use the rk4 code(is Runge-Kutta method of 4th order) use Matlab plz, I need Matlab code

Matlab script. Consider the rotational motion of spacecraft in 1-dimensional space. Answer the following questions. In the following discussion, the state space is defined to be X = [0,0,t]", where 0 is the rotation angle, o is the angular velocity, and t is time. Note that for X, the units of the first, second, and third elements are rad, rad/sec, and sec, respectively. I is used to describe the moment of inertia. 1. Assume that there is no torque acting on the spacecraft. Develop an RK4 scheme to answer the following questions. (a) Solve this equation numerically by assuming X = [0,0.1,07 at t = 0 sec and I = 3.293 kg m to show X at t = 8.32 sec. A x 10 B x 10-1 C x 100 (b) Solve this equation numerically by assuming X = [0.108,-0.023,07 at t = 0 sec and I = 8.319 kg m to show X at t = 13.19 sec. D x 10 E x 10 2 Fx 10' Matlab script. Consider the rotational motion of spacecraft in 1-dimensional space. Answer the following questions. In the following discussion, the state space is defined to be X = [0,0,t]", where 0 is the rotation angle, o is the angular velocity, and t is time. Note that for X, the units of the first, second, and third elements are rad, rad/sec, and sec, respectively. I is used to describe the moment of inertia. 1. Assume that there is no torque acting on the spacecraft. Develop an RK4 scheme to answer the following questions. (a) Solve this equation numerically by assuming X = [0,0.1,07 at t = 0 sec and I = 3.293 kg m to show X at t = 8.32 sec. A x 10 B x 10-1 C x 100 (b) Solve this equation numerically by assuming X = [0.108,-0.023,07 at t = 0 sec and I = 8.319 kg m to show X at t = 13.19 sec. D x 10 E x 10 2 Fx 10