AircraftGroupMass:

Path: ACPro/ACPerformance

% Create masses for an aircraft.

   You pass in the subsystem name and the aircraft mass. As shown in the
   demo, you need to iterate on the function as you build up the aircraft
   mass. Type AircraftGroupMass for a demo which just calls
   AircraftGroupMassStatement.

   Since version 4 (ACT).
--------------------------------------------------------------------------
   Form:
   m = AircraftGroupMass( group, MTOM, p )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   group     (1,:) Group name
   MTOM      (1,1) Takeoff mass (kg)
   p         (1,1) Data structure for the aircraft

   -------
   Outputs
   -------
   m        (1,1) Mass (kg)

--------------------------------------------------------------------------
   References:	Kundu, A., J. "Aircraft Design", Cambridge.
--------------------------------------------------------------------------

Children:

ACPro: ACDesign/AircraftGroupMassStatement

Back to the ACPro Module page