User’s Guide to Running the Trajectory Code Using AAE450 ...

This is an ordinary differential equation solver; the state variables 1 through 6 are for the time history of the position and the velocity in the spherical coordinating system, and the state variables 7 and 8 are the ΔV’s due to the drag and the propulsion respectively. ... function xdot=AAE450_Trajectory_ODE_AC_linear(t,x,T_full,m0,m_dot,a ... ................
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