Publisher review:MATLAB simulation of fixed-mass rigid-body 6DOF - Calculate aircraft fixed-mass rigid-body six-degrees-of-freedom equations of motion using MATLAB ODE 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 coordinatesMoments = 3x1 vectory of moments in body coordinatesMass = fixed mass of the aircraftInertia = 3x3 Inertia Tensor matrixtarray = time series vector
OPTIONAL INPUTS:Ipos_i = 3x1 vector of initial positionIvel_b = 3x1 vector of initial velocity (body)Irates_b = 3x1 vector of initial body ratesIeuler = 3x1 vector of initial euler anglesOutputs:t = simulation timey(1:3) = body ratesy(4:6) = velocity in body coordinatesy(7:9) = position in body coordinates
MATLAB simulation of fixed-mass rigid-body 6DOF is a Matlab script for Astronomy/Aerospace scripts design by Stacey Gage.
It runs on following operating system: Windows / Linux / BSD / Solaris.
Operating system:Windows / Linux / BSD / Solaris