Path: AC/Aircraft
% Compute the state space system based on aerodynamic derivatives. See DC8.m for an example of the database format. The state vector is either: 'wind': [vT; alpha; beta; p; q; r; phi; theta; psi] or 'stability': [u; v; w; p; q; r; phi; theta; psi] -------------------------------------------------------------------------- Form: [g, gLat, gLon] = AeroD( f, axisSystem ) -------------------------------------------------------------------------- ------ Inputs ------ f Aircraft data or database for input axisSystem 'wind', 'stability' ------- Outputs ------- g State space system of type statespace gLat Lateral dynamics gLon Longitudinal dynamics --------------------------------------------------------------------------
Common: Classes/@statespace/and.m Common: Classes/@statespace/close.m Common: Classes/@statespace/connect.m Common: Classes/@statespace/eig.m Common: Classes/@statespace/get.m Common: Classes/@statespace/getabcd.m Common: Classes/@statespace/getsub.m Common: Classes/@statespace/isempty.m Common: Classes/@statespace/mtimes.m Common: Classes/@statespace/plus.m Common: Classes/@statespace/series.m Common: Classes/@statespace/set.m Common: Classes/@statespace/statespace.m Common: CommonData/SwooshWatermark Common: Control/Append Common: Control/C2DZOH Common: Control/EigEval Common: Control/Parallel Common: Control/S2Damp Common: Control/SVPlot Common: Control/Series Common: Control/SizeABCD Common: Control/Step Common: Control/TrnsZero Common: Control/WPZ Common: Control/WReson Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/LogLimit Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/TimeLabl Math: Linear/ColCompR Math: Linear/IsZero Math: Linear/RowCompU
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