Path: Missions/Comsat
% Simulates transfer orbit -------------------------------------------------------------------------- Form: TransferOrbit( event, mET, a, eventName, dateStart, database ) -------------------------------------------------------------------------- ------ Inputs ------ 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'] --------------------------------------------------------------------------