PhysicalProperties (ORbit Extrapolation KIT 11.1.2 API)

java.lang.Object
- org.orekit.files.ccsds.section.CommentsContainer
- - org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties

All Implemented Interfaces:

Section
```
public class PhysicalProperties
extends CommentsContainer
```
Spacecraft physical properties.

Since:

11.0

Author:

Luc Maisonobe

Method Summary

All Methods Instance Methods Concrete Methods
Modifier and Type	Method and Description
`String`	`getAttitudeActuatorType()` Get the type of actuator for attitude control.
`double`	`getAttitudeControlAccuracy()` Get the accuracy of attitude control.
`String`	`getAttitudeControlMode()` Get the attitude control mode.
`double`	`getAttitudeKnowledgeAccuracy()` Get the accuracy of attitude knowledge.
`double`	`getAttitudePointingAccuracy()` Get the overall accuracy of spacecraft to maintain attitude.
`double`	`getBolDv()` Get the total ΔV capability at beginning of life.
`String`	`getBusModel()` Get the bus model name.
`List<String>`	`getDockedWith()` Get the other space objects this object is docked to.
`double`	`getDragCoefficient()` Get the nominal drag coefficient.
`double`	`getDragConstantArea()` Get the attitude-independent drag cross-sectional area, not already into attitude-dependent area along OEB.
`double`	`getDragUncertainty()` Get the drag coefficient 1σ uncertainty.
`double`	`getDryMass()` Get the mass without propellant.
`RealMatrix`	`getInertiaMatrix()` Get the inertia matrix.
`double`	`getInitialWetMass()` Get the total mass at beginning of life.
`double`	`getManeuversFrequency()` Get the average frequency of orbit or attitude maneuvers (in SI units, hence per second).
`double`	`getManeuversPerYear()` Get the average number of orbit or attitude maneuvers per year.
`String`	`getManufacturer()` Get manufacturer name.
`double`	`getMaxAreaForCollisionProbability()` Get the maximum cross-sectional area for collision probability estimation purposes.
`double`	`getMaxRcs()` Get the maximum radar cross-section.
`double`	`getMaxThrust()` Get the maximum composite thrust the spacecraft can accomplish.
`double`	`getMinAreaForCollisionProbability()` Get the minimum cross-sectional area for collision probability estimation purposes.
`double`	`getMinRcs()` Get the minimum radar cross-section.
`double`	`getOebAreaAlongIntermediate()` Get the cross-sectional area of Optimally Enclosing Box along Y-OEB.
`double`	`getOebAreaAlongMax()` Get the cross-sectional area of Optimally Enclosing Box along X-OEB.
`double`	`getOebAreaAlongMin()` Get the cross-sectional area of Optimally Enclosing Box along Z-OEB.
`double`	`getOebIntermediate()` Get the dimensions of Optimally Enclosing Box along Y-OEB (i.e intermediate).
`double`	`getOebMax()` Get the dimensions of Optimally Enclosing Box along X-OEB (i.e max).
`double`	`getOebMin()` Get the dimensions of Optimally Enclosing Box along Z-OEB (i.e min).
`FrameFacade`	`getOebParentFrame()` Get the Optimally Enclosing Box parent reference frame.
`AbsoluteDate`	`getOebParentFrameEpoch()` Get the Optimally Enclosing Box parent reference frame epoch.
`Quaternion`	`getOebQ()` Get the quaternion defining Optimally Enclosing Box.
`double`	`getRcs()` Get the typical (50th percentile) radar cross-section.
`double`	`getReflectivity()` Get the typical (50th percentile) coefficient of reflectivity.
`double`	`getRemainingDv()` Get the total ΔV remaining for spacecraft.
`double`	`getSrpCoefficient()` Get the nominal SRP coefficient.
`double`	`getSrpConstantArea()` Get the attitude-independent SRP area, not already into attitude-dependent area along OEB.
`double`	`getSrpUncertainty()` Get the SRP coefficient 1σ uncertainty.
`double`	`getTypAreaForCollisionProbability()` Get the typical (50th percentile) cross-sectional area for collision probability estimation purposes.
`double`	`getVmAbsolute()` Get the typical (50th percentile) visual magnitude.
`double`	`getVmApparent()` Get the typical (50th percentile) apparent visual magnitude.
`double`	`getVmApparentMax()` Get the maximum apparent visual magnitude.
`double`	`getVmApparentMin()` Get the minimum apparent visual magnitude.
`double`	`getWetMass()` Get the total mass at T₀.
`void`	`setAttitudeActuatorType(String attitudeActuatorType)` Set the type of actuator for attitude control.
`void`	`setAttitudeControlAccuracy(double attitudeControlAccuracy)` Set the accuracy of attitude control.
`void`	`setAttitudeControlMode(String attitudeControlMode)` Set the attitude control mode.
`void`	`setAttitudeKnowledgeAccuracy(double attitudeKnowledgeAccuracy)` Set the accuracy of attitude knowledge.
`void`	`setAttitudePointingAccuracy(double attitudePointingAccuracy)` Set the overall accuracy of spacecraft to maintain attitude.
`void`	`setBolDv(double bolDv)` Set the total ΔV capability at beginning of life.
`void`	`setBusModel(String busModel)` Set the bus model name.
`void`	`setDockedWith(List<String> dockedWith)` Set the other space objects this object is docked to.
`void`	`setDragCoefficient(double dragCoefficient)` Set the the nominal drag coefficient.
`void`	`setDragConstantArea(double dragConstantArea)` Set the attitude-independent drag cross-sectional area, not already into attitude-dependent area along OEB.
`void`	`setDragUncertainty(double dragUncertainty)` Set the drag coefficient 1σ uncertainty.
`void`	`setDryMass(double dryMass)` Set the mass without propellant.
`void`	`setInertiaMatrixEntry(int j, int k, double entry)` Set an entry in the inertia matrix.
`void`	`setInitialWetMass(double initialWetMass)` Set the total mass at beginning of life.
`void`	`setManeuversFrequency(double maneuversFrequency)` Set the average frequency of orbit or attitude maneuvers (in SI units, hence per second).
`void`	`setManufacturer(String manufacturer)` Set manufacturer name.
`void`	`setMaxAreaForCollisionProbability(double maxAreaForCollisionProbability)` Set the maximum cross-sectional area for collision probability estimation purposes.
`void`	`setMaxRcs(double maxRcs)` Set the maximum radar cross-section.
`void`	`setMaxThrust(double maxThrust)` Set the maximum composite thrust the spacecraft can accomplish.
`void`	`setMinAreaForCollisionProbability(double minAreaForCollisionProbability)` Set the minimum cross-sectional area for collision probability estimation purposes.
`void`	`setMinRcs(double minRcs)` Set the minimum radar cross-section.
`void`	`setOebAreaAlongIntermediate(double oebAreaAlongIntermediate)` Set the cross-sectional area of Optimally Enclosing Box along Y-OEB.
`void`	`setOebAreaAlongMax(double oebAreaAlongMax)` Set the cross-sectional area of Optimally Enclosing Box along X-OEB.
`void`	`setOebAreaAlongMin(double oebAreaAlongMin)` Set the cross-sectional area of Optimally Enclosing Box along Z-OEB.
`void`	`setOebIntermediate(double oebIntermediate)` Set the dimensions of Optimally Enclosing Box along Y-OEB (i.e intermediate).
`void`	`setOebMax(double oebMax)` Set the dimensions of Optimally Enclosing Box along X-OEB (i.e max).
`void`	`setOebMin(double oebMin)` Set the dimensions of Optimally Enclosing Box along Z-OEB (i.e min).
`void`	`setOebParentFrame(FrameFacade oebParentFrame)` Set the Optimally Enclosing Box parent reference frame.
`void`	`setOebParentFrameEpoch(AbsoluteDate oebParentFrameEpoch)` Set the Optimally Enclosing Box parent reference frame epoch.
`void`	`setOebQ(int i, double qI)` set the component of quaternion defining Optimally Enclosing Box.
`void`	`setRcs(double rcs)` Set the typical (50th percentile) radar cross-section.
`void`	`setReflectivity(double reflectivity)` Set the typical (50th percentile) coefficient of reflectivity.
`void`	`setRemainingDv(double remainingDv)` Set the total ΔV remaining for spacecraft.
`void`	`setSrpCoefficient(double srpCoefficient)` Set the nominal SRP coefficient.
`void`	`setSrpConstantArea(double srpConstantArea)` Set the attitude-independent SRP area, not already into attitude-dependent area along OEB.
`void`	`setSrpUncertainty(double srpUncertainty)` Set the SRP coefficient 1σ uncertainty.
`void`	`setTypAreaForCollisionProbability(double typAreaForCollisionProbability)` Get the typical (50th percentile) cross-sectional area for collision probability estimation purposes.
`void`	`setVmAbsolute(double vmAbsolute)` Set the typical (50th percentile) visual magnitude.
`void`	`setVmApparent(double vmApparent)` Set the typical (50th percentile) apparent visual magnitude.
`void`	`setVmApparentMax(double vmApparentMax)` Set the maximum apparent visual magnitude.
`void`	`setVmApparentMin(double vmApparentMin)` Set the minimum apparent visual magnitude.
`void`	`setWetMass(double wetMass)` Set the total mass at T₀.

Methods inherited from class org.orekit.files.ccsds.section.CommentsContainer
acceptComments, addComment, checkAllowed, checkNotNaN, checkNotNegative, checkNotNull, getComments, refuseFurtherComments, validate

Methods inherited from class java.lang.Object
clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

- Method Detail
  - getManufacturer
```
public String getManufacturer()
```
    Get manufacturer name.
    
    Returns:
    
    manufacturer name
  - setManufacturer
```
public void setManufacturer(String manufacturer)
```
    Set manufacturer name.
    
    Parameters:
    
    manufacturer - manufacturer name
  - getBusModel
```
public String getBusModel()
```
    Get the bus model name.
    
    Returns:
    
    bus model name
  - setBusModel
```
public void setBusModel(String busModel)
```
    Set the bus model name.
    
    Parameters:
    
    busModel - bus model name
  - getDockedWith
```
public List<String> getDockedWith()
```
    Get the other space objects this object is docked to.
    
    Returns:
    
    the oother space objects this object is docked to
  - setDockedWith
```
public void setDockedWith(List<String> dockedWith)
```
    Set the other space objects this object is docked to.
    
    Parameters:
    
    dockedWith - the other space objects this object is docked to
  - getDragConstantArea
```
public double getDragConstantArea()
```
    Get the attitude-independent drag cross-sectional area, not already into attitude-dependent area along OEB.
    
    Returns:
    
    attitude-independent drag cross-sectional area, not already into attitude-dependent area along OEB
  - setDragConstantArea
```
public void setDragConstantArea(double dragConstantArea)
```
    Set the attitude-independent drag cross-sectional area, not already into attitude-dependent area along OEB.
    
    Parameters:
    
    dragConstantArea - attitude-independent drag cross-sectional area, not already into attitude-dependent area along OEB
  - getDragCoefficient
```
public double getDragCoefficient()
```
    Get the nominal drag coefficient.
    
    Returns:
    
    the nominal drag coefficient
  - setDragCoefficient
```
public void setDragCoefficient(double dragCoefficient)
```
    Set the the nominal drag coefficient.
    
    Parameters:
    
    dragCoefficient - the nominal drag coefficient
  - getDragUncertainty
```
public double getDragUncertainty()
```
    Get the drag coefficient 1σ uncertainty.
    
    Returns:
    
    drag coefficient 1σ uncertainty (in %)
  - setDragUncertainty
```
public void setDragUncertainty(double dragUncertainty)
```
    Set the drag coefficient 1σ uncertainty.
    
    Parameters:
    
    dragUncertainty - drag coefficient 1σ uncertainty (in %)
  - getInitialWetMass
```
public double getInitialWetMass()
```
    Get the total mass at beginning of life.
    
    Returns:
    
    total mass at beginning of life
  - setInitialWetMass
```
public void setInitialWetMass(double initialWetMass)
```
    Set the total mass at beginning of life.
    
    Parameters:
    
    initialWetMass - total mass at beginning of life
  - getWetMass
```
public double getWetMass()
```
    Get the total mass at T₀.
    
    Returns:
    
    total mass at T₀
  - setWetMass
```
public void setWetMass(double wetMass)
```
    Set the total mass at T₀.
    
    Parameters:
    
    wetMass - total mass at T₀
  - getDryMass
```
public double getDryMass()
```
    Get the mass without propellant.
    
    Returns:
    
    mass without propellant
  - setDryMass
```
public void setDryMass(double dryMass)
```
    Set the mass without propellant.
    
    Parameters:
    
    dryMass - mass without propellant
  - getOebParentFrame
```
public FrameFacade getOebParentFrame()
```
    Get the Optimally Enclosing Box parent reference frame.
    
    Returns:
    
    Optimally Enclosing Box parent reference frame
  - setOebParentFrame
```
public void setOebParentFrame(FrameFacade oebParentFrame)
```
    Set the Optimally Enclosing Box parent reference frame.
    
    Parameters:
    
    oebParentFrame - Optimally Enclosing Box parent reference frame
  - getOebParentFrameEpoch
```
public AbsoluteDate getOebParentFrameEpoch()
```
    Get the Optimally Enclosing Box parent reference frame epoch.
    
    Returns:
    
    Optimally Enclosing Box parent reference frame epoch
  - setOebParentFrameEpoch
```
public void setOebParentFrameEpoch(AbsoluteDate oebParentFrameEpoch)
```
    Set the Optimally Enclosing Box parent reference frame epoch.
    
    Parameters:
    
    oebParentFrameEpoch - Optimally Enclosing Box parent reference frame epoch
  - getOebQ
```
public Quaternion getOebQ()
```
    Get the quaternion defining Optimally Enclosing Box.
    
    Returns:
    
    quaternion defining Optimally Enclosing Box
  - setOebQ
```
public void setOebQ(int i,
                    double qI)
```
    set the component of quaternion defining Optimally Enclosing Box.
    
    Parameters:
    
    i - index of the component
    
    qI - component of quaternion defining Optimally Enclosing Box
  - getOebMax
```
public double getOebMax()
```
    Get the dimensions of Optimally Enclosing Box along X-OEB (i.e max).
    
    Returns:
    
    dimensions of Optimally Enclosing Box along X-OEB (i.e max)
  - setOebMax
```
public void setOebMax(double oebMax)
```
    Set the dimensions of Optimally Enclosing Box along X-OEB (i.e max).
    
    Parameters:
    
    oebMax - dimensions of Optimally Enclosing Box along X-OEB (i.e max)
  - getOebIntermediate
```
public double getOebIntermediate()
```
    Get the dimensions of Optimally Enclosing Box along Y-OEB (i.e intermediate).
    
    Returns:
    
    dimensions of Optimally Enclosing Box along Y-OEB (i.e intermediate).
  - setOebIntermediate
```
public void setOebIntermediate(double oebIntermediate)
```
    Set the dimensions of Optimally Enclosing Box along Y-OEB (i.e intermediate).
    
    Parameters:
    
    oebIntermediate - dimensions of Optimally Enclosing Box along Y-OEB (i.e intermediate).
  - getOebMin
```
public double getOebMin()
```
    Get the dimensions of Optimally Enclosing Box along Z-OEB (i.e min).
    
    Returns:
    
    dimensions of Optimally Enclosing Box along Z-OEB (i.e min)
  - setOebMin
```
public void setOebMin(double oebMin)
```
    Set the dimensions of Optimally Enclosing Box along Z-OEB (i.e min).
    
    Parameters:
    
    oebMin - dimensions of Optimally Enclosing Box along Z-OEB (i.e min)
  - getOebAreaAlongMax
```
public double getOebAreaAlongMax()
```
    Get the cross-sectional area of Optimally Enclosing Box along X-OEB.
    
    Returns:
    
    cross-sectional area of Optimally Enclosing Box along X-OEB
  - setOebAreaAlongMax
```
public void setOebAreaAlongMax(double oebAreaAlongMax)
```
    Set the cross-sectional area of Optimally Enclosing Box along X-OEB.
    
    Parameters:
    
    oebAreaAlongMax - cross-sectional area of Optimally Enclosing Box along X-OEB
  - getOebAreaAlongIntermediate
```
public double getOebAreaAlongIntermediate()
```
    Get the cross-sectional area of Optimally Enclosing Box along Y-OEB.
    
    Returns:
    
    cross-sectional area of Optimally Enclosing Box along Y-OEB
  - setOebAreaAlongIntermediate
```
public void setOebAreaAlongIntermediate(double oebAreaAlongIntermediate)
```
    Set the cross-sectional area of Optimally Enclosing Box along Y-OEB.
    
    Parameters:
    
    oebAreaAlongIntermediate - cross-sectional area of Optimally Enclosing Box along X-OEB
  - getOebAreaAlongMin
```
public double getOebAreaAlongMin()
```
    Get the cross-sectional area of Optimally Enclosing Box along Z-OEB.
    
    Returns:
    
    cross-sectional area of Optimally Enclosing Box along X-OEB
  - setOebAreaAlongMin
```
public void setOebAreaAlongMin(double oebAreaAlongMin)
```
    Set the cross-sectional area of Optimally Enclosing Box along Z-OEB.
    
    Parameters:
    
    oebAreaAlongMin - cross-sectional area of Optimally Enclosing Box along X-OEB
  - getMinAreaForCollisionProbability
```
public double getMinAreaForCollisionProbability()
```
    Get the minimum cross-sectional area for collision probability estimation purposes.
    
    Returns:
    
    minimum cross-sectional area for collision probability estimation purposes
  - setMinAreaForCollisionProbability
```
public void setMinAreaForCollisionProbability(double minAreaForCollisionProbability)
```
    Set the minimum cross-sectional area for collision probability estimation purposes.
    
    Parameters:
    
    minAreaForCollisionProbability - minimum cross-sectional area for collision probability estimation purposes
  - getMaxAreaForCollisionProbability
```
public double getMaxAreaForCollisionProbability()
```
    Get the maximum cross-sectional area for collision probability estimation purposes.
    
    Returns:
    
    maximum cross-sectional area for collision probability estimation purposes
  - setMaxAreaForCollisionProbability
```
public void setMaxAreaForCollisionProbability(double maxAreaForCollisionProbability)
```
    Set the maximum cross-sectional area for collision probability estimation purposes.
    
    Parameters:
    
    maxAreaForCollisionProbability - maximum cross-sectional area for collision probability estimation purposes
  - getTypAreaForCollisionProbability
```
public double getTypAreaForCollisionProbability()
```
    Get the typical (50th percentile) cross-sectional area for collision probability estimation purposes.
    
    Returns:
    
    typical (50th percentile) cross-sectional area for collision probability estimation purposes
  - setTypAreaForCollisionProbability
```
public void setTypAreaForCollisionProbability(double typAreaForCollisionProbability)
```
    Get the typical (50th percentile) cross-sectional area for collision probability estimation purposes.
    
    Parameters:
    
    typAreaForCollisionProbability - typical (50th percentile) cross-sectional area for collision probability estimation purposes
  - getRcs
```
public double getRcs()
```
    Get the typical (50th percentile) radar cross-section.
    
    Returns:
    
    typical (50th percentile) radar cross-section
  - setRcs
```
public void setRcs(double rcs)
```
    Set the typical (50th percentile) radar cross-section.
    
    Parameters:
    
    rcs - typical (50th percentile) radar cross-section
  - getMinRcs
```
public double getMinRcs()
```
    Get the minimum radar cross-section.
    
    Returns:
    
    minimum radar cross-section
  - setMinRcs
```
public void setMinRcs(double minRcs)
```
    Set the minimum radar cross-section.
    
    Parameters:
    
    minRcs - minimum radar cross-section
  - getMaxRcs
```
public double getMaxRcs()
```
    Get the maximum radar cross-section.
    
    Returns:
    
    maximum radar cross-section
  - setMaxRcs
```
public void setMaxRcs(double maxRcs)
```
    Set the maximum radar cross-section.
    
    Parameters:
    
    maxRcs - maximum radar cross-section
  - getSrpConstantArea
```
public double getSrpConstantArea()
```
    Get the attitude-independent SRP area, not already into attitude-dependent area along OEB.
    
    Returns:
    
    attitude-independent SRP area, not already into attitude-dependent area along OEB
  - setSrpConstantArea
```
public void setSrpConstantArea(double srpConstantArea)
```
    Set the attitude-independent SRP area, not already into attitude-dependent area along OEB.
    
    Parameters:
    
    srpConstantArea - attitude-independent SRP area, not already into attitude-dependent area along OEB
  - getSrpCoefficient
```
public double getSrpCoefficient()
```
    Get the nominal SRP coefficient.
    
    Returns:
    
    nominal SRP coefficient
  - setSrpCoefficient
```
public void setSrpCoefficient(double srpCoefficient)
```
    Set the nominal SRP coefficient.
    
    Parameters:
    
    srpCoefficient - nominal SRP coefficient
  - getSrpUncertainty
```
public double getSrpUncertainty()
```
    Get the SRP coefficient 1σ uncertainty.
    
    Returns:
    
    SRP coefficient 1σ uncertainty
  - setSrpUncertainty
```
public void setSrpUncertainty(double srpUncertainty)
```
    Set the SRP coefficient 1σ uncertainty.
    
    Parameters:
    
    srpUncertainty - SRP coefficient 1σ uncertainty.
  - getVmAbsolute
```
public double getVmAbsolute()
```
    Get the typical (50th percentile) visual magnitude.
    
    Returns:
    
    typical (50th percentile) visual magnitude
  - setVmAbsolute
```
public void setVmAbsolute(double vmAbsolute)
```
    Set the typical (50th percentile) visual magnitude.
    
    Parameters:
    
    vmAbsolute - typical (50th percentile) visual magnitude
  - getVmApparentMin
```
public double getVmApparentMin()
```
    Get the minimum apparent visual magnitude.
    
    Returns:
    
    minimum apparent visual magnitude
  - setVmApparentMin
```
public void setVmApparentMin(double vmApparentMin)
```
    Set the minimum apparent visual magnitude.
    
    Parameters:
    
    vmApparentMin - minimum apparent visual magnitude
  - getVmApparent
```
public double getVmApparent()
```
    Get the typical (50th percentile) apparent visual magnitude.
    
    Returns:
    
    typical (50th percentile) apparent visual magnitude
  - setVmApparent
```
public void setVmApparent(double vmApparent)
```
    Set the typical (50th percentile) apparent visual magnitude.
    
    Parameters:
    
    vmApparent - typical (50th percentile) apparent visual magnitude
  - getVmApparentMax
```
public double getVmApparentMax()
```
    Get the maximum apparent visual magnitude.
    
    Returns:
    
    maximum apparent visual magnitude
  - setVmApparentMax
```
public void setVmApparentMax(double vmApparentMax)
```
    Set the maximum apparent visual magnitude.
    
    Parameters:
    
    vmApparentMax - maximum apparent visual magnitude
  - getReflectivity
```
public double getReflectivity()
```
    Get the typical (50th percentile) coefficient of reflectivity.
    
    Returns:
    
    typical (50th percentile) coefficient of reflectivity
  - setReflectivity
```
public void setReflectivity(double reflectivity)
```
    Set the typical (50th percentile) coefficient of reflectivity.
    
    Parameters:
    
    reflectivity - typical (50th percentile) coefficient of reflectivity
  - getAttitudeControlMode
```
public String getAttitudeControlMode()
```
    Get the attitude control mode.
    
    Returns:
    
    attitude control mode
  - setAttitudeControlMode
```
public void setAttitudeControlMode(String attitudeControlMode)
```
    Set the attitude control mode.
    
    Parameters:
    
    attitudeControlMode - attitude control mode
  - getAttitudeActuatorType
```
public String getAttitudeActuatorType()
```
    Get the type of actuator for attitude control.
    
    Returns:
    
    type of actuator for attitude control
  - setAttitudeActuatorType
```
public void setAttitudeActuatorType(String attitudeActuatorType)
```
    Set the type of actuator for attitude control.
    
    Parameters:
    
    attitudeActuatorType - type of actuator for attitude control
  - getAttitudeKnowledgeAccuracy
```
public double getAttitudeKnowledgeAccuracy()
```
    Get the accuracy of attitude knowledge.
    
    Returns:
    
    accuracy of attitude knowledge
  - setAttitudeKnowledgeAccuracy
```
public void setAttitudeKnowledgeAccuracy(double attitudeKnowledgeAccuracy)
```
    Set the accuracy of attitude knowledge.
    
    Parameters:
    
    attitudeKnowledgeAccuracy - accuracy of attitude knowledge
  - getAttitudeControlAccuracy
```
public double getAttitudeControlAccuracy()
```
    Get the accuracy of attitude control.
    
    Returns:
    
    accuracy of attitude control
  - setAttitudeControlAccuracy
```
public void setAttitudeControlAccuracy(double attitudeControlAccuracy)
```
    Set the accuracy of attitude control.
    
    Parameters:
    
    attitudeControlAccuracy - accuracy of attitude control
  - getAttitudePointingAccuracy
```
public double getAttitudePointingAccuracy()
```
    Get the overall accuracy of spacecraft to maintain attitude.
    
    Returns:
    
    overall accuracy of spacecraft to maintain attitude
  - setAttitudePointingAccuracy
```
public void setAttitudePointingAccuracy(double attitudePointingAccuracy)
```
    Set the overall accuracy of spacecraft to maintain attitude.
    
    Parameters:
    
    attitudePointingAccuracy - overall accuracy of spacecraft to maintain attitude
  - getManeuversPerYear
```
public double getManeuversPerYear()
```
    Get the average number of orbit or attitude maneuvers per year.
    
    Returns:
    
    average number of orbit or attitude maneuvers per year.
  - getManeuversFrequency
```
public double getManeuversFrequency()
```
    Get the average frequency of orbit or attitude maneuvers (in SI units, hence per second).
    
    Returns:
    
    average frequency of orbit or attitude maneuvers (in SI units, hence per second).
  - setManeuversFrequency
```
public void setManeuversFrequency(double maneuversFrequency)
```
    Set the average frequency of orbit or attitude maneuvers (in SI units, hence per second).
    
    Parameters:
    
    maneuversFrequency - average frequency of orbit or attitude (in SI units, hence per second).
  - getMaxThrust
```
public double getMaxThrust()
```
    Get the maximum composite thrust the spacecraft can accomplish.
    
    Returns:
    
    maximum composite thrust the spacecraft can accomplish
  - setMaxThrust
```
public void setMaxThrust(double maxThrust)
```
    Set the maximum composite thrust the spacecraft can accomplish.
    
    Parameters:
    
    maxThrust - maximum composite thrust the spacecraft can accomplish
  - getBolDv
```
public double getBolDv()
```
    Get the total ΔV capability at beginning of life.
    
    Returns:
    
    total ΔV capability at beginning of life
  - setBolDv
```
public void setBolDv(double bolDv)
```
    Set the total ΔV capability at beginning of life.
    
    Parameters:
    
    bolDv - total ΔV capability at beginning of life
  - getRemainingDv
```
public double getRemainingDv()
```
    Get the total ΔV remaining for spacecraft.
    
    Returns:
    
    total ΔV remaining for spacecraft
  - setRemainingDv
```
public void setRemainingDv(double remainingDv)
```
    Set the total ΔV remaining for spacecraft.
    
    Parameters:
    
    remainingDv - total ΔV remaining for spacecraft
  - getInertiaMatrix
```
public RealMatrix getInertiaMatrix()
```
    Get the inertia matrix.
    
    Returns:
    
    the inertia matrix
  - setInertiaMatrixEntry
```
public void setInertiaMatrixEntry(int j,
                                  int k,
                                  double entry)
```
    Set an entry in the inertia matrix.
    Both I(j, k) and I(k, j) are set.
    
    Parameters:
    
    j - row index (must be between 0 and 3 (inclusive)
    
    k - column index (must be between 0 and 3 (inclusive)
    
    entry - value of the matrix entry

Class PhysicalProperties

Method Summary

Methods inherited from class org.orekit.files.ccsds.section.CommentsContainer

Methods inherited from class java.lang.Object

Method Detail

getManufacturer

setManufacturer

getBusModel

setBusModel

getDockedWith

setDockedWith

getDragConstantArea

setDragConstantArea

getDragCoefficient

setDragCoefficient

getDragUncertainty

setDragUncertainty

getInitialWetMass

setInitialWetMass

getWetMass

setWetMass

getDryMass

setDryMass

getOebParentFrame

setOebParentFrame

getOebParentFrameEpoch

setOebParentFrameEpoch

getOebQ

setOebQ

getOebMax

setOebMax

getOebIntermediate

setOebIntermediate

getOebMin

setOebMin

getOebAreaAlongMax

setOebAreaAlongMax

getOebAreaAlongIntermediate

setOebAreaAlongIntermediate

getOebAreaAlongMin

setOebAreaAlongMin

getMinAreaForCollisionProbability

setMinAreaForCollisionProbability

getMaxAreaForCollisionProbability

setMaxAreaForCollisionProbability

getTypAreaForCollisionProbability

setTypAreaForCollisionProbability

getRcs

setRcs

getMinRcs

setMinRcs

getMaxRcs

setMaxRcs

getSrpConstantArea

setSrpConstantArea

getSrpCoefficient

setSrpCoefficient

getSrpUncertainty

setSrpUncertainty

getVmAbsolute

setVmAbsolute

getVmApparentMin

setVmApparentMin

getVmApparent

setVmApparent

getVmApparentMax

setVmApparentMax

getReflectivity

setReflectivity

getAttitudeControlMode

setAttitudeControlMode

getAttitudeActuatorType

setAttitudeActuatorType

getAttitudeKnowledgeAccuracy

setAttitudeKnowledgeAccuracy

getAttitudeControlAccuracy

setAttitudeControlAccuracy

getAttitudePointingAccuracy

setAttitudePointingAccuracy

getManeuversPerYear