I have to transform two models into Laplace transforms and then into transfer functions. They refer to a missile travelling through the air, assuming perfect/ideal condtions i.e, no wind , no impact on missile’s Yaw or Roll. I am interested in analyzing the missile’s pitch angle θ only.
For the first model I have Y(s)=5/(s^2+20s+4)
For the second I have Y(s)=4/(s+(1/τ)).
I am rather unsure if these are correct as I am not the best at Laplace transforms!
For the first model I have Y(s)=5/(s^2+20s+4)
For the second I have Y(s)=4/(s+(1/τ)).
I am rather unsure if these are correct as I am not the best at Laplace transforms!
