GenerateAirshipAeroMats:

Path: Airships/Analysis

% Compute the aerodynamic force and torque for an airship 
 For a range of  flight conditions. Results stored in mat-file for later
 analysis.

 The force and torque due to buoyancy is included. No controls are applied
 (zero throttle, zero deflections)
--------------------------------------------------------------------------
   Form:
   data = GenerateAirshipAeroMats( name, xo, h, theta, alpha, V );
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   name        (:)       Airship model name
   xo          (1)       x-Location of body-frame origin   [m] (from nose)
   h           (1)       Altitude                          [m]
   theta       (1)       Flight path angle                 [rad]
   alpha      (1,M)      Range of Angle of attack values   [rad]
   V          (1,N)      Range of Velocity values          [m/s]

   -------
   Outputs
   -------
   data        (.)       Data structure with:
                          - name
                          - xo:       x-location of origin
                          - h:        altitude
                          - theta:    flight path angle
                          - alpha:    angle of attack         (1xM vector)
                          - V:        velocity                (1xN vector)
                          - Fx:       force in x-direction    (MxN matrix)
                          - Fz:       force in z-direction    (MxN matrix)
                          - My:       moment about y-axis     (MxN matrix)

--------------------------------------------------------------------------

Children:

AC: ACCoord/ECIToNED
AC: ACCoord/QECI
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
AerospaceUtils: AeroData/AtmData
Airships: Mass/AirshipMassModel
Airships: Mass/BuildAirshipMassModel
Airships: Mass/IntegrateMassProps
Airships: Modeling/AddedMass
Airships: Modeling/AirshipCV
Airships: Modeling/AirshipCoefficients
Airships: Modeling/AirshipGeometry
Airships: Modeling/AirshipInertiaFactors
Airships: Modeling/AirshipIntegrals
Airships: Modeling/BuildAirshipModel
Airships: Modeling/FinFactors
Airships: Modeling/FinGeometry
Airships: Modeling/GondolaGeometry
Airships: Modeling/HalfEllipsoid
Airships: Simulation/AirshipAero
Common: Atmosphere/StdAtm
Common: CommonData/SwooshWatermark
Common: General/CellToMat
Common: General/DeleteSuffix
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle
Common: Quaternion/Mat2Q
Common: Quaternion/QForm
Common: Quaternion/QMult
Common: Transform/Eul2Q
Common: Transform/IConvP
Math: Linear/Cross
Math: Linear/SkewSq
Math: Linear/Unit

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