Path: FormationFlying/Utility
% Compute a 3xN acceleration vector from a "maneuver" data structure. A constant timestep is used. Since version 7. -------------------------------------------------------------------------- Usage: [aC,t] = ManeuverStruct2AccelVector( mvr, dT ); [aC] = ManeuverStruct2AccelVector( mvr, t ); -------------------------------------------------------------------------- ------ Inputs ------ mvr (.) Maneuver data structure dT (1) or (N) Time-step or time vector [sec] ------- Outputs ------- aC (3,N) [x;y;z] acceleration over N time intervals [km/sec^2] t (1,N) Time vector [sec] --------------------------------------------------------------------------
Math: Linear/Mag Math: Linear/Unit
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