Sign in to save

Bookmark this page so you can find it later.

Sign in to save

Bookmark this page so you can find it later.

Root locus sketching shows how the closed-loop poles of a feedback control system move as a gain parameter changes. This cheat sheet helps engineering students organize the standard sketching rules into a reliable sequence. It is useful for exams, design problems, and quick checks of stability and transient response trends.

A clear root locus sketch connects algebraic characteristic equations to controller design choices.

The core idea is to apply the open-loop transfer function G(s)H(s) and study points s that satisfy the angle and magnitude conditions. Important rules include locating open-loop poles and zeros, finding real-axis segments, computing asymptotes, and identifying breakaway or break-in points. Imaginary-axis crossings are commonly found using the Routh-Hurwitz criterion.

Once the locus is sketched, gain values and pole locations can be interpreted in terms of damping, natural frequency, settling time, and stability.

Key Facts

  • For negative unity feedback, the closed-loop characteristic equation is 1 + K G(s)H(s) = 0.
  • A point s is on the root locus if angle G(s)H(s) = (2q + 1)180 degrees, where q is any integer.
  • The gain at a point on the locus is K = 1 / |G(s)H(s)| when the characteristic equation is 1 + K G(s)H(s) = 0.
  • The number of root locus branches equals the number of open-loop poles of G(s)H(s).
  • Root locus branches start at open-loop poles when K = 0 and end at open-loop zeros or at infinity as K approaches infinity.
  • A point on the real axis is on the root locus if the number of real open-loop poles and zeros to its right is odd.
  • The asymptote centroid is sigma_a = (sum of open-loop poles - sum of open-loop zeros) / (n - m), where n is the number of poles and m is the number of zeros.
  • The asymptote angles are theta_k = (2k + 1)180 degrees / (n - m), for k = 0, 1, 2, ..., n - m - 1.

Vocabulary

Root locus
A plot of closed-loop pole locations in the s-plane as the gain K varies from 0 to infinity.
Open-loop pole
A value of s that makes the denominator of G(s)H(s) equal to zero.
Open-loop zero
A value of s that makes the numerator of G(s)H(s) equal to zero.
Asymptote
A straight-line direction followed by root locus branches that go to infinity.
Breakaway point
A point on the real axis where two or more root locus branches leave the real axis.
Routh-Hurwitz criterion
A tabular test used to determine stability and find gain values where roots cross the imaginary axis.

Common Mistakes to Avoid

  • Counting real-axis segments incorrectly is wrong because only poles and zeros to the right of the test point determine whether the count is odd.
  • Using the number of zeros instead of the number of poles for the branch count is wrong because every branch begins at an open-loop pole.
  • Forgetting zeros at infinity is wrong because when n > m, exactly n - m branches must go to infinity along asymptotes.
  • Choosing every solution of dK/ds = 0 as a breakaway point is wrong because the candidate must lie on a valid real-axis root locus segment.
  • Assuming a sketch proves stability for all gains is wrong because imaginary-axis crossings and gain ranges should be checked with Routh-Hurwitz or direct substitution.

Practice Questions

  1. 1 For G(s)H(s) = K / [s(s + 2)(s + 5)], how many root locus branches are there, and how many asymptotes go to infinity?
  2. 2 For G(s)H(s) = K(s + 4) / [s(s + 1)(s + 3)], find the asymptote centroid sigma_a.
  3. 3 For open-loop poles at 0, -2, and -6 with no finite zeros, list the real-axis intervals that belong to the root locus.
  4. 4 Explain why adding a zero near the desired closed-loop pole location can reshape the root locus and affect transient response.