Assignment You plan to launch a rocket that has the parameters provided below, you are to write a program that will calculate flight trajectory without wind resistance. Your program is to utilize the finite difference approach for calculating trajectory parameters every 0.01 seconds until it hits the ground (negative elevation). As before, see that your program code and output plots are properly documented as directed by tutorials provided in this course. When the trajectory has been calculated, you are to generate the following plots: 1st Plot Window": acceleration, velocity, height, and mass versus time. 2nd Plot Window: Force of Thrust vs Time 3rd Plot Window: Kinetic Energy, Potential Energy, and Total Energy vs Time Upon completing the assignment, submit a single .m file on Moodle. *Note that the first four graphs are all Subplots in one Window (2 columns 2 rows). . . 0.0 sec Initial Conditions: Initial elevation: Casing mass: Fuel mass: Fuel burn rate: 1m 16 kg 134 kg 4.8 kg/sec Initial time: Time increments: Force of thrust: 0.01 sec 1560 N Assignment You plan to launch a rocket that has the parameters provided below, you are to write a program that will calculate flight trajectory without wind resistance. Your program is to utilize the finite difference approach for calculating trajectory parameters every 0.01 seconds until it hits the ground (negative elevation). As before, see that your program code and output plots are properly documented as directed by tutorials provided in this course. When the trajectory has been calculated, you are to generate the following plots: 1st Plot Window": acceleration, velocity, height, and mass versus time. 2nd Plot Window: Force of Thrust vs Time 3rd Plot Window: Kinetic Energy, Potential Energy, and Total Energy vs Time Upon completing the assignment, submit a single .m file on Moodle. *Note that the first four graphs are all Subplots in one Window (2 columns 2 rows). . . 0.0 sec Initial Conditions: Initial elevation: Casing mass: Fuel mass: Fuel burn rate: 1m 16 kg 134 kg 4.8 kg/sec Initial time: Time increments: Force of thrust: 0.01 sec 1560 N