class VDator
extends java.lang.Object
Copyright (c) 2018
Constructor and Description |
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VDator() |
Modifier and Type | Method and Description |
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protected static double |
getArgOfPeri()
Gets the argument of perigee.
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protected static double |
getAxisLength()
Gets the length of the orbital semi-major axis.
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protected static double |
getEccentricity()
Gets the orbital eccentricity.
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protected static double |
getInclination()
Gets the orbital inclination.
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protected static double |
getMeanAnomaly()
Gets the orbital mean anomaly.
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protected static jll.celcalc.ASTUtils.ASTVect |
getPosVect()
Gets the state vector's positional vector.
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protected static double |
getRAAN()
Gets the right ascension of the ascending node.
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protected static jll.celcalc.ASTUtils.ASTVect |
getVelVect()
Gets the state vector's velocity vector.
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protected static boolean |
validateKeplerianElements()
Display a form to get Keplerian elements and validate the
data values the user enters
User will enter inclination, eccentricity, axis,
RAAN, argument of perigee, and M0.
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static boolean |
validateStateVect()
Display a form to get a state vector and validate the
data values the user enters.
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protected static boolean validateKeplerianElements()
protected static double getInclination()
protected static double getEccentricity()
protected static double getAxisLength()
protected static double getRAAN()
protected static double getArgOfPeri()
protected static double getMeanAnomaly()
public static boolean validateStateVect()
protected static jll.celcalc.ASTUtils.ASTVect getPosVect()
protected static jll.celcalc.ASTUtils.ASTVect getVelVect()