AirshipTrimAnalysis:

Path: Airships/Analysis

% Compute the trim controls for an airship at a range of flight conditions
--------------------------------------------------------------------------
   Form:
   data = AirshipTrimAnalysis( data )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   data    (.)   Data structure generated by the function,
                 "GenerateAirshipAeroMats", with fields:
                  .name
                  .xo:       x-location of origin                   [m]
                  .h:        altitude                               [m]
                  .theta:    flight path angle                      [rad]
                  .alpha:    angle of attack         (1xM vector)   [rad]
                  .V:        velocity                (1xN vector)   [m/s]
                  .Fx:       force in x-direction    (MxN matrix)   [N]
                  .Fz:       force in z-direction    (MxN matrix)   [N]
                  .My:       moment about y-axis     (MxN matrix)   [Nm]

   -------
   Outputs
   -------
   data    (.)   New data structure. Copy of input with additional fields:
                  .T:        Trim thrust value        (MxN matrix)  [N]
                  .mu:       Trim thrust pitch angle  (MxN matrix)  [rad]
                  .dELV:     Trim elevator deflection (MxN matrix)  [rad]

--------------------------------------------------------------------------
   See also GenerateAirshipAeroMats, BuildAirshipModel
--------------------------------------------------------------------------

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: Analysis/GenerateAirshipAeroMats
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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