Task #2: Create a .m file for the "Zprime" function, and create a MATLAB program (that calls "ZPrime") to solve for the spacecraft's motion from t=0 to t=24, given the following initial data:

-17 x y D ES115 M Project.pdf x C Chegg Study l Guided Sc x e https://blackboard.hartford.edu/bbcswebdav/pid-1566272-dt-content-rid-572 You are given: d2 x d y M (x-E) x d t2 d t rz dx E y M y d t2 dt r 3 (x M)2 y