TrnsfOrb

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   Simulates transfer orbit
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   Form:
   TrnsfOrb( event, mET, a, eventName, dateStart, database )
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   Inputs
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   event           (:,:) Event to be simulated
   mET             (1,1) Mission elapsed time [h,m,s]
   a               (1,:) Event data
   eventName       (1,:) Name of event
   dateStart       (1,6) [year month day hour minute second]
   database        (1,:) Database name
   inertiaName     (1,:) Name of the starting inertia
   units           (2,3) ['mks'|'lbf'|'sft';'deg'|'rad';'rpm'|'rps']

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