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STABILITY ANALYSIS
Introduction
The most important problem in linear control systems concerns stability.
That is, under what conditions will a system become unstable? If it is
unstable, how should we stabilize the system?
Stability may be defined as the ability of a system to restore its
equilibrium position when disturbed or a system which has a bounded
response for a bounded output.
Stability Analysis in the Complex Plane
The stability of a linear closed‐loop system can be determined from
the location of the closed‐loop poles in the s‐plane. If any of these poles
lie in the Right ‐Half of the s‐plane (RHS), (either the poles are real or
complex as shown in Fig. 1.) then with increasing time, they give rise to
the dominant mode, and the transient response increases monotonically or
oscillate with increasing amplitude. Either of these systems represents an
unstable system.
For such a system, as soon as the power is turned on, the output may
increase with time. If no saturation takes place in the system and no
mechanical stop is provided, then the system may eventually be damaged
and fail, since the response of a real physical system cannot increase
indefinitely.
Fig. 1. Poles located in RHS gives unstable response
Consider a simple feedback system shown in Fig. 2.
Fig. 2, closed-loop control system
The roots of the characteristic equation are called closed loop poles. The
location of such roots or poles on the s-plane will indicate the condition
of stability as shown in Fig. 3.
Fig. 3. Stability condition based on the location of the closed loop poles
Routh Stability criterion (Two Necessary But Insufficient Conditions)
Since most liner closed loop systems have closed loop transfer function
of the form
Where the a's and b's are constant and m ≤ n, we must first factor the
polynomial A(s) in order to find the closed loop poles.
Hurwitz Stability criterion (Necessary and Sufficient Condition)
Arrange the coefficients of the polynomial in rows and columns according to
the following pattern:
Routh-Hurwitz stability criterion states that the number of roots of the
characteristic equation with positive real parts is equal to the number of
changes in sign of the coefficients of the first column of the array.
It should be noted that the exact values of the terms in the first column
need not be known; instead, only the signs are needed.
The necessary and sufficient condition that all roots of the characteristic
equation lie in the left-half s plane is that:
a) All the coefficients of the characteristic equation be positive, and
b) All terms in the first column of the array have positive signs.
5 2020 05_06!01_10_30_pm
5 2020 05_06!01_10_30_pm
5 2020 05_06!01_10_30_pm

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BRAIN TUMOR DETECTION for seminar ppt.pdf
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5 2020 05_06!01_10_30_pm

  • 1. STABILITY ANALYSIS Introduction The most important problem in linear control systems concerns stability. That is, under what conditions will a system become unstable? If it is unstable, how should we stabilize the system? Stability may be defined as the ability of a system to restore its equilibrium position when disturbed or a system which has a bounded response for a bounded output. Stability Analysis in the Complex Plane The stability of a linear closed‐loop system can be determined from the location of the closed‐loop poles in the s‐plane. If any of these poles lie in the Right ‐Half of the s‐plane (RHS), (either the poles are real or complex as shown in Fig. 1.) then with increasing time, they give rise to the dominant mode, and the transient response increases monotonically or oscillate with increasing amplitude. Either of these systems represents an unstable system. For such a system, as soon as the power is turned on, the output may increase with time. If no saturation takes place in the system and no mechanical stop is provided, then the system may eventually be damaged and fail, since the response of a real physical system cannot increase indefinitely. Fig. 1. Poles located in RHS gives unstable response
  • 2. Consider a simple feedback system shown in Fig. 2. Fig. 2, closed-loop control system The roots of the characteristic equation are called closed loop poles. The location of such roots or poles on the s-plane will indicate the condition of stability as shown in Fig. 3. Fig. 3. Stability condition based on the location of the closed loop poles
  • 3. Routh Stability criterion (Two Necessary But Insufficient Conditions) Since most liner closed loop systems have closed loop transfer function of the form Where the a's and b's are constant and m ≤ n, we must first factor the polynomial A(s) in order to find the closed loop poles.
  • 4. Hurwitz Stability criterion (Necessary and Sufficient Condition) Arrange the coefficients of the polynomial in rows and columns according to the following pattern:
  • 5. Routh-Hurwitz stability criterion states that the number of roots of the characteristic equation with positive real parts is equal to the number of changes in sign of the coefficients of the first column of the array. It should be noted that the exact values of the terms in the first column need not be known; instead, only the signs are needed. The necessary and sufficient condition that all roots of the characteristic equation lie in the left-half s plane is that: a) All the coefficients of the characteristic equation be positive, and b) All terms in the first column of the array have positive signs.