Write Wolfram Mathematica code

Add the navigation equations and the altitude equation to the $9$ core equations and simulate the case

from Task $2$ with at least two of the control vector components being $+-10\%$ from the trim values. Take zero

initial position and some reasonable value for the initial altitude close to the sea level. Plot the time histories

for the $9$ core states and the flight path angle, course angle, and altitude. Use different time ranges to investigate

what happens in the first $5-10$ seconds and also in the first $1-2$ minutes. Animate the attitude motion. Plot the

CoM trajectory. Comment on the plots.