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

All Implemented Interfaces:

Section
```
public class OrbitPhysicalProperties
extends CommonPhysicalProperties
```
Spacecraft physical properties.

Since:

11.0

Author:

Luc Maisonobe

Constructor Summary

Constructors
Constructor Description

OrbitPhysicalProperties(AbsoluteDate epochT0)
Simple constructor.

Method Summary

All Methods Instance Methods Concrete Methods
Modifier and Type	Method	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`	`getMaxThrust()`	Get the maximum composite thrust the spacecraft can accomplish.
`double`	`getMinAreaForCollisionProbability()`	Get the minimum cross-sectional area for collision probability estimation purposes.
`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`	`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`	`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`	`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`	`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, setComments

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

- Constructor Detail
  - OrbitPhysicalProperties
```
public OrbitPhysicalProperties(AbsoluteDate epochT0)
```
    Simple constructor.
    
    Parameters:
    
    epochT0 - T0 epoch from file metadata
- 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
  - 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
  - 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.
  - 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 OrbitPhysicalProperties

Constructor Summary

Method Summary

Methods inherited from class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

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

Methods inherited from class java.lang.Object

Constructor Detail

OrbitPhysicalProperties

Method Detail

getManufacturer

setManufacturer

getBusModel

setBusModel

getDockedWith

setDockedWith

getDragConstantArea

setDragConstantArea

getDragCoefficient

setDragCoefficient

getDragUncertainty

setDragUncertainty

getInitialWetMass

setInitialWetMass

getWetMass

setWetMass

getDryMass

setDryMass

getMinAreaForCollisionProbability

setMinAreaForCollisionProbability

getMaxAreaForCollisionProbability

setMaxAreaForCollisionProbability

getTypAreaForCollisionProbability

setTypAreaForCollisionProbability

getSrpConstantArea

setSrpConstantArea

getSrpCoefficient

setSrpCoefficient

getSrpUncertainty

setSrpUncertainty

getAttitudeControlMode

setAttitudeControlMode

getAttitudeActuatorType

setAttitudeActuatorType

getAttitudeKnowledgeAccuracy

setAttitudeKnowledgeAccuracy

getAttitudeControlAccuracy

setAttitudeControlAccuracy

getAttitudePointingAccuracy

setAttitudePointingAccuracy

getManeuversPerYear

getManeuversFrequency

setManeuversFrequency

getMaxThrust

setMaxThrust

getBolDv

setBolDv

getRemainingDv

setRemainingDv

getInertiaMatrix

setInertiaMatrixEntry