public class MassEquation extends Object implements AdditionalEquations
MassProvider,
Serialized Form| Modifier and Type | Field and Description |
|---|---|
static String |
PREFIX
Default prefix for mass equation
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| Constructor and Description |
|---|
MassEquation()
Empty constructor for
Externalizable use. |
MassEquation(String partName)
Create a new mass equation, for a given part.
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| Modifier and Type | Method and Description |
|---|---|
void |
addMassDerivative(double flow)
Set the flow rate.
|
double[] |
buildAdditionalState(double[] y,
double[] yDot)
Build full first order additional state from second order y and yDot.
|
void |
computeDerivatives(SpacecraftState s,
TimeDerivativesEquations adder)
Compute the derivatives related to the additional state parameters.
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double[] |
computeSecondDerivatives(SpacecraftState s)
Compute the second derivatives related to the additional state parameters.
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double[] |
extractY(double[] additionalState)
Retrieve second order additional state y from full first order additional state.
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double[] |
extractYDot(double[] additionalState)
Retrieve second order additional state derivative yDot from full first order additional state.
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static String |
genName(String name)
Generate a name in the form "MASS_
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int |
getFirstOrderDimension()
Returns the number of first order additional states.
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String |
getName()
Get the name of the additional equation.
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int |
getSecondOrderDimension()
Returns the number of second order additional states.
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void |
readExternal(ObjectInput oi) |
void |
setMassDerivativeZero()
Set the flow rate to zero.
|
void |
writeExternal(ObjectOutput oo) |
public static final String PREFIX
public MassEquation()
Externalizable use.public MassEquation(String partName)
partName - name of part subject to this equationpublic String getName()
getName in interface AdditionalEquationspublic void computeDerivatives(SpacecraftState s, TimeDerivativesEquations adder) throws PatriusException
computeDerivatives in interface AdditionalEquationss - current state information: date, kinematics, attitude, additional statesadder - object where the contribution of the additional parameters
to the orbit evolution (accelerations) should be addedPatriusException - if some specific error occurspublic void setMassDerivativeZero()
public void addMassDerivative(double flow)
flow - ratepublic static String genName(String name)
name - part namepublic double[] computeSecondDerivatives(SpacecraftState s) throws PatriusException
CowellIntegrator.computeSecondDerivatives in interface AdditionalEquationss - current state information: date, kinematics, attitude, additional statesPatriusException - if some specific error occurspublic int getFirstOrderDimension()
CowellIntegrator.getFirstOrderDimension in interface AdditionalEquationspublic int getSecondOrderDimension()
CowellIntegrator.getSecondOrderDimension in interface AdditionalEquationspublic double[] buildAdditionalState(double[] y,
double[] yDot)
CowellIntegrator.buildAdditionalState in interface AdditionalEquationsy - second order additional state yyDot - second order additional state derivative yDotpublic double[] extractY(double[] additionalState)
CowellIntegrator.extractY in interface AdditionalEquationsadditionalState - full first order additional statepublic double[] extractYDot(double[] additionalState)
CowellIntegrator.extractYDot in interface AdditionalEquationsadditionalState - full first order additional statepublic void writeExternal(ObjectOutput oo) throws IOException
writeExternal in interface ExternalizableIOExceptionpublic void readExternal(ObjectInput oi) throws IOException, ClassNotFoundException
readExternal in interface ExternalizableIOExceptionClassNotFoundExceptionCopyright © 2025 CNES. All rights reserved.