Elio Saade
Note

Type 0, 1, 2, 3 Systems

Topics: Feedback Control Systems

The type of the system refers to the number of poles at the origin s=0s=0 in the system, also known as free integrators.

Type 0:

G(s)=K(s−z1)...(s−zm)(s−p1)...(s−pm)G(s) = K \frac{(s-z_1) ... (s-z_m)}{(s-p_1) ... (s-p_m)}

Type 1:

G(s)=K(s−z1)...(s−zm)s(s−p1)...(s−pm)G(s) = K \frac{(s-z_1) ... (s-z_m)}{s(s-p_1) ... (s-p_m)}

Type 2:

G(s)=K(s−z1)...(s−zm)s2(s−p1)...(s−pm)G(s) = K \frac{(s-z_1) ... (s-z_m)}{s^2(s-p_1) ... (s-p_m)}

Type 3:

G(s)=K(s−z1)...(s−zm)s3(s−p1)...(s−pm)G(s) = K \frac{(s-z_1) ... (s-z_m)}{s^3(s-p_1) ... (s-p_m)}

The system type relates to the steady-state error of the system given certain types of inputs:
For zero steady-state error to a waveform with a Laplace transform 1/sk1/s^k, the forward transfer function must have at least kk free integrators.

In other words,

  • to have ess=0e_{ss} = 0 for a step input 1/s1/s (constant position), the system must be at least Type 1
  • to have ess=0e_{ss} = 0 for a ramp input 1/s21/s^2 (constant velocity), the system must be at least Type 2
  • to have ess=0e_{ss} = 0 for a step parabolic input 1/s1/s (constant acceleration), the system must be at least Type 3

The table below summarizes the steady-state error conditions
System_Types.png

References

  1. https://www.ocw.mit.edu/courses/2-004-dynamics-and-control-ii-spring-2008/519745ee31d586a1320098c606fc31aa_lecture_24.pdf

Connections

Direct relationships to this note.