a
// new name
return autoPtr<sixDOFODE>
(
new quaternionSixDOF
(
name,
*this
)
);
}
// * * * * * * * * * * * * * * * * Destructor * * * * * * * * * * * * * * * //
Foam::quaternionSixDOF::~quaternionSixDOF()
{}
// * * * * * * * * * * * * * * * Member Functions * * * * * * * * * * * * * //
const Foam::dimensionedVector& Foam::quaternionSixDOF::Xrel() const
{
return Xrel_;
}
const Foam::dimensionedVector& Foam::quaternionSixDOF::omega() const
{
return omega_;
}
Foam::dimensionedVector Foam::quaternionSixDOF::X() const
{
return Xequilibrium() + Xrel_;
}
const Foam::dimensionedVector& Foam::quaternionSixDOF::U() const
{
return U_;
}
const Foam::dimensionedVector& Foam::quaternionSixDOF::Uaverage() const
{
return Uaverage_;
}
const Foam::finiteRotation& Foam::quaternionSixDOF::rotation() const
{
return rotation_;
}
Foam::vector Foam::quaternionSixDOF::rotVector() const
{
return rotation_.rotVector();
}
Foam::dimensionedScalar Foam::quaternionSixDOF::rotAngle() const
{
return dimensionedScalar("rotAngle", dimless, rotation_.rotAngle());
}
void Foam::quaternionSixDOF::setXrel(const vector& x)
{
Xrel_.value() = x;
// Set X in coefficients
coeffs_[0] = x.x();
coeffs_[1] = x.y();
coeffs_[2] = x.z();
}
void Foam::quaternionSixDOF::setU(const vector& U)
{
U_.value() = U;
Uaverage_ = U_;
// Set U in coefficients
coeffs_[3] = U.x();
coeffs_[4] = U.y();
coeffs_[5] = U.z();
}
void Foam::quaternionSixDOF::setRotation(const HamiltonRodriguezRot& rot)
{
// Cannot call update rotation: simply set up coefficients
// HJ, 23/Mar/2015
coeffs_[9] = rot.e0();
coeffs_[10] = rot.e1();
coeffs_[11] = rot.e2();
coeffs_[12] = rot.e3();
}
void Foam::quaternionSixDOF::setOmega(const vector& omega)
{
omega_.value() = omega;
omegaAverage_ = omega_;
omegaAverageAbsolute_ = omega_;
// Set omega in coefficients
coeffs_[6] = omega.x();
coeffs_[7] = omega.y();
coeffs_[8] = omega.z();
}
void Foam::quaternionSixDOF::setReferentRotation
(
const HamiltonRodriguezRot& rot
)
{
referentRotation_ = rot;
referentMotionConstraints_ = true;
}
void Foam::quaternionSixDOF::setState(const sixDOFODE& sd)
{
// First set the state in base class subobject
sixDOFODE::setState(sd);
// Cast sixDOFODE& to quaternionSixDOF&
const quaternionSixDOF& qsd = refCast<const quaternionSixDOF>(sd);
// Set state variables for this class
Xrel_ = qsd.Xrel_;
U_ = qsd.U_;
Uaverage_ = qsd.Uaverage_;
rotation_ = qsd.rotation_;
omega_ = qsd.omega_;
omegaAverage_ = qsd.omegaAverage_;
omegaAverageAbsolute_ = qsd.omegaAverageAbsolute_;
// Copy ODE coefficients: this carries actual ODE state
// HJ, 23/Mar/2015
coeffs_ = qsd.coeffs_;
fixedSurge_ = qsd.fixedSurge_;
fixedSway_ = qsd.fixedSway_;
fixedHeave_ = qsd.fixedHeave_;
fixedRoll_ = qsd.fixedRoll_;
fixedPitch_ = qsd.fixedPitch_;
fixedYaw_ = qsd.fixedYaw_;
referentMotionConstraints_ = qsd.referentMotionConstraints_;
referentRotation_ = qsd.referentRotation_;
}
Foam::vector Foam::quaternionSixDOF::rotVectorAverage() const
{
return rotation_.rotVectorAverage();
}
const Foam::dimensionedVector& Foam::quaternionSixDOF::omegaAverage() const
{
return omegaAverage_;
}
const Foam::dimensionedVector&
Foam::quaternionSixDOF::omegaAverageAbsolute() const
{
return omegaAverageAbsolute_;
}
Foam::tensor Foam::quaternionSixDOF::toRelative() const
{
return rotation_.eCurrent().R();
}
Foam::tensor Foam::quaternionSixDOF::toAbsolute() const
{
return rotation_.eCurrent().invR();
}
const Foam::tensor& Foam::quaternionSixDOF::rotIncrementTensor() const
{
return rotation_.rotIncrementTensor();
}
void Foam::quaternionSixDOF::derivatives
(
const scalar x,
const scalarField& y,
scalarField& dydx
) const
{
// Set the derivatives for displacement
dydx[0] = y[3];
dydx[1] = y[4];
dydx[2] = y[5];
dimensionedVector curX("curX", dimLength, vector(y[0], y[1], y[2]));
dimensionedVector curU("curU", dimVelocity, vector(y[3], y[4], y[5]));
const HamiltonRodriguezRot curRotation
(
y[9],
y[10],
y[11],
y[12]
);
const vector accel = A(curX, curU, curRotation).value();
dydx[3] = accel.x();
dydx[4] = accel.y();
dydx[5] = accel.z();
// Set the derivatives for rotation
dimensionedVector curOmega
(
"curOmega",
dimless/dimTime,
vector(y[6], y[7], y[8])
);
const vector omegaDot = OmegaDot(curRotation, curOmega).value();
dydx[6] = omegaDot.x();
dydx[7] = omegaDot.y();
dydx[8] = omegaDot.z();
dydx[9] = curRotation.eDot(curOmega.value(), 0);
dydx[10] = curRotation.eDot(curOmega.value(), 1);
dydx[11] = curRotation.eDot(curOmega.value(), 2);
dydx[12] = curRotation.eDot(curOmega.value(), 3);
// Add rotational constraints by setting RHS of given components to zero
if (fixedRoll_)
{
dydx[10] = 0; // Roll axis (roll quaternion evolution RHS)
}
if (fixedPitch_)
{
dydx[11] = 0; // Pitch axis (pitch quaternion evolution RHS)
}
if (fixedYaw_)
{
dydx[12] = 0; // Yaw axis (yaw quaternion evolution RHS)
}
}
void Foam::quaternionSixDOF::update(const scalar delta)
{
// Update position
vector Xold = Xrel_.value();
vector& Xval = Xrel_.value();
Xval.x() = coeffs_[0];
Xval.y() = coeffs_[1];
Xval.z() = coeffs_[2];
// Update velocity
Uaverage_.value() = (Xval - Xold)/delta;
vector& Uval = U_.value();
Uval.x() = coeffs_[3];
Uval.y() = coeffs_[4];
Uval.z() = coeffs_[5];
// Constrain velocity
constrainTranslation(Uval);
coeffs_[3] = Uval.x();
coeffs_[4] = Uval.y();
coeffs_[5] = Uval.z();
// Update omega
vector& omegaVal = omega_.value();
omegaVal.x() = coeffs_[6];
omegaVal.y() = coeffs_[7];
omegaVal.z() = coeffs_[8];
// Constrain omega
constrainRotation(omegaVal);
coeffs_[6] = omegaVal.x();
coeffs_[7] = omegaVal.y();
coeffs_[8] = omegaVal.z();
rotation_.updateRotation
(
HamiltonRodriguezRot
(
coeffs_[9],
coeffs_[10],
coeffs_[11],
coeffs_[12]
)
);
omegaAverage_.value() = rotation_.omegaAverage(delta);
// Calculate and constrain omegaAverageAbsolute appropriately
vector& omegaAverageAbsoluteValue = omegaAverageAbsolute_.value();
omegaAverageAbsoluteValue = rotation_.omegaAverageAbsolute(delta);
if (fixedRoll_)
{
omegaAverageAbsoluteValue.x() = 0;
}
if (fixedPitch_)
{
omegaAverageAbsoluteValue.y() = 0;
}
if (fixedYaw_)
{
omegaAverageAbsoluteValue.z() = 0;
}
}
bool Foam::quaternionSixDOF::writeData(Ostream& os) const
{
// First write the part related to base class subobject
sixDOFODE::writeData(os);
// Write type name
os.writeKeyword("type") << tab << type() << token::END_STATEMENT << endl;
// Write data
os.writeKeyword("Xrel") << tab << this->Xrel()
<< token::END_STATEMENT << nl;
os.writeKeyword("U") << tab << this->U() << token::END_STATEMENT << nl;
os.writeKeyword("rotationVector") << tab << this->rotVector()
<< token::END_STATEMENT << nl;
os.writeKeyword("rotationAngle") << tab << this->rotAngle()
<< token::END_STATEMENT << nl;
os.writeKeyword("omega") << tab << this->omega()
<< token::END_STATEMENT << nl << nl;
os.writeKeyword("fixedSurge") << tab << this->fixedSurge_ <<
token::END_STATEMENT << endl;
os.writeKeyword("fixedSway") << tab << this->fixedSway_ <<
token::END_STATEMENT << endl;
os.writeKeyword("fixedHeave") << tab << this->fixedHeave_ <<
token::END_STATEMENT << endl;
os.writeKeyword("fixedRoll") << tab << this->fixedRoll_ <<
token::END_STATEMENT << endl;
os.writeKeyword("fixedPitch") << tab << this->fixedPitch_ <<
token::END_STATEMENT << endl;
os.writeKeyword("fixedYaw") << tab << this->fixedYaw_ <<
token::END_STATEMENT << endl;
return os.good();
}
// ************************************************************************* //

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@ -0,0 +1,351 @@
/*---------------------------------------------------------------------------*\
========= |
\\ / F ield | foam-extend: Open Source CFD
\\ / O peration | Version: 4.0
\\ / A nd | Web: http://www.foam-extend.org
\\/ M anipulation | For copyright notice see file Copyright
-------------------------------------------------------------------------------
License
This file is part of foam-extend.
foam-extend is free software: you can redistribute it and/or modify it
under the terms of the GNU General Public License as published by the
Free Software Foundation, either version 3 of the License, or (at your
option) any later version.
foam-extend is distributed in the hope that it will be useful, but
WITHOUT ANY WARRANTY; without even the implied warranty of
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
General Public License for more details.
You should have received a copy of the GNU General Public License
along with foam-extend. If not, see <http://www.gnu.org/licenses/>.
Class
quaternionSixDOF
Description
6-DOF solver using quaternions
Author
Dubravko Matijasevic, FSB Zagreb. All rights reserved.
Hrvoje Jasak, FSB Zagreb. All rights reserved.
Vuko Vukcevic, FSB Zagreb. All rights reserved.
SourceFiles
quaternionSixDOF.C
\*---------------------------------------------------------------------------*/
#ifndef quaternionSixDOF_H
#define quaternionSixDOF_H
#include "sixDOFODE.H"
#include "finiteRotation.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
namespace Foam
{
/*---------------------------------------------------------------------------*\
Class quaternionSixDOF Declaration
\*---------------------------------------------------------------------------*/
class quaternionSixDOF
:
public sixDOFODE
{
// Private data
// Initial body state variables
//- Displacement relative to spring equilibrium
dimensionedVector Xrel_;
//- Velocity of mass centroid
dimensionedVector U_;
//- Average velocity of mass centroid at previous time-step
dimensionedVector Uaverage_;
//- Finite rotation
finiteRotation rotation_;
//- Rotational velocity about mass centroid
dimensionedVector omega_;
// Average variables that need to be stored
//- Average rotational velocity in relative coordinate system
dimensionedVector omegaAverage_;
//- Average rotational velocity in absolute coordinate system
dimensionedVector omegaAverageAbsolute_;
//- ODE coefficients
scalarField coeffs_;
//- Motion constraints (given as fixed motion components)
//- Fixed surge (x-translation)
Switch fixedSurge_;
//- Fixed sway (y-translation)
Switch fixedSway_;
//- Fixed heave (z-translation)
Switch fixedHeave_;
//- Fixed roll (rotation around x)
Switch fixedRoll_;
//- Fixed pitch (rotation around y)
Switch fixedPitch_;
//- Fixed yaw (rotation around z)
Switch fixedYaw_;
//- Restraints in referent coordinate system
Switch referentMotionConstraints_;
//- Rotation of referent coordinate system
HamiltonRodriguezRot referentRotation_;
// Private Member Functions
//- Disallow default bitwise copy construct
quaternionSixDOF(const quaternionSixDOF&);
//- Disallow default bitwise assignment
void operator=(const quaternionSixDOF&);
// Variables in relative coordinate system (solved for)
//- Return acceleration in relative coordinate system
// given current values of relative displacement and velocity
dimensionedVector A
(
const dimensionedVector& xR,
const dimensionedVector& uR,
const HamiltonRodriguezRot& rotation
) const;
//- Return rotational acceleration in relative coordinate system
// given current values for relative rotational velocity
dimensionedVector OmegaDot
(
const HamiltonRodriguezRot& rotation,
const dimensionedVector& omega
) const;
//- Return the Euler part of moment equation
dimensionedVector E
(
const dimensionedVector& omega
) const;
//- Constrain rotation vector in referent or global coordinate
// system
void constrainRotation(vector& vec) const;
//- Constrain translation vector in referent or global coordinate
// system
void constrainTranslation(vector& vec) const;
protected:
// Protected Member Functions
//- Set ODE coefficients from position and rotation
virtual void setCoeffs();
public:
// Run-time type information
TypeName("quaternionSixDOF");
// Constructors
//- Construct from dictionary
quaternionSixDOF(const IOobject& io);
//- Construct quaternionSixDOF object, changing name
quaternionSixDOF
(
const word& name,
const quaternionSixDOF& qsd
);
//- Return a clone, changing the name
virtual autoPtr<sixDOFODE> clone(const word& name) const;
// Destructor
virtual ~quaternionSixDOF();
// Member Functions
// Virtual interface for 6DOF motion state
// Variables in relative coordinate system
//- Return displacement in translated coordinate system
// relative to spring equilibrium
virtual const dimensionedVector& Xrel() const;
//- Return rotational velocity in relative coordinate system
virtual const dimensionedVector& omega() const;
// Displacement and rotation in the absolute coordinate system
//- Return position of origin in absolute coordinate system
virtual dimensionedVector X() const;
//- Return velocity of origin
virtual const dimensionedVector& U() const;
//- Return average velocity of origin for the previous time-step
virtual const dimensionedVector& Uaverage() const;
//- Return finite rotation
virtual const finiteRotation& rotation() const;
//- Return rotational vector of body
virtual vector rotVector() const;
//- Return rotation angle of body
virtual dimensionedScalar rotAngle() const;
// Non-access control for setting state variables
//- Set position of origin
virtual void setXrel(const vector& x);
//- Set velocity of origin
virtual void setU(const vector& u);
//- Set rotational angle in relative coordinate system
virtual void setRotation(const HamiltonRodriguezRot& rot);
//- Set rotational velocity in relative coordinate system
virtual void setOmega(const vector& omega);
//- Set referent coordinate system to apply constraints
virtual void setReferentRotation
(
const HamiltonRodriguezRot& rot
);
//- Set ODE parameters from another ODE
virtual void setState(const sixDOFODE&);
// Average motion per time-step
//- Return average rotational vector of body
virtual vector rotVectorAverage() const;
//- Return average rotational velocity in relative coordinate
// system
virtual const dimensionedVector& omegaAverage() const;
//- Return average rotational velocity in absolute coordinate
// system
virtual const dimensionedVector& omegaAverageAbsolute() const;
// Rotations
//- Return rotation tensor to relative coordinate system
virtual tensor toRelative() const;
//- Return rotation tensor to absolute coordinate system
virtual tensor toAbsolute() const;
//- Return transformation tensor between new and previous
// rotation
virtual const tensor& rotIncrementTensor() const;
// ODE parameters
//- Return number of equations
virtual label nEqns() const
{
return 13;
}
//- Return access to coefficients
virtual scalarField& coeffs()
{
return coeffs_;
}
//- Return reference to coefficients
virtual const scalarField& coeffs() const
{
return coeffs_;
}
//- Evaluate derivatives
virtual void derivatives
(
const scalar x,
const scalarField& y,
scalarField& dydx
) const;
//- Evaluate Jacobian
virtual void jacobian
(
const scalar x,
const scalarField& y,
scalarField& dfdx,
scalarSquareMatrix& dfdy
) const
{
notImplemented
(
"quaternionSixDOF::jacobian\n"
"(\n"
" const scalar x,\n"
" const scalarField& y,\n"
" scalarField& dfdx,\n"
" scalarSquareMatrix& dfdy,\n"
") const"
);
}
//- Update ODE after the solution, advancing by delta
virtual void update(const scalar delta);
// Write controls
//- WriteData member function required by regIOobject
virtual bool writeData(Ostream&) const;
};
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
} // End namespace Foam
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
#endif
// ************************************************************************* //

View file

@ -22,6 +22,18 @@ License
along with OpenFOAM; if not, write to the Free Software Foundation, along with OpenFOAM; if not, write to the Free Software Foundation,
Inc., 51 Franklin St, Fifth Floor, Boston, MA 02110-1301 USA Inc., 51 Franklin St, Fifth Floor, Boston, MA 02110-1301 USA
Class
sixDOFODE
Description
Abstract base class for six-degrees-of-freedom (6DOF) ordinary differential
equations
Author
Dubravko Matijasevic, FSB Zagreb. All rights reserved.
Hrvoje Jasak, FSB Zagreb. All rights reserved.
Vuko Vukcevic, FSB Zagreb. All rights reserved.
\*---------------------------------------------------------------------------*/ \*---------------------------------------------------------------------------*/
#include "error.H" #include "error.H"

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@ -209,7 +209,25 @@ void Foam::sixDOFODE::relaxAcceleration
} }
// * * * * * * * * * * * * * * * Friend Operators * * * * * * * * * * * * * // void Foam::sixDOFODE::setState(const sixDOFODE& sd)
{
// Set state does not copy AList_, AOld_, relaxFactor_ and
// relaxFactorOld_. In case of multiple updates, overwriting Aitkens
// relaxation parameters would invalidate the underrelaxation.
// IG, 5/May/2016
mass_ = sd.mass_;
momentOfInertia_ = sd.momentOfInertia_;
Xequilibrium_ = sd.Xequilibrium_;
linSpringCoeffs_ = sd.linSpringCoeffs_;
linDampingCoeffs_ = sd.linDampingCoeffs_;
force_ = sd.force_;
moment_ = sd.moment_;
forceRelative_ = sd.forceRelative_;
momentRelative_ = sd.momentRelative_;
}
bool Foam::sixDOFODE::writeData(Ostream& os) const bool Foam::sixDOFODE::writeData(Ostream& os) const
{ {

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@ -182,7 +182,6 @@ public:
//- Return autoPtr to the selected sixDOFODE //- Return autoPtr to the selected sixDOFODE
static autoPtr<sixDOFODE> New(const IOobject& io); static autoPtr<sixDOFODE> New(const IOobject& io);
// Destructor // Destructor
virtual ~sixDOFODE(); virtual ~sixDOFODE();
@ -210,6 +209,12 @@ public:
//- Return access to equilibrium position of origin //- Return access to equilibrium position of origin
inline dimensionedVector& Xequilibrium(); inline dimensionedVector& Xequilibrium();
//- Return linear spring coefficient
inline const dimensionedDiagTensor& linSpringCoeffs() const;
//- Return linear damping coefficient
inline const dimensionedDiagTensor& linDampingCoeffs() const;
// Access to forces and moments // Access to forces and moments
@ -304,6 +309,9 @@ public:
const HamiltonRodriguezRot& rot const HamiltonRodriguezRot& rot
) = 0; ) = 0;
//- Set ODE parameters from another ODE
virtual void setState(const sixDOFODE&);
// Average motion per time-step // Average motion per time-step
@ -332,9 +340,6 @@ public:
// rotation // rotation
virtual const tensor& rotIncrementTensor() const = 0; virtual const tensor& rotIncrementTensor() const = 0;
//- Set ODE parameters from another ODE
virtual void setState(const sixDOFODE&) = 0;
// ODE parameters // ODE parameters

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@ -21,6 +21,18 @@ License
You should have received a copy of the GNU General Public License You should have received a copy of the GNU General Public License
along with foam-extend. If not, see <http://www.gnu.org/licenses/>. along with foam-extend. If not, see <http://www.gnu.org/licenses/>.
Class
sixDOFODE
Description
Abstract base class for six-degrees-of-freedom (6DOF) ordinary differential
equations
Author
Dubravko Matijasevic, FSB Zagreb. All rights reserved.
Hrvoje Jasak, FSB Zagreb. All rights reserved.
Vuko Vukcevic, FSB Zagreb. All rights reserved.
\*---------------------------------------------------------------------------*/ \*---------------------------------------------------------------------------*/
// * * * * * * * * * * * * * * * Member Functions * * * * * * * * * * * * * // // * * * * * * * * * * * * * * * Member Functions * * * * * * * * * * * * * //
@ -61,6 +73,18 @@ Foam::dimensionedVector& Foam::sixDOFODE::Xequilibrium()
} }
const Foam::dimensionedDiagTensor& Foam::sixDOFODE::linSpringCoeffs() const
{
return linSpringCoeffs_;
}
const Foam::dimensionedDiagTensor& Foam::sixDOFODE::linDampingCoeffs() const
{
return linDampingCoeffs_;
}
const Foam::dimensionedVector& Foam::sixDOFODE::force() const const Foam::dimensionedVector& Foam::sixDOFODE::force() const
{ {
return force_; return force_;