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MATLAB simulation of fixed-mass rigid-body 6DOF 1.0
File ID: 79344






MATLAB simulation of fixed-mass rigid-body 6DOF 1.0
Download MATLAB simulation of fixed-mass rigid-body 6DOF 1.0http://www.mathworks.comReport Error Link
License: Freeware
File Size: 10.0 KB
Downloads: 63
User Rating:1 Stars  (1 rating)
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MATLAB simulation of fixed-mass rigid-body 6DOF 1.0 Description
Description: 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

License: Freeware

Related: forces, velocity, Time, Simulation, inputs, outputs, inertia, vectory, Vector, Position, fixed, matlab ode, time series vector, aircraft inertia, tensor matrix tarray, vector optional inputs, velocity body irates, Body, 3d 3x3, 3d 3x1

O/S:BSD, Linux, Solaris, Mac OS X

File Size: 10.0 KB

Downloads: 63



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