E2M:

Path: SC/BasicOrbit

% Converts eccentric anomaly to mean anomaly.

--------------------------------------------------------------------------
   Form:
   meanAnom = E2M( ecc, eccAnom )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   ecc       (1,:) Eccentricity
   eccAnom   (1,:) Eccentric anomaly

   -------
   Outputs
   -------
   meanAnom  (1,:) Mean anomaly

--------------------------------------------------------------------------
   References:	Bate, R. R. Fundamentals of Astrodynamics. pp. 185-187.
--------------------------------------------------------------------------

Children:

Common: CommonData/SwooshWatermark
Common: General/CellToMat
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle
Math: Linear/DupVect

Back to the SC Module page