Guidance and trajectory for a missile

Trajectory and guidance analysis

this question is from advance weapon system about flying a proectile

You are to evaluate guidance laws while flying a projectile to a stationary intercept point in your 2-D simulation (use the ProjectileFramework Matlab script). You will evaluate how the initial conditions of a guidance law effect the trajectory shape, and you are to prove (or disprove) basic guidance optimization criteria, and common “rules of thumb” in the guidance field

[darova]

What is the question? Do you have problemS?

[Image Analyst]

For what it's worth, attached is my demo for computing and showing just about everything you could possibly want to know about trajectory and a projectile. It has variables/parameters for initial conditions like height, speed, angle, etc.