TimeUntilTheta:

Path: FormationFlying/Utility

% Computes the time in seconds until the latitude "theta2" is reached from the 
   original latitude, "theta1".

   Since version 7.
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   ------
   Inputs
   ------
   a              (1)  Semimajor axis                   [km]
   w              (1)  Argument of perigee              [rad]
   e              (1)  Eccentricity
   theta0         (1)  Initial argument of latitude     [rad]
   theta1         (1)  Final argument of latitude       [rad]
   mu             (1)  Gravitational constant           [km^3/sec^2] (optional)

   -------
   Outputs
   -------
   dT             (1)  Time until next theta is reached [sec]
   
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Children:

AC: ACData/ACTConstants
SC: BasicOrbit/E2M
SC: BasicOrbit/Nu2E
SC: BasicOrbit/Nu2M
SC: SCData/sCTConstants
Common: CommonData/Constants
Common: CommonData/SwooshWatermark
Common: CommonData/xSplashSmall
Common: Database/Constant
Common: General/CellToMat
Common: General/DeleteCell
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle
Math: Linear/DupVect
Math: Trigonometry/WrapPhase

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