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e-ISSN: 2582-5208
International Research Journal of Modernization in Engineering Technology and Science
Volume:02/Issue:04/April-2020 www.irjmets.com
www.irjmets.com @International Research Journal of Modernization in Engineering, Technology and Science
[111]
STATE AND DISTURBANCE ESTIMATION OF A LINEAR SYSTEMS
USING PROPORTIONAL INTEGRAL OBSERVER
Mustefa Jibril*1
, Messay Tadese*2
, Eliyas Alemayehu Tadese*3
*1,2
Msc, School of Electrical & Computer Engineering, Dire Dawa Institute of Technology, Dire Dawa, Ethiopia
*3
Msc, Faculty of Electrical & Computer Engineering, Jimma Institute of Technology, Jimma, Ethiopia
ABSTRACT
This paper offers a short survey of linear systems Proportional-Integral-Observer design. This observer has the capacity
to estimate simultaneously the states and unknown inputs which include disturbances or model uncertainties appearing
on the system. The design of state and output estimation using PO and state, output and disturbance estimation using
PIO is done using Matlab/Simulink successfully. The simulation is done for estimating using PO and PIO and the
results proved that estimates the state variables and output correctly when there is no disturbance in the plant and there
is a constant steady-state error in estimation after leading a constant disturbance into the plant for both state variables
and plant output for the Proportional Observer and there is ability to estimate state variables, disturbance and system
output correctly with or without the disturbance in plant for the Proportional Integral Observer.
Keywords: Proportional Integral Observer, Proportional Observer, uncertainties
I. INTRODUCTION
Observers play a vital rules on control system because some control techniques require the accurate estimation of
system to realize the close loop control obligations. Measuring all states is not usually feasible due to the fact a few
states aren't measurable or the usage of sensors may additionally too high priced. Meanwhile excessive quality
performance may be accomplished thru the estimation of unknown inputs affecting the system inclusive of disturbances
or model uncertainties. Beside the estimation of states and unknown inputs, observers are also able to growth the control
performance. In this contribution a quick survey and evaluation of PI-Observer design and its formulation for a linear
system is presented
II. STATE AND DISTURBANCE ESTIMATION
The state-space model of an nth
order, p input and qoutput plant with l independent disturbance of constant value is
described as:
 
˙
1
˙ 0
x Ax Bu Ed
d
   

 
The plant state vector x is n × 1, the plant input vector u is p × 1, and the independent disturbance d is an l × 1 vector. In
case of the disturbance model is unknown, the matrix E can be assumed to be identity matrix with the same order of
plant. The output y, a q × 1 vector, of the plant is:
 2y Cx
Figure 1: Block diagram of proportional observer
e-ISSN: 2582-5208
International Research Journal of Modernization in Engineering Technology and Science
Volume:02/Issue:04/April-2020 www.irjmets.com
www.irjmets.com @International Research Journal of Modernization in Engineering, Technology and Science
[112]
Proportional observers are built to estimate state variables using the plant input and output, as is shown in Figure 1. The
state-space model of proportional observer in shown as follows:
   ˙
ˆ ˆ ˆ 3x Ax Bu L y Cx   
In which xˆ is the estimated of state variables. Subtract equation (3) from (1), letting e = x − xˆ, which is the error
between actual and estimated variables and disturbances, so that:
     ˙
ˆ ˆ 4e x x Ax Ed A LC x Ly A LC e Ed          
Therefore, if there is no disturbance in plant (d = 0), a proportional observer has the ability to estimate the state
variables, if (A−LC) is Routh-Hurwitz stable which means all eigenvalues of (A−LC) have negative real parts. However,
if d is a non-zero constant, there will be a constant steady-state error between the estimated and actual state variables.
In order to eliminate this error in estimation, disturbance observer (DO) is described as follows:
 
 
 
ˆˆ ˆ ˆ
5
ˆ ˆ
P
I
x Ax Bu L y Cx Ed
d L y Cx
     

  


According to the definition [5], the state space mode of proportional integral observer is:
 
 
 
ˆ ˆ ˆ
6
ˆ
x Ax Bu Ev G y Cx
v F y Cx
     

  


Comparing equation (5) and equation (6), it is obvious that disturbance observer can be regarded as proportional integral
observer in a special case. The block diagram of proportional integral observer is shown in Figure 2.
Figure 2: Block diagram of proportional integral observer
Recall the state space model of the plant with disturbance described by equation (1). These two equations can be
combined together by defining
x
z
d
 
  
 
, so that
 7
0 0 0
Z Z
A E x B
z u A z B u
d
     
        
     

The output of the plant is given by the following equation:
   0 8Z
x
y Cx C C z
d
 
   
 
e-ISSN: 2582-5208
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[113]
Similarly, the state space model of disturbance observer described by equation (5) can also be rewritten into the
following equation by defining
ˆ
ˆ
ˆ
x
z
d
 
  
 
:
 ˆ ˆ 9
00
p p
I I
A L C E L B
z z y u
L C L
     
       
     

By forming
,
 
 
   
 
0 0
0
0
Z n l n l
Z n l p
Z q n l
p
Z n l q
I
A E
A
B
B
C C
L
L
L
  
 
 
 
 
  
 
 
  
 

 
  
 
Equation (9) is equivalent to:
 
 
 
ˆ ˆ0
0 0 0 10
ˆ
p p
I I
Z Z Z Z Z
L LA E B
z C z y u
L L
A L C z L y B u
       
                    

    

In this paper, the state space model of plant with disturbance (AZ,BZ,CZ) described by equation (7) will be called the
extended plant model, and the state space model of DO described by equation (10) will be called the extended observer.
Subtract equation (7) by equation (10), letting e = z − zˆ, which is the error between actual and estimated variables and
disturbances, so that:
Noticing that y = Czz in equation (8), the equation above can be rewritten as:
     ˆ 12z Z Z Z Z Z Z Z Z Ze A z L C z A L C z A L C e     
Thus, as long as
0
p
Z Z Z
I
A L C E
A L C
L C
 
   
 
is Routh-Hurwitz stable, the error between actual and estimated
variables will become zero as t →∞
Recall equation (8) and (10):
 
 
ˆ ˆ
13Z Z Z Z Z
Z
z A L C z L y B u
y C z
    

 

Comparing the equations above with the state-space model of proportional observer described by equation (2) and (3):
e-ISSN: 2582-5208
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[114]
 
 
ˆ ˆ
14
x A LC x Ly Bu
y Cx
    

 

It is obvious that the extended PIO model has the same formation with PO, by changing (A, B, C, L) into (AZ,BZ,CZ,LZ).
Therefore, disturbance observer and proportional integral observer both can be regarded as a higher order proportional
observer for the extended model, with
ˆ
ˆ
ˆ
x
z
d
 
  
 
. Thus, design methods for proportional observers can be applied to
observer gain L calculation for proportional integral observers with this extended observer model.
III. ILLUSTRATIVE EXAMPLES
3.1 State and Output Estimation with PO
A 3rd order single-input, single-output (SISO) system, the state space model is given by:
 
4 2 2 10 1
20 20 5 , 2 , 1 0 1 , 2.828
16 8 8 0.1 3.464
A B C E
     
     
          
           
The initial state of the system is  3.142 2.718 0.618
T
ox  , and a constant disturbance d = 10 is added to the
plant at t = 2 sec. The PO state space representation is
51.31 27.15 50.31 4.631 6 1 0 0 0 0
136.6 51.3 144.6 , 15.46 5 , 0 1 0 , 0 0
48.99 28.49 80.99 7.299 0.9 0 0 1 0 0
PO PO PO POA B C D
        
       
            
               
The Simulink model for the Estimated and actual state variables and Estimated and actual system output using PO is
shown in Figure 3 below.
Figure 3: Simulink model for the Estimated and actual state variables and Estimated and actual system output using PO
e-ISSN: 2582-5208
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[115]
The estimated and actual state variables and estimated and actual system output using PO simulation result is shown in
Figure 4 and Figure 5 respectively.
Figure 4: Estimated and actual state variables
Figure 5: Estimated and actual system output
e-ISSN: 2582-5208
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[116]
The simulation result given by Figure 4 and 5 shows that proportional observer estimates the state variables and output
correctly when there is no disturbance in the plant for t < 2 sec. However, there will be a constant steady-state error in
estimation after leading a constant disturbance into the plant at t = 2 sec, for both state variables and plant output.
3.2 State, Output and Disturbance Estimation with PIO
A 3rd order single-input, single-output (SISO) system, the state space model is given by:
 
4 4 6 10 4
25 10 15 , 21 , 1 0 1 , 1.43
16 18 8 0.98 4.34
A B C E
     
     
          
           
The initial state of the system is  2.82 4.6 0.8
T
ox  , and a constant disturbance d = 10 is added to the plant at t
= 2 sec. The PIO state space representation is
91.43 2 89.43 1 87.43 10 1 0 0 0 0 0
91.4 20 105.4 1.414 111.4 1 0 1 0 0 0 0
, , ,
40.73 4 24.73 1.732 28.73 0.1 0 0 1 0 0 0
359.3 0 359.3 0 359.3 0 0 0 0 1 0 0
PIO PIO PIO PIOA B C D
        
       
            
        
       
        
The Simulink model for the estimated and actual state variables and estimated and actual system output using PIO is
shown in Figure 6 below.
Figure 6: Simulink model for the Estimated and actual state variables and Estimated and actual system output using PIO
e-ISSN: 2582-5208
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[117]
The estimated and actual state variables, estimated and actual system output and estimated disturbance using PIO
simulation result is shown in Figure 7, Figure 8 and Figure 9 respectively.
Figure 7: Estimated and actual state variables
Figure 8: Estimated and actual system output
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[118]
Figure 9: Estimated disturbance
As is shown in Figure 7, 8 and 9, simulation result shows that PIO has the ability to estimate state variables, disturbance
and system output correctly within 0.6 sec, with or without the disturbance in plant.
IV. CONCLUSION
Observers are systems that estimate the values of unmeasured state variables from input-output measurements. The
envisioned state variables produced by means of proportional observers converge to the values of the actual ones if
there are no disturbances appearing on the plant. In the presence of disturbances, a proportional integral observer is
wanted to gain correct estimations. For the proportional observer, the simulation result shows that estimates the state
variables and output correctly when there is no disturbance in the plant and there is a constant steady-state error in
estimation after leading a constant disturbance into the plant for both state variables and plant output. For the
proportional integral observer, the simulation result shows that the ability to estimate state variables, disturbance and
system output correctly with or without the disturbance in plant.
V. REFERENCES
[1] Abdellah B et al. “Actuator Fault Estimation Based on Proportional Integral Observer for Discrete Time Switched
Systems” Journal of Dynamic Systems, Measurement and Control, Vol. 141, No. 3, 2019.
[2] Eyes B et al. “Design of a Proportional Integral Observer Based on Sliding Mode Principle for Uncertain Takagi-
Sugeno Fuzzy Systems: Applications to a Turbo Reactor” International Journal of Automation and Control, Vol.
12, Issue. 2, 2018.
[3] W. He et al. “Incremental Passivity Based Control for DC-DC Boost Converters under Time Varying Disturbances
via Generalized Proportional Integral Observer” Journal of Power Electronics, 2018.
[4] T Youssef et al.”Actuator and Sensor Faults Estimation Based on Proportional Integral Observer for TS Fuzzy
Model” Journal of the Franklin Institute, 2017.
[5] B Shafai et al. “Proportional Integral Observer in Robust Control, Fault Detection and Decentralized Control of
Dynamic Systems” Control and Systems Engineering, 2015.
[6] F. Bakhshande et al.”Proportional-Integral-Observer: A brief survey with special attention to the actual methods
using ACC Benchmark “IFAC-PapersOnline, Vol. 48, Issue.1,pp. 532–537, 2015.
[7] Nan GAO et al.”H infinity dynamic observer design for linear time invariant systems” 53rd IEEE Conference on
Decision and Control, December, 15-17, 2014. Los Angeles, California, USA
[8] Baishun Liu et al.”Conventional and Added-Order ProportionalNonlinear Integral Observers” International Journal
of Modern Nonlinear Theory and Application, Vol. 3, pp. 210-220, 2014.

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  • 1. e-ISSN: 2582-5208 International Research Journal of Modernization in Engineering Technology and Science Volume:02/Issue:04/April-2020 www.irjmets.com www.irjmets.com @International Research Journal of Modernization in Engineering, Technology and Science [111] STATE AND DISTURBANCE ESTIMATION OF A LINEAR SYSTEMS USING PROPORTIONAL INTEGRAL OBSERVER Mustefa Jibril*1 , Messay Tadese*2 , Eliyas Alemayehu Tadese*3 *1,2 Msc, School of Electrical & Computer Engineering, Dire Dawa Institute of Technology, Dire Dawa, Ethiopia *3 Msc, Faculty of Electrical & Computer Engineering, Jimma Institute of Technology, Jimma, Ethiopia ABSTRACT This paper offers a short survey of linear systems Proportional-Integral-Observer design. This observer has the capacity to estimate simultaneously the states and unknown inputs which include disturbances or model uncertainties appearing on the system. The design of state and output estimation using PO and state, output and disturbance estimation using PIO is done using Matlab/Simulink successfully. The simulation is done for estimating using PO and PIO and the results proved that estimates the state variables and output correctly when there is no disturbance in the plant and there is a constant steady-state error in estimation after leading a constant disturbance into the plant for both state variables and plant output for the Proportional Observer and there is ability to estimate state variables, disturbance and system output correctly with or without the disturbance in plant for the Proportional Integral Observer. Keywords: Proportional Integral Observer, Proportional Observer, uncertainties I. INTRODUCTION Observers play a vital rules on control system because some control techniques require the accurate estimation of system to realize the close loop control obligations. Measuring all states is not usually feasible due to the fact a few states aren't measurable or the usage of sensors may additionally too high priced. Meanwhile excessive quality performance may be accomplished thru the estimation of unknown inputs affecting the system inclusive of disturbances or model uncertainties. Beside the estimation of states and unknown inputs, observers are also able to growth the control performance. In this contribution a quick survey and evaluation of PI-Observer design and its formulation for a linear system is presented II. STATE AND DISTURBANCE ESTIMATION The state-space model of an nth order, p input and qoutput plant with l independent disturbance of constant value is described as:   ˙ 1 ˙ 0 x Ax Bu Ed d        The plant state vector x is n × 1, the plant input vector u is p × 1, and the independent disturbance d is an l × 1 vector. In case of the disturbance model is unknown, the matrix E can be assumed to be identity matrix with the same order of plant. The output y, a q × 1 vector, of the plant is:  2y Cx Figure 1: Block diagram of proportional observer
  • 2. e-ISSN: 2582-5208 International Research Journal of Modernization in Engineering Technology and Science Volume:02/Issue:04/April-2020 www.irjmets.com www.irjmets.com @International Research Journal of Modernization in Engineering, Technology and Science [112] Proportional observers are built to estimate state variables using the plant input and output, as is shown in Figure 1. The state-space model of proportional observer in shown as follows:    ˙ ˆ ˆ ˆ 3x Ax Bu L y Cx    In which xˆ is the estimated of state variables. Subtract equation (3) from (1), letting e = x − xˆ, which is the error between actual and estimated variables and disturbances, so that:      ˙ ˆ ˆ 4e x x Ax Ed A LC x Ly A LC e Ed           Therefore, if there is no disturbance in plant (d = 0), a proportional observer has the ability to estimate the state variables, if (A−LC) is Routh-Hurwitz stable which means all eigenvalues of (A−LC) have negative real parts. However, if d is a non-zero constant, there will be a constant steady-state error between the estimated and actual state variables. In order to eliminate this error in estimation, disturbance observer (DO) is described as follows:       ˆˆ ˆ ˆ 5 ˆ ˆ P I x Ax Bu L y Cx Ed d L y Cx             According to the definition [5], the state space mode of proportional integral observer is:       ˆ ˆ ˆ 6 ˆ x Ax Bu Ev G y Cx v F y Cx             Comparing equation (5) and equation (6), it is obvious that disturbance observer can be regarded as proportional integral observer in a special case. The block diagram of proportional integral observer is shown in Figure 2. Figure 2: Block diagram of proportional integral observer Recall the state space model of the plant with disturbance described by equation (1). These two equations can be combined together by defining x z d        , so that  7 0 0 0 Z Z A E x B z u A z B u d                       The output of the plant is given by the following equation:    0 8Z x y Cx C C z d        
  • 3. e-ISSN: 2582-5208 International Research Journal of Modernization in Engineering Technology and Science Volume:02/Issue:04/April-2020 www.irjmets.com www.irjmets.com @International Research Journal of Modernization in Engineering, Technology and Science [113] Similarly, the state space model of disturbance observer described by equation (5) can also be rewritten into the following equation by defining ˆ ˆ ˆ x z d        :  ˆ ˆ 9 00 p p I I A L C E L B z z y u L C L                      By forming ,           0 0 0 0 Z n l n l Z n l p Z q n l p Z n l q I A E A B B C C L L L                                Equation (9) is equivalent to:       ˆ ˆ0 0 0 0 10 ˆ p p I I Z Z Z Z Z L LA E B z C z y u L L A L C z L y B u                                     In this paper, the state space model of plant with disturbance (AZ,BZ,CZ) described by equation (7) will be called the extended plant model, and the state space model of DO described by equation (10) will be called the extended observer. Subtract equation (7) by equation (10), letting e = z − zˆ, which is the error between actual and estimated variables and disturbances, so that: Noticing that y = Czz in equation (8), the equation above can be rewritten as:      ˆ 12z Z Z Z Z Z Z Z Z Ze A z L C z A L C z A L C e      Thus, as long as 0 p Z Z Z I A L C E A L C L C         is Routh-Hurwitz stable, the error between actual and estimated variables will become zero as t →∞ Recall equation (8) and (10):     ˆ ˆ 13Z Z Z Z Z Z z A L C z L y B u y C z          Comparing the equations above with the state-space model of proportional observer described by equation (2) and (3):
  • 4. e-ISSN: 2582-5208 International Research Journal of Modernization in Engineering Technology and Science Volume:02/Issue:04/April-2020 www.irjmets.com www.irjmets.com @International Research Journal of Modernization in Engineering, Technology and Science [114]     ˆ ˆ 14 x A LC x Ly Bu y Cx          It is obvious that the extended PIO model has the same formation with PO, by changing (A, B, C, L) into (AZ,BZ,CZ,LZ). Therefore, disturbance observer and proportional integral observer both can be regarded as a higher order proportional observer for the extended model, with ˆ ˆ ˆ x z d        . Thus, design methods for proportional observers can be applied to observer gain L calculation for proportional integral observers with this extended observer model. III. ILLUSTRATIVE EXAMPLES 3.1 State and Output Estimation with PO A 3rd order single-input, single-output (SISO) system, the state space model is given by:   4 2 2 10 1 20 20 5 , 2 , 1 0 1 , 2.828 16 8 8 0.1 3.464 A B C E                                    The initial state of the system is  3.142 2.718 0.618 T ox  , and a constant disturbance d = 10 is added to the plant at t = 2 sec. The PO state space representation is 51.31 27.15 50.31 4.631 6 1 0 0 0 0 136.6 51.3 144.6 , 15.46 5 , 0 1 0 , 0 0 48.99 28.49 80.99 7.299 0.9 0 0 1 0 0 PO PO PO POA B C D                                               The Simulink model for the Estimated and actual state variables and Estimated and actual system output using PO is shown in Figure 3 below. Figure 3: Simulink model for the Estimated and actual state variables and Estimated and actual system output using PO
  • 5. e-ISSN: 2582-5208 International Research Journal of Modernization in Engineering Technology and Science Volume:02/Issue:04/April-2020 www.irjmets.com www.irjmets.com @International Research Journal of Modernization in Engineering, Technology and Science [115] The estimated and actual state variables and estimated and actual system output using PO simulation result is shown in Figure 4 and Figure 5 respectively. Figure 4: Estimated and actual state variables Figure 5: Estimated and actual system output
  • 6. e-ISSN: 2582-5208 International Research Journal of Modernization in Engineering Technology and Science Volume:02/Issue:04/April-2020 www.irjmets.com www.irjmets.com @International Research Journal of Modernization in Engineering, Technology and Science [116] The simulation result given by Figure 4 and 5 shows that proportional observer estimates the state variables and output correctly when there is no disturbance in the plant for t < 2 sec. However, there will be a constant steady-state error in estimation after leading a constant disturbance into the plant at t = 2 sec, for both state variables and plant output. 3.2 State, Output and Disturbance Estimation with PIO A 3rd order single-input, single-output (SISO) system, the state space model is given by:   4 4 6 10 4 25 10 15 , 21 , 1 0 1 , 1.43 16 18 8 0.98 4.34 A B C E                                    The initial state of the system is  2.82 4.6 0.8 T ox  , and a constant disturbance d = 10 is added to the plant at t = 2 sec. The PIO state space representation is 91.43 2 89.43 1 87.43 10 1 0 0 0 0 0 91.4 20 105.4 1.414 111.4 1 0 1 0 0 0 0 , , , 40.73 4 24.73 1.732 28.73 0.1 0 0 1 0 0 0 359.3 0 359.3 0 359.3 0 0 0 0 1 0 0 PIO PIO PIO PIOA B C D                                                         The Simulink model for the estimated and actual state variables and estimated and actual system output using PIO is shown in Figure 6 below. Figure 6: Simulink model for the Estimated and actual state variables and Estimated and actual system output using PIO
  • 7. e-ISSN: 2582-5208 International Research Journal of Modernization in Engineering Technology and Science Volume:02/Issue:04/April-2020 www.irjmets.com www.irjmets.com @International Research Journal of Modernization in Engineering, Technology and Science [117] The estimated and actual state variables, estimated and actual system output and estimated disturbance using PIO simulation result is shown in Figure 7, Figure 8 and Figure 9 respectively. Figure 7: Estimated and actual state variables Figure 8: Estimated and actual system output
  • 8. e-ISSN: 2582-5208 International Research Journal of Modernization in Engineering Technology and Science Volume:02/Issue:04/April-2020 www.irjmets.com www.irjmets.com @International Research Journal of Modernization in Engineering, Technology and Science [118] Figure 9: Estimated disturbance As is shown in Figure 7, 8 and 9, simulation result shows that PIO has the ability to estimate state variables, disturbance and system output correctly within 0.6 sec, with or without the disturbance in plant. IV. CONCLUSION Observers are systems that estimate the values of unmeasured state variables from input-output measurements. The envisioned state variables produced by means of proportional observers converge to the values of the actual ones if there are no disturbances appearing on the plant. In the presence of disturbances, a proportional integral observer is wanted to gain correct estimations. For the proportional observer, the simulation result shows that estimates the state variables and output correctly when there is no disturbance in the plant and there is a constant steady-state error in estimation after leading a constant disturbance into the plant for both state variables and plant output. For the proportional integral observer, the simulation result shows that the ability to estimate state variables, disturbance and system output correctly with or without the disturbance in plant. V. REFERENCES [1] Abdellah B et al. “Actuator Fault Estimation Based on Proportional Integral Observer for Discrete Time Switched Systems” Journal of Dynamic Systems, Measurement and Control, Vol. 141, No. 3, 2019. [2] Eyes B et al. “Design of a Proportional Integral Observer Based on Sliding Mode Principle for Uncertain Takagi- Sugeno Fuzzy Systems: Applications to a Turbo Reactor” International Journal of Automation and Control, Vol. 12, Issue. 2, 2018. [3] W. He et al. “Incremental Passivity Based Control for DC-DC Boost Converters under Time Varying Disturbances via Generalized Proportional Integral Observer” Journal of Power Electronics, 2018. [4] T Youssef et al.”Actuator and Sensor Faults Estimation Based on Proportional Integral Observer for TS Fuzzy Model” Journal of the Franklin Institute, 2017. [5] B Shafai et al. “Proportional Integral Observer in Robust Control, Fault Detection and Decentralized Control of Dynamic Systems” Control and Systems Engineering, 2015. [6] F. Bakhshande et al.”Proportional-Integral-Observer: A brief survey with special attention to the actual methods using ACC Benchmark “IFAC-PapersOnline, Vol. 48, Issue.1,pp. 532–537, 2015. [7] Nan GAO et al.”H infinity dynamic observer design for linear time invariant systems” 53rd IEEE Conference on Decision and Control, December, 15-17, 2014. Los Angeles, California, USA [8] Baishun Liu et al.”Conventional and Added-Order ProportionalNonlinear Integral Observers” International Journal of Modern Nonlinear Theory and Application, Vol. 3, pp. 210-220, 2014.