Motion constraints in sixDOFqODE

This commit is contained in:
Vuko Vukcevic 2015-10-23 13:43:35 +02:00
parent 5e78a541c5
commit 4de19563e9
7 changed files with 138 additions and 11 deletions

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@ -1,9 +1,9 @@
/*---------------------------------------------------------------------------*\ /*---------------------------------------------------------------------------*\
========= | ========= |
\\ / F ield | foam-extend: Open Source CFD \\ / F ield | foam-extend: Open Source CFD
\\ / O peration | Version: 3.2 \\ / O peration |
\\ / A nd | Web: http://www.foam-extend.org \\ / A nd | For copyright notice see file Copyright
\\/ M anipulation | For copyright notice see file Copyright \\/ M anipulation |
------------------------------------------------------------------------------- -------------------------------------------------------------------------------
License License
This file is part of foam-extend. This file is part of foam-extend.
@ -72,7 +72,7 @@ Foam::scalar Foam::finiteRotation::rotAngle(const tensor& rotT)
Foam::vector Foam::finiteRotation::eulerAngles(const tensor& rotT) Foam::vector Foam::finiteRotation::eulerAngles(const tensor& rotT)
{ {
// Define a vector containing euler angles (x = roll, y = pitch, z = yaw) // Create a vector containing euler angles (x = roll, y = pitch, z = yaw)
vector eulerAngles; vector eulerAngles;
scalar& rollAngle = eulerAngles.x(); scalar& rollAngle = eulerAngles.x();

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@ -1,9 +1,9 @@
/*---------------------------------------------------------------------------*\ /*---------------------------------------------------------------------------*\
========= | ========= |
\\ / F ield | foam-extend: Open Source CFD \\ / F ield | foam-extend: Open Source CFD
\\ / O peration | Version: 3.2 \\ / O peration |
\\ / A nd | Web: http://www.foam-extend.org \\ / A nd | For copyright notice see file Copyright
\\/ M anipulation | For copyright notice see file Copyright \\/ M anipulation |
------------------------------------------------------------------------------- -------------------------------------------------------------------------------
License License
This file is part of foam-extend. This file is part of foam-extend.
@ -69,7 +69,7 @@ class finiteRotation
//- Calculate rotation angle from given rotation tensor //- Calculate rotation angle from given rotation tensor
static scalar rotAngle(const tensor& rotT); static scalar rotAngle(const tensor& rotT);
//- Calculate Euler angles (x-y-z (roll-pitch-yaw) convenction) from //- Calculate Euler angles (x-y-z (roll-pitch-yaw) convention) from
// given rotation tensor. Reference: Mike Day, Insomniac Games, // given rotation tensor. Reference: Mike Day, Insomniac Games,
// Extracting Euler Angles from a Rotation Matrix. // Extracting Euler Angles from a Rotation Matrix.
static vector eulerAngles(const tensor& rotT); static vector eulerAngles(const tensor& rotT);

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@ -118,11 +118,14 @@ Foam::dimensionedVector Foam::sixDOFqODE::E
Foam::sixDOFqODE::sixDOFqODE(const IOobject& io) Foam::sixDOFqODE::sixDOFqODE(const IOobject& io)
: :
IOdictionary(io), IOdictionary(io),
mass_(lookup("mass")), mass_(lookup("mass")),
momentOfInertia_(lookup("momentOfInertia")), momentOfInertia_(lookup("momentOfInertia")),
Xequilibrium_(lookup("equilibriumPosition")), Xequilibrium_(lookup("equilibriumPosition")),
linSpringCoeffs_(lookup("linearSpring")), linSpringCoeffs_(lookup("linearSpring")),
linDampingCoeffs_(lookup("linearDamping")), linDampingCoeffs_(lookup("linearDamping")),
Xrel_(lookup("Xrel")), Xrel_(lookup("Xrel")),
U_(lookup("U")), U_(lookup("U")),
Uaverage_(U_), Uaverage_(U_),
@ -134,11 +137,20 @@ Foam::sixDOFqODE::sixDOFqODE(const IOobject& io)
omega_(lookup("omega")), omega_(lookup("omega")),
omegaAverage_(omega_), omegaAverage_(omega_),
omegaAverageAbsolute_(omega_), omegaAverageAbsolute_(omega_),
force_(lookup("force")), force_(lookup("force")),
moment_(lookup("moment")), moment_(lookup("moment")),
forceRelative_(lookup("forceRelative")), forceRelative_(lookup("forceRelative")),
momentRelative_(lookup("momentRelative")), momentRelative_(lookup("momentRelative")),
coeffs_(13, 0.0)
coeffs_(13, 0.0),
fixedSurge_(lookup("fixedSurge")),
fixedSway_(lookup("fixedSway")),
fixedHeave_(lookup("fixedHeave")),
fixedRoll_(lookup("fixedRoll")),
fixedPitch_(lookup("fixedPitch")),
fixedYaw_(lookup("fixedYaw"))
{ {
setCoeffs(); setCoeffs();
} }
@ -163,11 +175,14 @@ Foam::sixDOFqODE::sixDOFqODE
IOobject::NO_WRITE IOobject::NO_WRITE
) )
), ),
mass_(sd.mass_.name(), sd.mass_), mass_(sd.mass_.name(), sd.mass_),
momentOfInertia_(sd.momentOfInertia_.name(), sd.momentOfInertia_), momentOfInertia_(sd.momentOfInertia_.name(), sd.momentOfInertia_),
Xequilibrium_(sd.Xequilibrium_.name(), sd.Xequilibrium_), Xequilibrium_(sd.Xequilibrium_.name(), sd.Xequilibrium_),
linSpringCoeffs_(sd.linSpringCoeffs_.name(), sd.linSpringCoeffs_), linSpringCoeffs_(sd.linSpringCoeffs_.name(), sd.linSpringCoeffs_),
linDampingCoeffs_(sd.linDampingCoeffs_.name(), sd.linDampingCoeffs_), linDampingCoeffs_(sd.linDampingCoeffs_.name(), sd.linDampingCoeffs_),
Xrel_(sd.Xrel_.name(), sd.Xrel_), Xrel_(sd.Xrel_.name(), sd.Xrel_),
U_(sd.U_.name(), sd.U_), U_(sd.U_.name(), sd.U_),
Uaverage_(sd.Uaverage_.name(), sd.Uaverage_), Uaverage_(sd.Uaverage_.name(), sd.Uaverage_),
@ -179,11 +194,20 @@ Foam::sixDOFqODE::sixDOFqODE
sd.omegaAverageAbsolute_.name(), sd.omegaAverageAbsolute_.name(),
sd.omegaAverageAbsolute_ sd.omegaAverageAbsolute_
), ),
force_(sd.force_.name(), sd.force_), force_(sd.force_.name(), sd.force_),
moment_(sd.moment_.name(), sd.moment_), moment_(sd.moment_.name(), sd.moment_),
forceRelative_(sd.forceRelative_.name(), sd.forceRelative_), forceRelative_(sd.forceRelative_.name(), sd.forceRelative_),
momentRelative_(sd.momentRelative_.name(), sd.momentRelative_), momentRelative_(sd.momentRelative_.name(), sd.momentRelative_),
coeffs_(sd.coeffs_)
coeffs_(sd.coeffs_),
fixedSurge_(sd.fixedSurge_),
fixedSway_(sd.fixedSway_),
fixedHeave_(sd.fixedHeave_),
fixedRoll_(sd.fixedRoll_),
fixedPitch_(sd.fixedPitch_),
fixedYaw_(sd.fixedYaw_)
{} {}
@ -199,9 +223,11 @@ void Foam::sixDOFqODE::setState(const sixDOFqODE& sd)
{ {
mass_ = sd.mass_; mass_ = sd.mass_;
momentOfInertia_ = sd.momentOfInertia_; momentOfInertia_ = sd.momentOfInertia_;
Xequilibrium_ = sd.Xequilibrium_; Xequilibrium_ = sd.Xequilibrium_;
linSpringCoeffs_ = sd.linSpringCoeffs_; linSpringCoeffs_ = sd.linSpringCoeffs_;
linDampingCoeffs_ = sd.linDampingCoeffs_; linDampingCoeffs_ = sd.linDampingCoeffs_;
Xrel_ = sd.Xrel_; Xrel_ = sd.Xrel_;
U_ = sd.U_; U_ = sd.U_;
Uaverage_ = sd.Uaverage_; Uaverage_ = sd.Uaverage_;
@ -209,6 +235,7 @@ void Foam::sixDOFqODE::setState(const sixDOFqODE& sd)
omega_ = sd.omega_; omega_ = sd.omega_;
omegaAverage_ = sd.omegaAverage_; omegaAverage_ = sd.omegaAverage_;
omegaAverageAbsolute_ = sd.omegaAverageAbsolute_; omegaAverageAbsolute_ = sd.omegaAverageAbsolute_;
force_ = sd.force_; force_ = sd.force_;
moment_ = sd.moment_; moment_ = sd.moment_;
forceRelative_ = sd.forceRelative_; forceRelative_ = sd.forceRelative_;
@ -217,6 +244,13 @@ void Foam::sixDOFqODE::setState(const sixDOFqODE& sd)
// Copy ODE coefficients: this carries actual ODE state // Copy ODE coefficients: this carries actual ODE state
// HJ, 23/Mar/2015 // HJ, 23/Mar/2015
coeffs_ = sd.coeffs_; coeffs_ = sd.coeffs_;
fixedSurge_ = sd.fixedSurge_;
fixedSway_ = sd.fixedSway_;
fixedHeave_ = sd.fixedHeave_;
fixedRoll_ = sd.fixedRoll_;
fixedPitch_ = sd.fixedPitch_;
fixedYaw_ = sd.fixedYaw_;
} }
@ -248,6 +282,23 @@ void Foam::sixDOFqODE::derivatives
dydx[4] = accel.y(); dydx[4] = accel.y();
dydx[5] = accel.z(); dydx[5] = accel.z();
// Add translational constraints by setting RHS of given components to zero
if (fixedSurge_)
{
dydx[0] = 0; // Surge velocity
dydx[3] = 0; // Surge acceleration
}
if (fixedSway_)
{
dydx[1] = 0; // Sway velocity
dydx[4] = 0; // Sway acceleration
}
if (fixedHeave_)
{
dydx[2] = 0; // Heave velocity
dydx[5] = 0; // Heave acceleration
}
// Set the derivatives for rotation // Set the derivatives for rotation
dimensionedVector curOmega dimensionedVector curOmega
( (
@ -266,6 +317,23 @@ void Foam::sixDOFqODE::derivatives
dydx[10] = curRotation.eDot(curOmega.value(), 1); dydx[10] = curRotation.eDot(curOmega.value(), 1);
dydx[11] = curRotation.eDot(curOmega.value(), 2); dydx[11] = curRotation.eDot(curOmega.value(), 2);
dydx[12] = curRotation.eDot(curOmega.value(), 3); dydx[12] = curRotation.eDot(curOmega.value(), 3);
// Add rotational constraints by setting RHS of given components to zero
if (fixedRoll_)
{
dydx[6] = 0; // Roll angular acceleration
dydx[10] = 0; // Roll angular velocity (roll quaternion evolution RHS)
}
if (fixedPitch_)
{
dydx[7] = 0; // Pitch angular acceleration
dydx[11] = 0; // Pitch angular velocity (pitch quaternion evolution RHS)
}
if (fixedYaw_)
{
dydx[8] = 0; // Yaw angular acceleration
dydx[12] = 0; // Yaw angular velocity (yaw quaternion evolution RHS)
}
} }
@ -367,6 +435,19 @@ Foam::Ostream& Foam::operator<<(Ostream& os, const sixDOFqODE& sds)
os.writeKeyword("momentRelative") << tab << sds.momentRelative() os.writeKeyword("momentRelative") << tab << sds.momentRelative()
<< token::END_STATEMENT << endl; << token::END_STATEMENT << endl;
os.writeKeyword("fixedSurge") << tab << sds.fixedSurge_ <<
token::END_STATEMENT << endl;
os.writeKeyword("fixedSway") << tab << sds.fixedSway_ <<
token::END_STATEMENT << endl;
os.writeKeyword("fixedHeave") << tab << sds.fixedHeave_ <<
token::END_STATEMENT << endl;
os.writeKeyword("fixedRoll") << tab << sds.fixedRoll_ <<
token::END_STATEMENT << endl;
os.writeKeyword("fixedPitch") << tab << sds.fixedPitch_ <<
token::END_STATEMENT << endl;
os.writeKeyword("fixedYaw") << tab << sds.fixedYaw_ <<
token::END_STATEMENT << endl;
return os; return os;
} }

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@ -131,6 +131,27 @@ class sixDOFqODE
scalarField coeffs_; 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_;
// Private Member Functions // Private Member Functions
//- Disallow default bitwise copy construct //- Disallow default bitwise copy construct

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@ -36,4 +36,12 @@ moment m [1 2 -2 0 0 0 0] (0 0 0);
forceRelative fRel [1 1 -2 0 0 0 0] (0 0 0); forceRelative fRel [1 1 -2 0 0 0 0] (0 0 0);
momentRelative mRel [1 2 -2 0 0 0 0] (-0.5773502692 -0.5773502692 -0.5773502692); momentRelative mRel [1 2 -2 0 0 0 0] (-0.5773502692 -0.5773502692 -0.5773502692);
// Motion constraints
fixedSurge no;
fixedSway no;
fixedHeave no;
fixedRoll no;
fixedPitch no;
fixedYaw no;
// ************************************************************************* // // ************************************************************************* //

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@ -35,4 +35,12 @@ moment m [1 2 -2 0 0 0 0] (0 0 0);
forceRelative fRel [1 1 -2 0 0 0 0] (0 0 0); forceRelative fRel [1 1 -2 0 0 0 0] (0 0 0);
momentRelative mRel [1 2 -2 0 0 0 0] (0 0 10); momentRelative mRel [1 2 -2 0 0 0 0] (0 0 10);
// Motion constraints
fixedSurge no;
fixedSway no;
fixedHeave no;
fixedRoll no;
fixedPitch no;
fixedYaw no;
// ************************************************************************* // // ************************************************************************* //

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@ -35,4 +35,13 @@ moment m [1 2 -2 0 0 0 0] (0 0 0);
forceRelative fRel [1 1 -2 0 0 0 0] (0 0 0); forceRelative fRel [1 1 -2 0 0 0 0] (0 0 0);
momentRelative mRel [1 2 -2 0 0 0 0] (0 0 0); momentRelative mRel [1 2 -2 0 0 0 0] (0 0 0);
// Motion constraints
fixedSurge no;
fixedSway no;
fixedHeave no;
fixedRoll no;
fixedPitch no;
fixedYaw no;
// ************************************************************************* // // ************************************************************************* //