DefaultACState:

Path: AC/ACDemoFuns

% Provide a default aircraft state. 
--------------------------------------------------------------------------
   Form:
   x = DefaultACState;
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   None 

   -------
   Outputs
   -------
   x               Aircraft state vector, consisting of:
                    - r       (3,1) ECI position vector
                    - q       (4,1) Quaternion from ECI to body
                    - w       (3,1) Inertial body rate in body frame
                    - v       (3,1) Velocity of cm wrt air
                    - wR      (:,1) Angular velocity of rotors
                    - mass    (1,1) Mass
                    - inertia (6,1) Inertia
                    - cG      (3,1) Center of mass
                    - engine  (:,1) Engine states
                    - actuator(:,1) Actuator states
                    - sensor  (:,1) Sensor states
                    - flex    (:,1) Flex model states
                    - disturb (:,1) Disturbance model states

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Children:

AC: ACCoord/ECIToNED
AC: ACCoord/VTToVB
AC: Classes/@acstate/abs.m
AC: Classes/@acstate/acstate.m
AC: Classes/@acstate/get.m
AC: Classes/@acstate/length.m
AC: Classes/@acstate/minus.m
AC: Classes/@acstate/mrdivide.m
AC: Classes/@acstate/mtimes.m
AC: Classes/@acstate/plus.m
AC: Classes/@acstate/subsasgn.m
AC: Classes/@acstate/subsref.m
AC: Classes/@acstate/zeros.m
Common: Quaternion/Mat2Q
Common: Quaternion/QMult
Common: Transform/Eul2Q

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