Question 1
During stability analysis, what does a well-damped aircraft response usually suggest for control design?
Question 2
If analysis shows a lightly damped pitch oscillation, which control choice is most directly aimed at improving the response?
Question 3
Why do engineers study an airplane's natural modes before selecting control gains?
Question 4
What is a common sign that the control gain is too high?
Question 5
In a simple feedback loop, what two things are compared?
