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MATLAB simulation of fixed-mass rigid-body 6DOF

Calculate aircraft fixed-mass rigid-body six-degrees-of-freedom equations

Last Week downloads: 2
Total downloads: 666
Matlab
  • Last Updated: Jun 24, 2010
  • License: BSD Free
  • OS: Windows /Linux/Mac OS/BSD/Solaris
  • Requirements: No special requirements
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For MATLAB simulation of fixed-mass rigid-body 6DOF Publisher's description

BSEditor: % SIXDOF Calculate aircraft fixed-mass rigid-body six-degrees-of-Freedom
% equations of motion using MATLAB ODE45 solver.
%
% =-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=
% Inputs:
% =-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=
% Forces = 3x1 vector of forces in body coordinates
% Moments = 3x1 vectory of moments in body coordinates
% Mass = fixed mass of the aircraft
% Inertia = 3x3 Inertia Tensor Matrix
% tarray = time series vector
%
% OPTIONAL INPUTS:
% Ipos_i = 3x1 vector of initial position
% Ivel_b = 3x1 vector of initial velocity (body)
% Irates_b = 3x1 vector of initial body rates
% Ieuler = 3x1 vector of initial euler angles
%
% =-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=
% Outputs:
% =-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=
% t = simulation time
% y(1:3) = body rates
% y(4:6) = velocity in body coordinates
% y(7:9) = position in body coordinates
%
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