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

バージョン 1.1.0.1 (2.08 KB) 作成者:
Calculate aircraft fixed-mass rigid-body six-degrees-of-freedom equations of motion using MATLAB ODE

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% 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
%

### 引用

Stacey Gage (2023). 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. 取得済み .

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1.1.0.1