Path: Common/Control
% Computes state space matrices from a nonlinear function. This function computes state space matrices from f(x,t,u,varargin). The RHS must be of the form f(x,t,u,varargin). -------------------------------------------------------------------------- Form: [a, b] = SSFromNonlinear( f, x, t, u, k, varargin ) -------------------------------------------------------------------------- ------ Inputs ------ f (1,:) Dynamical function name x (n,1) Nominal state t (1,1) Time u (m,1) Nominal control kUse (1,:) States to use varargin Arguments passed to f ------- Outputs ------- a (n,n) State matrix b (n,m) Input matrix --------------------------------------------------------------------------
ACPro: ACPointMass/AircraftPointMassRHSWithSideslip ACPro: ACProAerodynamics/AeroCoefficientPointMass ACPro: ACProAerodynamics/DragPolar ACPro: ACProAerodynamics/GroundEffect AerospaceUtils: AtmosphericCalculations/AtmDens2 Common: CommonData/SwooshWatermark Common: DemoFuns/DoubleIntegratorRHS Common: DemoFuns/OscillatorRHS Common: General/CellToMat Common: General/DeBlankLT Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/TitleS Common: Graphics/XLabelS Common: Graphics/YLabelS Math: Analysis/Logistic Math: Linear/Mag
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