MATLAB Assignment-Assigned Jan 28; due Friday at noon, Feb 7 (submit a ".m" file on Moodle). 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 this course. When the trajectory has been calculated, you are to generate the following plots: 1" Plot Window - four graph plots 15, 20, 3d, & 4 graphs-allas Subplots in one Window (2 columns 2 rows) Acceleration vs Time Velocity vs Time Height vs Time Mass vs Time 2 Plot Window Force of Thrust vs Time 3d Plot Window Kinetic Energy, Potential Energy, and Total Energy vs Time (Unlike plot showbelow, include axis labels for energy and time w/units) Initial elevation: Casing mass: Fuel mass: Fuel burn rate: 1m 16 kg 134 kg 4.7 kg/sec Initial time: Time increments: Force of thrust: 0.0 sec 0.01 sec 1560 N Considerations: 1. Upwards is positive. 2. Ground level has an elevation of zero. 3. Thrust becomes zero when you run out of gas. 4. You will see the acceleration increase because of total mass reduction ... until you lose thrust. eg Please use the following variable names to help me read and grade - 150 programs: Gray, acceleration mfuel Furl mass Lathrust Thrust accel. tot Total mass total T otal acceleration pe Potential energy dums. Length of time step time Flapsed time thrust Force of thrust height Elevation vel clocity Index, or counter Kinetic energy Changes with time Case Casing mass Ls Totale If you get it your plot mich look something b etractly like the following... notice that I have not followed my own requirements for labeling plans I would give m e a mer credit because of this MATLAB Assignment-Assigned Jan 28; due Friday at noon, Feb 7 (submit a ".m" file on Moodle). 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 this course. When the trajectory has been calculated, you are to generate the following plots: 1" Plot Window - four graph plots 15, 20, 3d, & 4 graphs-allas Subplots in one Window (2 columns 2 rows) Acceleration vs Time Velocity vs Time Height vs Time Mass vs Time 2 Plot Window Force of Thrust vs Time 3d Plot Window Kinetic Energy, Potential Energy, and Total Energy vs Time (Unlike plot showbelow, include axis labels for energy and time w/units) Initial elevation: Casing mass: Fuel mass: Fuel burn rate: 1m 16 kg 134 kg 4.7 kg/sec Initial time: Time increments: Force of thrust: 0.0 sec 0.01 sec 1560 N Considerations: 1. Upwards is positive. 2. Ground level has an elevation of zero. 3. Thrust becomes zero when you run out of gas. 4. You will see the acceleration increase because of total mass reduction ... until you lose thrust. eg Please use the following variable names to help me read and grade - 150 programs: Gray, acceleration mfuel Furl mass Lathrust Thrust accel. tot Total mass total T otal acceleration pe Potential energy dums. Length of time step time Flapsed time thrust Force of thrust height Elevation vel clocity Index, or counter Kinetic energy Changes with time Case Casing mass Ls Totale If you get it your plot mich look something b etractly like the following... notice that I have not followed my own requirements for labeling plans I would give m e a mer credit because of this
