Package org.orekit.files.ccsds.ndm.cdm

Class AdditionalParameters

  • All Implemented Interfaces:
    Section
    public class AdditionalParameters
extends CommonPhysicalProperties
    Container for additional parameters data block.
    Since:
    11.2
    Author:
    Melina Vanel

    • Constructor Detail

      • AdditionalParameters

        public AdditionalParameters()
        Simple constructor.

    • Method Detail

      • validate

        public void validate​(double version)
        Check is all mandatory entries have been initialized.

        This method should throw an exception if some mandatory entries are missing or not compatible with version number.

        Specified by:
        validate in interface Section
        Overrides:
        validate in class CommonPhysicalProperties
        Parameters:
        version - format version

      • getAreaPC

        public double getAreaPC()
        Get the actual area of the object.
        Returns:
        the object area (in m²)

      • setAreaPC

        public void setAreaPC​(double areaPC)
        Set the actual area of the object.
        Parameters:
        areaPC - area (in m²) value to be set

      • getAreaDRG

        public double getAreaDRG()
        Get the effective area of the object exposed to atmospheric drag.
        Returns:
        the object area (in m²) exposed to atmospheric drag

      • setAreaDRG

        public void setAreaDRG​(double areaDRG)
        Set the effective area of the object exposed to atmospheric drag.
        Parameters:
        areaDRG - area (in m²) value to be set

      • getAreaSRP

        public double getAreaSRP()
        Get the effective area of the object exposed to solar radiation pressure.
        Returns:
        the object area (in m²) exposed to solar radiation pressure

      • setAreaSRP

        public void setAreaSRP​(double areaSRP)
        Set the effective area of the object exposed to solar radiation pressure.
        Parameters:
        areaSRP - area (in m²) to be set

      • getMass

        public double getMass()
        Get the mass of the object.
        Returns:
        the mass (in kg) of the object

      • setMass

        public void setMass​(double mass)
        Set the mass of the object.
        Parameters:
        mass - mass (in kg) of the object to be set

      • getCDAreaOverMass

        public double getCDAreaOverMass()
        Get the object’s Cd x A/m used to propagate the state vector and covariance to TCA.
        Returns:
        the object’s Cd x A/m (in m²/kg)

      • setCDAreaOverMass

        public void setCDAreaOverMass​(double CDAreaOverMass)
        Set the object’s Cd x A/m used to propagate the state vector and covariance to TCA.
        Parameters:
        CDAreaOverMass - object’s Cd x A/m (in m²/kg) value to be set

      • getCRAreaOverMass

        public double getCRAreaOverMass()
        Get the object’s Cr x A/m used to propagate the state vector and covariance to TCA.
        Returns:
        the object’s Cr x A/m (in m²/kg)

      • setCRAreaOverMass

        public void setCRAreaOverMass​(double CRAreaOverMass)
        Set the object’s Cr x A/m used to propagate the state vector and covariance to TCA.
        Parameters:
        CRAreaOverMass - object’s Cr x A/m (in m²/kg) value to be set

      • getThrustAcceleration

        public double getThrustAcceleration()
        Get the object’s acceleration due to in-track thrust used to propagate the state vector and covariance to TCA.
        Returns:
        the object’s acceleration (in m/s²) due to in-track thrust

      • setThrustAcceleration

        public void setThrustAcceleration​(double thrustAcceleration)
        Set the object’s acceleration due to in-track thrust used to propagate the state vector and covariance to TCA.
        Parameters:
        thrustAcceleration - object’s acceleration (in m/s²) due to in-track thrust

      • getSedr

        public double getSedr()
        Get the amount of energy being removed from the object’s orbit by atmospheric drag. This value is an average calculated during the OD. SEDR = Specific Energy Dissipation Rate.
        Returns:
        the amount of energy (in W/kg) being removed from the object’s orbit by atmospheric drag

      • setSedr

        public void setSedr​(double SEDR)
        Set the amount of energy being removed from the object’s orbit by atmospheric drag. This value is an average calculated during the OD. SEDR = Specific Energy Dissipation Rate.
        Parameters:
        SEDR - amount of energy (in W/kg) being removed from the object’s orbit by atmospheric drag

      • getAreaPCMin

        public double getAreaPCMin()
        Set the minimum area of the object to be used to compute the collision probability.
        Returns:
        the areaPCMin

      • setAreaPCMin

        public void setAreaPCMin​(double areaPCMin)
        Get the minimum area of the object to be used to compute the collision probability.
        Parameters:
        areaPCMin - the areaPCMin to set

      • getAreaPCMax

        public double getAreaPCMax()
        Get the maximum area of the object to be used to compute the collision probability.
        Returns:
        the areaPCMax

      • setAreaPCMax

        public void setAreaPCMax​(double areaPCMax)
        Set the maximum area for the object to be used to compute the collision probability.
        Parameters:
        areaPCMax - the areaPCMax to set

      • getHbr

        public double getHbr()
        Get the object hard body radius.
        Returns:
        the object hard body radius.

      • setHbr

        public void setHbr​(double hbr)
        Set the object hard body radius.
        Parameters:
        hbr - the object hard body radius.

      • getApoapsisAltitude

        public double getApoapsisAltitude()
        Get the distance of the furthest point in the objects orbit above the equatorial radius of the central body.
        Returns:
        the apoapsisAltitude

      • setApoapsisAltitude

        public void setApoapsisAltitude​(double apoapsisAltitude)
        Set the distance of the furthest point in the objects orbit above the equatorial radius of the central body.
        Parameters:
        apoapsisAltitude - the apoapsisHeight to set

      • getPeriapsisAltitude

        public double getPeriapsisAltitude()
        Get the distance of the closest point in the objects orbit above the equatorial radius of the central body.
        Returns:
        the periapsissAltitude

      • setPeriapsisAltitude

        public void setPeriapsisAltitude​(double periapsisAltitude)
        Set the distance of the closest point in the objects orbit above the equatorial radius of the central body.
        Parameters:
        periapsisAltitude - the periapsissHeight to set

      • getInclination

        public double getInclination()
        Get the angle between the objects orbit plane and the orbit centers equatorial plane.
        Returns:
        the inclination

      • setInclination

        public void setInclination​(double inclination)
        Set the angle between the objects orbit plane and the orbit centers equatorial plane.
        Parameters:
        inclination - the inclination to set

      • getCovConfidence

        public double getCovConfidence()
        Get the measure of the confidence in the covariance errors matching reality.
        Returns:
        the covConfidence

      • setCovConfidence

        public void setCovConfidence​(double covConfidence)
        Set the measure of the confidence in the covariance errors matching reality.
        Parameters:
        covConfidence - the covConfidence to set

      • getCovConfidenceMethod

        public String getCovConfidenceMethod()
        Get the method used for the calculation of COV_CONFIDENCE.
        Returns:
        the covConfidenceMethod

      • setCovConfidenceMethod

        public void setCovConfidenceMethod​(String covConfidenceMethod)
        Set the method used for the calculation of COV_CONFIDENCE.
        Parameters:
        covConfidenceMethod - the covConfidenceMethod to set