## MATLAB simulation of fixed-mass rigid-body 6DOF

version 1.1.0.1 (2.08 KB) by
Calculate aircraft fixed-mass rigid-body six-degrees-of-freedom equations of motion using MATLAB ODE

Updated 01 Sep 2016

% SIXDOF Calculate aircraft fixed-mass rigid-body six-degrees-of-freedom
% equations of motion using MATLAB ODE45 solver.
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% Inputs:
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% 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
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% Outputs:
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% 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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### Cite As

Stacey Gage (2022). MATLAB simulation of fixed-mass rigid-body 6DOF (https://www.mathworks.com/matlabcentral/fileexchange/3367-matlab-simulation-of-fixed-mass-rigid-body-6dof), MATLAB Central File Exchange. Retrieved .

##### MATLAB Release Compatibility
Created with R13
Compatible with any release
##### Platform Compatibility
Windows macOS Linux