Publisher review:MATLAB Simulation of variable-mass rigid-body 6DOF - Calculate aircraft variable-mass rigid-body six-degrees-of-freedom equations of motion using MATLAB SIXDOFVM Calculate aircraft variable-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 coordinatesdMass = mass rate of change for the aircraftdInertia = 3x3 Inertia Tensor matrix rate of changetarray = time series vectorOPTIONAL INPUTS:Ipos_i = 3x1 vector of initial positionIvel_b = 3x1 vector of initial velocity (body)Irates_b = 3x1 vector of initial body ratesImass = initial mass of aircraftIInertia = initial 3x3 Inertia Tensor matrixIeuler = 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 Requirements: ยท MATLAB Release: R13
MATLAB Simulation of variable-mass rigid-body 6DOF is a Matlab script for Astronomy/Aerospace scripts design by Stacey Gage.
It runs on following operating system: Windows / Linux / Mac OS / BSD / Solaris.
Operating system:Windows / Linux / Mac OS / BSD / Solaris
MATLAB Simulation of variable-mass rigid-body 6DOF script details 
