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DESIGN OF A ROBUST FUZZY LOGIC CONTROLLER FOR A SINGLE-
LINK FLEXIBLE MANIPULATOR
K.RINI SOWHARIKA Dr.R.VIJAYA SANTHI
PG Scholar Asst.Professor
Department Electrical Engineering,
Andhra University,
Visakhapatnam,
Andhra Pradesh.
Abstract: In this paper, a single link flexible
manipulator is designed and controlled using a
fuzzy-PID controller. The controller is employed
to control an uncertain Flexible Robotic Arm and
its internal parameters in the motor dynamics. In
order to verify this method, proposed controller is
being tested against the conventional Integral and
PID controller. The simulation results show the
robustness of the proposed Fuzzy PID controller
under motor dynamics.
I. INTRODUCTION
FLEXIBLE arm manipulators span a wide range
of applications: space robots, nuclear maintenance,
microsurgery, collision control, contouring control,
pattern recognition, and many others. The system,
described by partial differential equations (PDEs), is
a distributed-parameter system of infinite
dimensions. Its non minimum phase behavior makes
it difficult to achieve high-level performance. Control
techniques such as linear control, optimal control,
adaptive control, sliding-mode control, neural
networks, or fuzzy logic deal with the control of
flexible manipulators and the modeling based on a
truncated (finite dimensional) model obtained from
either the finite-element method (FEM) or assumed
modes method. These methods require several
sensors to be used in order to obtain an accurate
trajectory tracking, and many of them also require the
knowledge of all the system parameters to design
properly the controller. Here a new method is
considered to cancel the vibration of the flexible
beam which gathers an online identification
technique with a control scheme in a suited manner,
with the only measures of both the motor angle
obtained from an encoder and the coupling torque
obtained from a pair of strain gauges as done in the
work in. In that paper, the nonlinearities effect in the
motor dynamics, such as the Coulomb friction torque.
Robust control schemes minimized this effect.
Fuzzy logic is a form of many-valued logic;
it deals with reasoning that is approximate rather than
fixed and exact. Compared to traditional binary sets
fuzzy logic variables may have a truth value that
ranges in degree between 0 and 1. Fuzzy logic has
been extended to handle the concept of partial truth,
where the truth value may range between completely
true and completely false. Furthermore, when
linguistic variables are used, these degrees may be
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managed by specific functions. Irrationality can be
described in terms of what is known as the
fuzzjective. Fuzzy Logic Control Technique has been
a good replacement for conventional control
Techniques. Many researchers have suggested that
these controllers have the potential for robust control
in the face of system parameter and load
uncertainties. It is realized that fuzzy logic control
can perform very effectively when the operating
conditions change rapidly. These features make up
very attractive for power system applications since
power system is a highly non-linear and chaotic
system.
Fig. 1. Diagram of a single-link flexible arm.
II. MODEL DESCRIPTION
A. Flexible-Beam Dynamics
The flexible slewing beam studied in this
paper is considered to be a Euler–Bernoulli beam
whose behavior is described by a PDE. Its dynamics
involves infinite vibration modes. As the frequency
of those modes increases, its amplitude decreases.
This means that reduced models can be used, where
only the low frequencies, usually more significant,
are considered. In order to reduce the model, several
approaches were proposed: 1) distributed parameters
model where the infinite dimension is truncated to a
finite number of vibration modes; and 2) lumped
parameters models where a spatial discretization
leads to a finite-dimensional model. In this sense, the
spatial discretization can be done by both a FEM and
a lumped-mass model.
Fig. 2. Solid model design of flexible joint arm
A single-link flexible manipulator with tip
mass is modeled, as developed in, that can rotate
about the Z-axis perpendicular to the paper, as shown
in Fig. 1. The axial deformation and the gravitational
effect are neglected, because the mass of the flexible
beam is floating over an air table which allows us to
cancel the gravitational effect and the friction with
the surface of the table. Since structural damping
always increases the stability margin of the system, a
design without considering damping may provide a
valid but conservative result.
The real structure studied in this paper is
made of carbon fiber, with high mechanical
resistance and very small density. We study it under
the hypothesis of small deformations with all its mass
concentrated at the tip position because the mass of
the load is bigger than that of the bar, then the mass
of the beam can be neglected. In other words, the
flexible beam vibrates with the fundamental mode;
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therefore, the rest of the modes are very far from the
first one and they can be neglected. Thus, we only
consider one mode of vibration. The main
characteristic of this model is that the influence of the
load changes can be modeled in a very easy manner,
thus adaptive controller can be easily applied.
Based on these considerations, we propose the
following model for the flexible beam:
̈ = ( − ) (1)
where is the unknown mass at the tip position.
	and 	 = (3 / )		are the length of the flexible arm
and the stiffness of the bar, respectively, assumed to
be perfectly known. The stiffness depends on the
flexural rigidity and on the length of the bar .
is the angular position of the motor gear. and
are the unmeasured angular position and angular
acceleration of the tip, respectively.
Fig.3. compensation of coupling torque in a hub
B. DC-Motor Dynamics
A common electromechanical actuator, in many
control systems, is constituted by the dc motor. The
dc motor used is supplied by a servo amplifier with a
current inner loop control. We can write the dynamic
equation of the system by using Newton’s second
law.
= ̈ + ̇ + ̇ , + 	
(2)
The dynamics of the complete system,
actuated by a dc motor, is given by the following
simplified model:
̈ = ( − ) (3)
= ̈ + ̇ + + (4)
= ( − ) (5)
Equation (3) represents the dynamics of the
flexible beam;(4) expresses the dynamics of the dc
motor; and (5) stands for the coupling torque
measured in the hub and produced by the translation
of the flexible beam, which is directly proportional to
the stiffness of the beam and the difference between
the angles of the motor and the tip position,
respectively.
( ) =
( )
( )
= (6)
Where = ( ) is the unknown natural frequency
of the bar due to the lack of precise knowledge of	 .
The coupling torque can be canceled in the motor by
means of a compensation term. In this case, the
voltage applied to the motor is of the form;
= +
.
(7)
Where is the voltage applied before the
compensation term.
The system in (4) is then given by
= ̈ + ̇ + (8)
The controller to be designed will be robust with
respect to the unknown piecewise constant torque
disturbances affecting the motor dynamics . Then,
the perturbation-free system to be considered is the
following:
= ̈ + ̇ (9)
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where 	 = 	 / . To simplify the developments, let
	 = 	 / and	 	 = 	 / . The dc-motor transfer
function is then written as
( ) =
( )
( )
=
( )
. (10)
Fig. 3 shows the compensation scheme of
the coupling torque measured in the hub.
The regulation of the load position ( ) to
track a given smooth reference trajectory ∗
( ) is
desired. For the synthesis of the feedback-control
law, we are using only the measured motor position
	and the measured coupling torque . One of the
prevailing restrictions throughout our treatment of the
problem is our desire of not to measure, or compute
on the basis samplings, angular velocities of the
motor shaft or of the load.
The parameterization of 	in terms of	 is
given, in reduction-gear terms, by
= ̈ + = ̈ + (11)
System (11) is a second-order system in
which to regulate the tip position of the flexible bar
towards a given smooth reference trajectory,
∗
( ) is desired, with acting as an auxiliary
control input. Clearly, if there exists an auxiliary
open loop control input ∗
( )that ideally achieves
the tracking of ∗
( )for suitable initial conditions, it
satisfies then the second order dynamics, in
reduction-gear terms.
∗
( ) = ̈ ∗
( ) + ∗
( ) (12)
Subtracting (12) from (11), an expression in
terms of the angular tracking errors is obtained
̈ = ( − ) (13)
Where = − ∗
( ),
= − ∗
( ). Suppose for a moment, that we are
able to measure the angular-position tracking error
, then the outer loop feedback incremental
controller could be proposed to be the following PID
controller:
= + − ̇ − − ∫ ( )
(13)
In such a case, the closed-loop tracking error
evolves, governed by
( )
+ ̈ + ̇ + = 0 (14)
The design parameters { 2, 1, 0}	are then
chosen so as to render the closed-loop characteristic
polynomial into a Hurwitz polynomial with desirable
roots.
III. INNER LOOP
CONTROLLER
The angular position	 , generated as an
auxiliary control input in the previous controller
design step, is now regarded as a reference trajectory
for the motor controller. We denote this reference
trajectory by ∗
. The design of the controller to be
robust with respect to this torque disturbance is
desired.
The following feedback controller is
proposed:
= 	 ̂̇ + − 	 ̂̇ − −
∫ ( ) ( ) − ∫ ∫ ( ) ( ) ( )
(15)
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The following integral reconstructor for the angular-
velocity error signal 	 ̂̇ 	is obtained:
	 ̂̇ = ∫ ( ) ( ) −	 (16)
Replacing 	 ̂̇ in (25) into (24) and, after
some rearrangements, the feedback control law is
obtained
( − ∗
) = ( )
( ∗
− ) (17)
The open-loop control ∗( ) that ideally achieves the
open-loop tacking of the inner loop is given by
∗( ) = ̈ ∗
( ) + ̇ ∗
( ) (18)
The inner loop system in Fig. 4 is
exponentially stable. We can choose to place all the
closed-loop poles in a desired location of the left half
of the complex plane to design the
parameters	{ , , , }. As done with the outer
loop, all poles can be located at the same real value,
and , , , can be uniquely obtained by
equalizing the terms of the two following
polynomials:
( + ) = + 4 + 6 + 4 + = 0
(19)
+ ( + ) + ( + ) + +
= 0 (20)
Where the parameter represents the common
location of all the closed-loops poles, this being
strictly positive.
IV. FUZZY-PID CONTROLLER
Here, A classical FLS is represented as in
Fig-4. As shown, rules play a central role in the FLS
framework. Rules can be provided by experts or can
be extracted from numerical data. The IF-part of a
rule is an antecedent while the THEN-part of a rule is
its consequent. Fuzzy sets are associated with terms
that appear both in the antecedent and in the
consequent, while Membership Functions (MFs) are
used to describe these fuzzy sets.
Fig.4., structure of the fuzzy logic controller
Table:1
Control rules of the fuzzy controller
Input2
Input1 N Z P
N P N N
Z N P P
P N N N
Fuzzification: Translates inputs (real values)
to fuzzy values. Inference System: Applies a fuzzy
reasoning mechanism to obtain a fuzzy output. Type
Defuzzificator/Reductor: The defuzzificator
transduces one output to precise values; the type
redactor transforms a fuzzy set into a Type-1 fuzzy
set.
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Knowledge Base: Contains a set of fuzzy
rules, and a membership functions set known as the
database. The two normalized input variables, input1
and input2, are first fuzzified by two interval t fuzzy
sets i.e., ‘positive’ and ‘negative’ represented by
( 1) and ( 2) respectively.
BLOCK DIAGRAM OF THE SINGLE LINK FLEXIBLE MANIPULATOR USING FUZZY PID
CONTROL
Fig.5., Block Diagram Of The Single Link Flexible Manipulator Using Fuzzy PID Control
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V. SIMULATION & RESULTS
The major problems associated with the
control of flexible structures arise from the structure
is a distributed parameter system with many modes,
and there are likely to be many actuators.
There are three types of controllers used to
control the system which are simulated and compared
for better results.
They are;
1. Integral controller
2. Conventional PID controller
3. Fuzzy PID controller
The simulation results of the above controllers and
given bellow
I) Using Integral Controller
Fig.6, the simulation result of integral controller
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II) Using Conventional PID Controller
Fig.7, the simulation result of the conventional pid controller
III) Using Fuzzy PID Controller
Fig.8, the simulation result of the fuzzy PID controller
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IV) The Combined Figure Of The Output Simulated
Fig.9. The Combined Figure Of The Output Simulated
Therefore, the above results prove that the
system controlled by the fuzzy PID controller has
better n accurate results when compared to other
controllers
VI. CONCLUSION:
Here, fuzzy PID controller is designed to control
the single link flexible manipulator . The proposed
controller is being designed based on the
conventional PID controller. The proposed Fuzzy
PID controller is tested for different motor dynamics.
Simulation results show the efficiency of the
proposed controller, as it is being compared with the
conventional integral and PID controller.
VII. REFERENCES:
[1] S. K. Dwivedy and P. Eberhard, “Dynamic
analysis of flexible manipulators, a literature review,”
Mech.Mach. Theory, vol. 41, no. 7, pp. 749–777, Jul.
2006.
[2] R. H. Canon and E. Schmitz, “Initial experiments
on the end-point control of a flexible robot,” Int. J.
Rob. Res., vol. 3, no. 3, pp. 62–75, 1984.
[3] Y. P. Chen and H. T. Hsu, “Regulation and
vibration control of an FEM based single-link
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flexible arm using sliding-mode theory,” J. Vib.
Control, vol. 7, no. 5, pp. 741–752, 2001.
[4] Z. Su and K. A. Khorasani, “A neural-network-
based controller for a single-link flexible manipulator
using the inverse dynamics approach,” IEEE Trans.
Ind. Electron., vol. 48, no. 6, pp. 1074–1086,
Dec.2001.
[5] V. G. Moudgal, W. A. Kwong, K. M. Passino,
and S. Yurkovich, “Fuzzy learning control for a
flexible-link robot,” IEEE Trans. Fuzzy Syst., vol. 3,
no. 2, pp. 199–210, May 1995.
[6] J. Becedas, J. Trapero, H. Sira-Ramírez, and
V.Feliu, “Fast identification method to control a
flexible manipulator with parameter uncertainties,” in
Proc. ICRA, 2007, pp. 3445–3450.
[7] V. Feliu and F. Ramos, “Strain gauge based
control of single link flexible very light weight robots
robust to payload changes,” Mechatronics, vol. 15,
no. 5, pp. 547–571, Jun. 2005.
[8] H. Olsson, H. Amström, and C. C. de Wit,
“Friction models and friction compensation,” Eur. J.
Control, vol. 4, no. 3, pp. 176–195, 1998.
[9] S. Cicero, V. Santos, and B. de Carvahlo, “Active
control to flexible manipulators,” IEEE/ASME Trans.
Mechatronics, vol. 11, no. 1, pp. 75–83, Feb. 2006.
[10] E. Bayo, “A finite-element approach to control
the end-point motion of a single-link flexible robot,”
J. Robot. Syst., vol. 4, no. 1, pp. 63–75, Feb. 1987.
[11] V. Feliu, K. S. Rattan, and H. Brown, “Modeling
and control of single-link flexible arms with lumped
masses,” J. Dyn. Syst. Meas. Control, vol. 114, no. 7,
pp. 59–69, 1992.
[12] W. Liu and Z. Hou, “A new approach to
suppress spillover instability in structural vibration,”
Struct. Control Health Monitoring, vol. 11, no. 1, pp.
37–53, Jan.–Mar. 2004.
[13] R. D. Begamudre, Electro-Mechanical Energy
ConversionWith Dynamics of Machines. New York:
Wiley, 1998.
[14] H. Sira-Ramírez and S. Agrawal, Differentially
Flat Systems. NewYork: Marcel Dekker, 2004.
[15] P. C. Young, “Parameter estimation for
continuous-time models—A survey,” Automatica,
vol. 17, no. 1, pp. 23–29, Jan. 1981.
[16] H. Unbehauen and G. P. Rao, “Continuous-time
approaches to system identification—A survey,”
Automatica, vol. 26, no. 1, pp. 23–35, Jan. 1990.
[17] N. Sinha and G. Rao, Identification of
Continuous-Time Systems. Dordrecht, The
Netherlands: Kluwer, 1991.
[18] H. Unbehauen and G. Rao, Identification of
Continuous Systems. Amsterdam, The Netherlands:
North-Holland, 1987.
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Iaetsd design of a robust fuzzy logic controller for a single-link flexible manipulator

  • 1. DESIGN OF A ROBUST FUZZY LOGIC CONTROLLER FOR A SINGLE- LINK FLEXIBLE MANIPULATOR K.RINI SOWHARIKA Dr.R.VIJAYA SANTHI PG Scholar Asst.Professor Department Electrical Engineering, Andhra University, Visakhapatnam, Andhra Pradesh. Abstract: In this paper, a single link flexible manipulator is designed and controlled using a fuzzy-PID controller. The controller is employed to control an uncertain Flexible Robotic Arm and its internal parameters in the motor dynamics. In order to verify this method, proposed controller is being tested against the conventional Integral and PID controller. The simulation results show the robustness of the proposed Fuzzy PID controller under motor dynamics. I. INTRODUCTION FLEXIBLE arm manipulators span a wide range of applications: space robots, nuclear maintenance, microsurgery, collision control, contouring control, pattern recognition, and many others. The system, described by partial differential equations (PDEs), is a distributed-parameter system of infinite dimensions. Its non minimum phase behavior makes it difficult to achieve high-level performance. Control techniques such as linear control, optimal control, adaptive control, sliding-mode control, neural networks, or fuzzy logic deal with the control of flexible manipulators and the modeling based on a truncated (finite dimensional) model obtained from either the finite-element method (FEM) or assumed modes method. These methods require several sensors to be used in order to obtain an accurate trajectory tracking, and many of them also require the knowledge of all the system parameters to design properly the controller. Here a new method is considered to cancel the vibration of the flexible beam which gathers an online identification technique with a control scheme in a suited manner, with the only measures of both the motor angle obtained from an encoder and the coupling torque obtained from a pair of strain gauges as done in the work in. In that paper, the nonlinearities effect in the motor dynamics, such as the Coulomb friction torque. Robust control schemes minimized this effect. Fuzzy logic is a form of many-valued logic; it deals with reasoning that is approximate rather than fixed and exact. Compared to traditional binary sets fuzzy logic variables may have a truth value that ranges in degree between 0 and 1. Fuzzy logic has been extended to handle the concept of partial truth, where the truth value may range between completely true and completely false. Furthermore, when linguistic variables are used, these degrees may be 227 INTERNATIONAL CONFERENCE ON CURRENT INNOVATIONS IN ENGINEERING AND TECHNOLOGY INTERNATIONAL ASSOCIATION OF ENGINEERING & TECHNOLOGY FOR SKILL DEVELOPMENT ISBN: 378 - 26 - 138420 - 5 www.iaetsd.in
  • 2. managed by specific functions. Irrationality can be described in terms of what is known as the fuzzjective. Fuzzy Logic Control Technique has been a good replacement for conventional control Techniques. Many researchers have suggested that these controllers have the potential for robust control in the face of system parameter and load uncertainties. It is realized that fuzzy logic control can perform very effectively when the operating conditions change rapidly. These features make up very attractive for power system applications since power system is a highly non-linear and chaotic system. Fig. 1. Diagram of a single-link flexible arm. II. MODEL DESCRIPTION A. Flexible-Beam Dynamics The flexible slewing beam studied in this paper is considered to be a Euler–Bernoulli beam whose behavior is described by a PDE. Its dynamics involves infinite vibration modes. As the frequency of those modes increases, its amplitude decreases. This means that reduced models can be used, where only the low frequencies, usually more significant, are considered. In order to reduce the model, several approaches were proposed: 1) distributed parameters model where the infinite dimension is truncated to a finite number of vibration modes; and 2) lumped parameters models where a spatial discretization leads to a finite-dimensional model. In this sense, the spatial discretization can be done by both a FEM and a lumped-mass model. Fig. 2. Solid model design of flexible joint arm A single-link flexible manipulator with tip mass is modeled, as developed in, that can rotate about the Z-axis perpendicular to the paper, as shown in Fig. 1. The axial deformation and the gravitational effect are neglected, because the mass of the flexible beam is floating over an air table which allows us to cancel the gravitational effect and the friction with the surface of the table. Since structural damping always increases the stability margin of the system, a design without considering damping may provide a valid but conservative result. The real structure studied in this paper is made of carbon fiber, with high mechanical resistance and very small density. We study it under the hypothesis of small deformations with all its mass concentrated at the tip position because the mass of the load is bigger than that of the bar, then the mass of the beam can be neglected. In other words, the flexible beam vibrates with the fundamental mode; 228 INTERNATIONAL CONFERENCE ON CURRENT INNOVATIONS IN ENGINEERING AND TECHNOLOGY INTERNATIONAL ASSOCIATION OF ENGINEERING & TECHNOLOGY FOR SKILL DEVELOPMENT ISBN: 378 - 26 - 138420 - 5 www.iaetsd.in
  • 3. therefore, the rest of the modes are very far from the first one and they can be neglected. Thus, we only consider one mode of vibration. The main characteristic of this model is that the influence of the load changes can be modeled in a very easy manner, thus adaptive controller can be easily applied. Based on these considerations, we propose the following model for the flexible beam: ̈ = ( − ) (1) where is the unknown mass at the tip position. and = (3 / ) are the length of the flexible arm and the stiffness of the bar, respectively, assumed to be perfectly known. The stiffness depends on the flexural rigidity and on the length of the bar . is the angular position of the motor gear. and are the unmeasured angular position and angular acceleration of the tip, respectively. Fig.3. compensation of coupling torque in a hub B. DC-Motor Dynamics A common electromechanical actuator, in many control systems, is constituted by the dc motor. The dc motor used is supplied by a servo amplifier with a current inner loop control. We can write the dynamic equation of the system by using Newton’s second law. = ̈ + ̇ + ̇ , + (2) The dynamics of the complete system, actuated by a dc motor, is given by the following simplified model: ̈ = ( − ) (3) = ̈ + ̇ + + (4) = ( − ) (5) Equation (3) represents the dynamics of the flexible beam;(4) expresses the dynamics of the dc motor; and (5) stands for the coupling torque measured in the hub and produced by the translation of the flexible beam, which is directly proportional to the stiffness of the beam and the difference between the angles of the motor and the tip position, respectively. ( ) = ( ) ( ) = (6) Where = ( ) is the unknown natural frequency of the bar due to the lack of precise knowledge of . The coupling torque can be canceled in the motor by means of a compensation term. In this case, the voltage applied to the motor is of the form; = + . (7) Where is the voltage applied before the compensation term. The system in (4) is then given by = ̈ + ̇ + (8) The controller to be designed will be robust with respect to the unknown piecewise constant torque disturbances affecting the motor dynamics . Then, the perturbation-free system to be considered is the following: = ̈ + ̇ (9) 229 INTERNATIONAL CONFERENCE ON CURRENT INNOVATIONS IN ENGINEERING AND TECHNOLOGY INTERNATIONAL ASSOCIATION OF ENGINEERING & TECHNOLOGY FOR SKILL DEVELOPMENT ISBN: 378 - 26 - 138420 - 5 www.iaetsd.in
  • 4. where = / . To simplify the developments, let = / and = / . The dc-motor transfer function is then written as ( ) = ( ) ( ) = ( ) . (10) Fig. 3 shows the compensation scheme of the coupling torque measured in the hub. The regulation of the load position ( ) to track a given smooth reference trajectory ∗ ( ) is desired. For the synthesis of the feedback-control law, we are using only the measured motor position and the measured coupling torque . One of the prevailing restrictions throughout our treatment of the problem is our desire of not to measure, or compute on the basis samplings, angular velocities of the motor shaft or of the load. The parameterization of in terms of is given, in reduction-gear terms, by = ̈ + = ̈ + (11) System (11) is a second-order system in which to regulate the tip position of the flexible bar towards a given smooth reference trajectory, ∗ ( ) is desired, with acting as an auxiliary control input. Clearly, if there exists an auxiliary open loop control input ∗ ( )that ideally achieves the tracking of ∗ ( )for suitable initial conditions, it satisfies then the second order dynamics, in reduction-gear terms. ∗ ( ) = ̈ ∗ ( ) + ∗ ( ) (12) Subtracting (12) from (11), an expression in terms of the angular tracking errors is obtained ̈ = ( − ) (13) Where = − ∗ ( ), = − ∗ ( ). Suppose for a moment, that we are able to measure the angular-position tracking error , then the outer loop feedback incremental controller could be proposed to be the following PID controller: = + − ̇ − − ∫ ( ) (13) In such a case, the closed-loop tracking error evolves, governed by ( ) + ̈ + ̇ + = 0 (14) The design parameters { 2, 1, 0} are then chosen so as to render the closed-loop characteristic polynomial into a Hurwitz polynomial with desirable roots. III. INNER LOOP CONTROLLER The angular position , generated as an auxiliary control input in the previous controller design step, is now regarded as a reference trajectory for the motor controller. We denote this reference trajectory by ∗ . The design of the controller to be robust with respect to this torque disturbance is desired. The following feedback controller is proposed: = ̂̇ + − ̂̇ − − ∫ ( ) ( ) − ∫ ∫ ( ) ( ) ( ) (15) 230 INTERNATIONAL CONFERENCE ON CURRENT INNOVATIONS IN ENGINEERING AND TECHNOLOGY INTERNATIONAL ASSOCIATION OF ENGINEERING & TECHNOLOGY FOR SKILL DEVELOPMENT ISBN: 378 - 26 - 138420 - 5 www.iaetsd.in
  • 5. The following integral reconstructor for the angular- velocity error signal ̂̇ is obtained: ̂̇ = ∫ ( ) ( ) − (16) Replacing ̂̇ in (25) into (24) and, after some rearrangements, the feedback control law is obtained ( − ∗ ) = ( ) ( ∗ − ) (17) The open-loop control ∗( ) that ideally achieves the open-loop tacking of the inner loop is given by ∗( ) = ̈ ∗ ( ) + ̇ ∗ ( ) (18) The inner loop system in Fig. 4 is exponentially stable. We can choose to place all the closed-loop poles in a desired location of the left half of the complex plane to design the parameters { , , , }. As done with the outer loop, all poles can be located at the same real value, and , , , can be uniquely obtained by equalizing the terms of the two following polynomials: ( + ) = + 4 + 6 + 4 + = 0 (19) + ( + ) + ( + ) + + = 0 (20) Where the parameter represents the common location of all the closed-loops poles, this being strictly positive. IV. FUZZY-PID CONTROLLER Here, A classical FLS is represented as in Fig-4. As shown, rules play a central role in the FLS framework. Rules can be provided by experts or can be extracted from numerical data. The IF-part of a rule is an antecedent while the THEN-part of a rule is its consequent. Fuzzy sets are associated with terms that appear both in the antecedent and in the consequent, while Membership Functions (MFs) are used to describe these fuzzy sets. Fig.4., structure of the fuzzy logic controller Table:1 Control rules of the fuzzy controller Input2 Input1 N Z P N P N N Z N P P P N N N Fuzzification: Translates inputs (real values) to fuzzy values. Inference System: Applies a fuzzy reasoning mechanism to obtain a fuzzy output. Type Defuzzificator/Reductor: The defuzzificator transduces one output to precise values; the type redactor transforms a fuzzy set into a Type-1 fuzzy set. 231 INTERNATIONAL CONFERENCE ON CURRENT INNOVATIONS IN ENGINEERING AND TECHNOLOGY INTERNATIONAL ASSOCIATION OF ENGINEERING & TECHNOLOGY FOR SKILL DEVELOPMENT ISBN: 378 - 26 - 138420 - 5 www.iaetsd.in
  • 6. Knowledge Base: Contains a set of fuzzy rules, and a membership functions set known as the database. The two normalized input variables, input1 and input2, are first fuzzified by two interval t fuzzy sets i.e., ‘positive’ and ‘negative’ represented by ( 1) and ( 2) respectively. BLOCK DIAGRAM OF THE SINGLE LINK FLEXIBLE MANIPULATOR USING FUZZY PID CONTROL Fig.5., Block Diagram Of The Single Link Flexible Manipulator Using Fuzzy PID Control 232 INTERNATIONAL CONFERENCE ON CURRENT INNOVATIONS IN ENGINEERING AND TECHNOLOGY INTERNATIONAL ASSOCIATION OF ENGINEERING & TECHNOLOGY FOR SKILL DEVELOPMENT ISBN: 378 - 26 - 138420 - 5 www.iaetsd.in
  • 7. V. SIMULATION & RESULTS The major problems associated with the control of flexible structures arise from the structure is a distributed parameter system with many modes, and there are likely to be many actuators. There are three types of controllers used to control the system which are simulated and compared for better results. They are; 1. Integral controller 2. Conventional PID controller 3. Fuzzy PID controller The simulation results of the above controllers and given bellow I) Using Integral Controller Fig.6, the simulation result of integral controller 233 INTERNATIONAL CONFERENCE ON CURRENT INNOVATIONS IN ENGINEERING AND TECHNOLOGY INTERNATIONAL ASSOCIATION OF ENGINEERING & TECHNOLOGY FOR SKILL DEVELOPMENT ISBN: 378 - 26 - 138420 - 5 www.iaetsd.in
  • 8. II) Using Conventional PID Controller Fig.7, the simulation result of the conventional pid controller III) Using Fuzzy PID Controller Fig.8, the simulation result of the fuzzy PID controller 234 INTERNATIONAL CONFERENCE ON CURRENT INNOVATIONS IN ENGINEERING AND TECHNOLOGY INTERNATIONAL ASSOCIATION OF ENGINEERING & TECHNOLOGY FOR SKILL DEVELOPMENT ISBN: 378 - 26 - 138420 - 5 www.iaetsd.in
  • 9. IV) The Combined Figure Of The Output Simulated Fig.9. The Combined Figure Of The Output Simulated Therefore, the above results prove that the system controlled by the fuzzy PID controller has better n accurate results when compared to other controllers VI. CONCLUSION: Here, fuzzy PID controller is designed to control the single link flexible manipulator . The proposed controller is being designed based on the conventional PID controller. The proposed Fuzzy PID controller is tested for different motor dynamics. Simulation results show the efficiency of the proposed controller, as it is being compared with the conventional integral and PID controller. VII. REFERENCES: [1] S. K. Dwivedy and P. Eberhard, “Dynamic analysis of flexible manipulators, a literature review,” Mech.Mach. Theory, vol. 41, no. 7, pp. 749–777, Jul. 2006. [2] R. H. Canon and E. Schmitz, “Initial experiments on the end-point control of a flexible robot,” Int. J. Rob. Res., vol. 3, no. 3, pp. 62–75, 1984. [3] Y. P. Chen and H. T. Hsu, “Regulation and vibration control of an FEM based single-link 235 INTERNATIONAL CONFERENCE ON CURRENT INNOVATIONS IN ENGINEERING AND TECHNOLOGY INTERNATIONAL ASSOCIATION OF ENGINEERING & TECHNOLOGY FOR SKILL DEVELOPMENT ISBN: 378 - 26 - 138420 - 5 www.iaetsd.in
  • 10. flexible arm using sliding-mode theory,” J. Vib. Control, vol. 7, no. 5, pp. 741–752, 2001. [4] Z. Su and K. A. Khorasani, “A neural-network- based controller for a single-link flexible manipulator using the inverse dynamics approach,” IEEE Trans. Ind. Electron., vol. 48, no. 6, pp. 1074–1086, Dec.2001. [5] V. G. Moudgal, W. A. Kwong, K. M. Passino, and S. Yurkovich, “Fuzzy learning control for a flexible-link robot,” IEEE Trans. Fuzzy Syst., vol. 3, no. 2, pp. 199–210, May 1995. [6] J. Becedas, J. Trapero, H. Sira-Ramírez, and V.Feliu, “Fast identification method to control a flexible manipulator with parameter uncertainties,” in Proc. ICRA, 2007, pp. 3445–3450. [7] V. Feliu and F. Ramos, “Strain gauge based control of single link flexible very light weight robots robust to payload changes,” Mechatronics, vol. 15, no. 5, pp. 547–571, Jun. 2005. [8] H. Olsson, H. Amström, and C. C. de Wit, “Friction models and friction compensation,” Eur. J. Control, vol. 4, no. 3, pp. 176–195, 1998. [9] S. Cicero, V. Santos, and B. de Carvahlo, “Active control to flexible manipulators,” IEEE/ASME Trans. Mechatronics, vol. 11, no. 1, pp. 75–83, Feb. 2006. [10] E. Bayo, “A finite-element approach to control the end-point motion of a single-link flexible robot,” J. Robot. Syst., vol. 4, no. 1, pp. 63–75, Feb. 1987. [11] V. Feliu, K. S. Rattan, and H. Brown, “Modeling and control of single-link flexible arms with lumped masses,” J. Dyn. Syst. Meas. Control, vol. 114, no. 7, pp. 59–69, 1992. [12] W. Liu and Z. Hou, “A new approach to suppress spillover instability in structural vibration,” Struct. Control Health Monitoring, vol. 11, no. 1, pp. 37–53, Jan.–Mar. 2004. [13] R. D. Begamudre, Electro-Mechanical Energy ConversionWith Dynamics of Machines. New York: Wiley, 1998. [14] H. Sira-Ramírez and S. Agrawal, Differentially Flat Systems. NewYork: Marcel Dekker, 2004. [15] P. C. Young, “Parameter estimation for continuous-time models—A survey,” Automatica, vol. 17, no. 1, pp. 23–29, Jan. 1981. [16] H. Unbehauen and G. P. Rao, “Continuous-time approaches to system identification—A survey,” Automatica, vol. 26, no. 1, pp. 23–35, Jan. 1990. [17] N. Sinha and G. Rao, Identification of Continuous-Time Systems. Dordrecht, The Netherlands: Kluwer, 1991. [18] H. Unbehauen and G. Rao, Identification of Continuous Systems. Amsterdam, The Netherlands: North-Holland, 1987. 236 INTERNATIONAL CONFERENCE ON CURRENT INNOVATIONS IN ENGINEERING AND TECHNOLOGY INTERNATIONAL ASSOCIATION OF ENGINEERING & TECHNOLOGY FOR SKILL DEVELOPMENT ISBN: 378 - 26 - 138420 - 5 www.iaetsd.in