Mais conteúdo relacionado
06,07 elec3114
- 1. 1
Stability
• How to determine the stability of a system represented
as a transfer function
• How to determine the stability of a system represented
in state space
• How to determine system parameters to yield stability
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 2. 2
lntroduction
Definitions of stability for linear, time-invariant systems using the natural
response:
1. A system is stable if the natural response approaches zero as time
approaches infinity.
2. A system is unstable if the natural response approaches infinity as time
approaches infinity.
3. A system is marginally stable if the natural response neither decays nor
grows but remains constant or oscillates.
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 3. 3
Bounded-input bounded-output (BIBO) definitions of stability for linear,
time-invariant systems using the total response
1. A system is stable if every bounded input yields a bounded output.
2. A system is unstable if any bounded input yields an unbounded output.
Stable systems have closed-loop transfer functions with poles only in
the left half-plane
Unstable systems have closed loop transfer functions with at least one
pole in the right half-plane and/or poles of multiplicity greater than one
on the imaginary axis
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 4. 4
Marginally stable systems have closed loop transfer functions with only
imaginary axis poles of multiplicity 1 and poles in the left half-plane
Stable System Unstable System
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 5. 5
Routh-Hurwitz Criterion
• yields stability information without the need to solve for the closed-
loop system poles
Two steps:
(1) Generate a data table called a Routh table
(2) Interpret the Routh table to tell how many closed-loop system poles are in
the left half-plane and in the right half-plane.
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 6. 6
Generating a Basic Routh Table
Note: any row of the Routh table can be multiplied by a positive
constant without changing the values of the rows below.
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 7. 7
Interpreting the Basic Routh Table
• the number of roots of the polynomial that are in the right half-plane is
equal to the number of sign changes in the first column.
- two sign changes, hence two poles in the right half-plane
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 8. 8
Problem: Find range of gain K for which the system is stable, K>0
Solution:
System is stable for K<1386
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 9. 9
Stability in State Space
• we can determine the stability of a system represented in state
space by finding the eigenvalues (poles) of the system matrix, A,
and determining their locations on the s-plane
• we can find the poles using equation:
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 10. 10
Steady-State Errors
• How to find the steady-state error for a unity feedback system
• How to specify a system's steady-state error performance
• How to find the steady-state error for disturbance inputs
• How to find the steady-state error for nonunity feedback systems
• How to design system parameters to meet steady-state error
performance specifications
• How to find the steady-state error for systems represented in state
space
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 11. 11
Steady-State Errors
Steady-state error is the difference between the input and the output for a
prescribed test input as t → ∞
Test waveforms for evaluating steady-state errors of control systems
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 13. 13
Sources of Steady-State Errors
- zero error in the steady state
for a step input
Error:
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 14. 14
Steady-State Error for Unity Feedback
Systems
Steady-State Error in Terms of T(s) – closed loop transfer function
… final value theorem
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 15. 15
Steady-State Error in Terms of G(s) – open loop transfer function
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 16. 16
Response to step, ramp and parabolic input
Step input
if (at least one pole must be
at origin)
Thus if n ≥ 1 then lim G ( s) = ∞ and e(∞) = 0
s →0
Ramp input
Thus if n ≥ 2 then lim sG ( s) = ∞ and e(∞) = 0
s →0
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 17. 17
Parabolic input
Thus if n ≥ 3 then lim s 2G ( s ) = ∞ and e(∞) = 0
s →0
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 18. 18
Static Error Constants and System Type
Static Error Constants
Thus, for a step input:
for a ramp input:
for a parabolic input:
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 19. 19
System Type
n=0 … Type 0 system
n=1 … Type 1 system
n=2 … Type 2 system
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 20. 20
Problem Given the control system, find the value of K so that there is 10% error
in the steady state.
Solution
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 21. 21
Steady-State Error for Disturbances (1)
E ( s) = R( s) − C ( s)
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 22. 22
Steady-State Error for Disturbances (2)
- let us assume a step disturbance
- hence error can be reduced by increasing the DC gain of G1(s)
or decreasing the dc gain of G2(s)
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 23. 23
Steady-State Error for Nonunity Feedback Systems (1)
• Control systems often do not have unity feedback because of the
compensation used to improve performance or because of the physical
model for the system.
• When nonunity feedback is present, the plant's actuating signal is not the
actual error or difference between the input and the output.
G1(s) … input transducer
G2(s) … plant
H1(s) … feedback
G ( s ) = G1 ( s )G2 ( s )
H ( s ) = H1 ( s ) / G1 ( s )
Ea(s) … actuating signal (not the actual error)
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 24. 24
Steady-State Error for Nonunity Feedback Systems (2)
Let us modify, the block diagram to show explicitly the actual error E(s)=R(s)-C(s)
Ea(s) … actuating signal
(not the actual error)
E(s)=R(s)-C(s)
actual error
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 25. 25
Steady-State Error for Nonunity Feedback Systems (3)
- both disturbance and
nonunity feedback
If we consider step input and step disturbance, then R(s)=D(s)=1/s and
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 26. 26
For zero error:
Above equation can be satisfied if:
1. System is stable
2. G1 is a Type 1system
3. G2 is a Type 0 system
4. H is a Type 0 system with DCgain=1
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 27. 27
Problem Determine the system type, error constant, and the steady state error
for a unit step
Solution
E(s)=R(s)-C(s)
actual error
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 28. 28
Sensitivity
Sensitivity - the degree to which changes in system parameters affect system
transfer functions, and hence performance.
Sensitivity is the ratio of the fractional change in the function to the fractional
change in the parameter as the fractional change of the parameter approaches zero.
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 29. 29
Problem Find the sensitivity of the steady-state error to changes in parameter K
and parameter a for the system with a step input
Solution
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 30. 30
Steady-State Error for Systems in State Space
(1) analysis via final value theorem
(2) analysis via input substitution
Analysis via Final Value Theorem
closed-loop transfer
function
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 31. 31
Analysis via Input Substitution – avoids taking inverse of (sI - A)
Step input (r = 1)
If the input is a unit step r = 1 then a steady-state solution xSS for x is:
where Vi is constant.
yss = CV = −CA −1B
Thus, for a unit step input:
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.
- 32. 32
Ramp inputs (r = t)
We balance the equation:
Control Systems Engineering, Fourth Edition by Norman S. Nise
Copyright © 2004 by John Wiley & Sons. All rights reserved.