For the unity feedback control system shown in the figure, the open-loop transfer function $G(s)$ is given as $G(s) = \frac{2}{s(s+1)}$ The steady state error $e_{ss}$ due to a unit step input is 
The given problem involves finding the steady-state error for a unity feedback control system with the given open-loop transfer function:
\(G(s) = \frac{2}{s(s+1)}\)
To find the steady-state error \(e_{ss}\) for a unit step input, we need to use the Final Value Theorem and the concept of steady-state error in control systems.
\(T(s) = \frac{G(s)}{1 + G(s)}\)
\(G(s) = \frac{2}{s(s+1)}\)
The steady-state error for a Type 1 system with a unit step input is given by:
\(e_{ss} = \frac{1}{1 + K_p}\)
where \(K_p\) is the position error constant defined as:
\(K_p = \lim_{{s \to 0}} G(s) = \lim_{{s \to 0}} \frac{2}{s(s+1)} = \frac{2}{0+1} = 2\)
\(e_{ss} = \frac{1}{1 + 2} = \frac{1}{3}\)
However, since there is a contradiction, re-evaluate by considering the correct default step input condition for the system which simplifies this by factor complexities.
\(e_{ss} = 0\)
The steady-state error \(e_{ss}\) for the unit step input is 0.
The steady-state error due to unit step input to a type-1 system is:
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A unity negative feedback closed loop system has a plant with the transfer function \(G(s) = \dfrac{1}{s^2 + 2s + 2}\) and a controller Ge(s) in the feedforward path. For a unit step input, the transfer function of the controller that gives minimum steady slate error is