Concept:
The steady-state error ($e_{ss}$) of a closed-loop control system depends on both the type of the open-loop transfer function $G(s)H(s)$ and the nature of the reference input. The general expression for steady-state error using the Final Value Theorem is:
\[
e_{ss} = \lim_{s \rightarrow 0} \frac{s \cdot R(s)}{1 + G(s)H(s)}
\]
Step 1: Identify system Type and Input configuration.
The given open-loop transfer function is:
\[
G(s) = \frac{10}{s(s+2)}
\]
Since there is a single isolated integrator pole at the origin ($s^1$ in the denominator), this is a Type 1 system. The feedback system is a unity configurations, meaning $H(s) = 1$. The reference input is a unit step function, which in the Laplace domain is:
\[
R(s) = \frac{1}{s}
\]
Step 2: Calculate the Position Error Constant ($K_p$).
For a step input, the steady-state error is given by:
\[
e_{ss} = \frac{1}{1 + K_p}
\]
where $K_p$ is the static position error constant defined as:
\[
K_p = \lim_{s \rightarrow 0} G(s)H(s) = \lim_{s \rightarrow 0} \frac{10}{s(s+2)}
\]
Evaluating this limit as $s$ approaches 0:
\[
K_p = \frac{10}{0 \cdot (0+2)} = \frac{10}{0} \rightarrow \infty
\]
Step 3: Evaluate the final steady-state error.
Substitute the infinite value of $K_p$ into the steady-state error formula:
\[
e_{ss} = \frac{1}{1 + \infty} = 0
\]
This shows that a Type 1 system tracks a step input with zero steady-state error.