A satellite attitude control system, as shown below, has a plant with transfer function $G(s) = \frac{1}{s^2}$ cascaded with a compensator $C(s) = \frac{K(s+\alpha)}{s+4}$, where $K$ and $\alpha$ are positive real constants. 
In order for the closed-loop system to have poles at $-1 \pm j\sqrt{3}$, the value of $a$ must be __________
To find the value of \( \alpha \) such that the closed-loop system has poles at \( s = -1 \pm j\sqrt{3} \), we use the Angle Criterion from the Root Locus method.
The open-loop transfer function \( L(s) \) is the product of the compensator \( C(s) \) and the plant \( G(s) \):
$$L(s) = C(s)G(s) = \frac{K(s + \alpha)}{s+4} \cdot \frac{1}{s^2} = \frac{K(s + \alpha)}{s^2(s + 4)}$$
From this, we identify the open-loop poles and zeros:
For a point \( s_0 \) to be a closed-loop pole, it must satisfy the angle condition:
$$\sum \angle(s_0 + z_i) - \sum \angle(s_0 + p_i) = \pm 180^\circ (2n + 1)$$
Let the target pole be \( s_0 = -1 + j\sqrt{3} \).
Let \( \phi_z \) be the angle contributed by the zero at \( s = -\alpha \). Applying the angle criterion:
$$\phi_z - (240^\circ + 30^\circ) = -180^\circ$$ $$\phi_z - 270^\circ = -180^\circ$$ $$\phi_z = 90^\circ$$
The angle of the vector from the zero at \( -\alpha \) to the point \( s_0 = -1 + j\sqrt{3} \) is given by:
$$\angle(s_0 + \alpha) = \angle((\alpha - 1) + j\sqrt{3}) = 90^\circ$$
For a complex number to have an angle of \( 90^\circ \), its real part must be zero and its imaginary part must be positive:
$$\alpha - 1 = 0 \implies \alpha = 1$$
In order for the closed-loop system to have poles at \( -1 \pm j\sqrt{3} \), the value of \( \alpha \) must be 1.
Given below are two statements:
Statement I: In proportional control, the actuating signal for the control action in a control system is proportional to the error signal
Statement II: It is desirable that control system be over damped for the point of view of quick response
In the light of the above statements, choose thecorrectanswer from the options given below:
Which of the following controllers improves the transient response of a system?
The transfer function of the lead compensator is:
Which of the following terms is responsible for noise measurement in the PID controller?
The overall transfer function of a control system is given by the following equation. Find out the value of Derivative rate feedback constant K t. (Consider the Damping ratio 0.9)
\(\dfrac{C(s)}{R(s)}= \dfrac{36}{s^2+3.6s+36}\)