\[C(j0) = K = 20\log K (dB).\]
\[C(j\omega) = K/\beta = 20\log K-20\log \beta (dB).\]
Consider again the solar tracking system, The transfer function of the system is given by \[G(s) = \frac{10}{s(s+1)}.\] Design a lag compensator such that \[K_v \geq 100,\,\phi_m \geq 40^\circ,\, K_g \geq 10\text{dB}.\]
We will use the straight line approximation:
We choose \(T = 10/\omega_g = 10.\)
The phase margin is \(44.5^\circ\) and the gain margin is \(\infty\).
After the compensation, the system responses slower, but has less overshoot. Also the system is more robust to noise.
Lead Compensator | Lag Compensator | |
---|---|---|
Rise Time | \(\downarrow\) | \(\uparrow\) |
Gain Crossover Frequency | \(\uparrow\) | \(\downarrow\) |