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MATLAB simulation of fixed-mass rigid-body 6DOF

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

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Last Week downloads: 0
Total downloads: 784
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

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MATLAB simulation of fixed-mass rigid-body 6DOF is a Scripts software developed by Stacey Gage. After our trial and test, the software is proved to be official, secure and free. Here is the official description for MATLAB simulation of fixed-mass rigid-body 6DOF:

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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