# MATLAB simulation of fixed-mass rigid-body 6DOF (Scripts) 1.0

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• Last update: 6 years ago
• Price: Free |
• Operating system: Linux, Mac OS X, Win All, BSD, Solaris
• Publisher: Stacey Gage (6 other programs)
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## MATLAB simulation of fixed-mass rigid-body 6DOF (Scripts) Publisher's description

### SIXDOF Calculate aircraft fixed-mass rigid-body six-degrees-of-freedom

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

#### System Requirements:

MATLAB 6.5 (R13)
Program Release Status: Major Update
Program Install Support: Install and Uninstall

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