Control
System Design - Biplane - Root Locus
The system has a closed loop transfer function with a denominator of:

The root locus for
the system is shown below.

Using this root locus
answer the following questions.
-
For what gain does the
system become unstable?
-
What is the fastest response
time (say 10-90 rise time) that can be achieved with this system?
-
What is the best damping
that can be achieved with this system?