master defense

58
Master Thesis Defense “Hardware-in-the-loop simulation of a servo cylinder test rig operating in a closed loop position control system under the effect of a servo loading cylinder” Submitted by Khaled Hossam Emam Under Supervision of Dr. Eng. Taher M. Salah El din Master Thesis Defense Faculty of Engineering and Material Science Mechatronics Department The German University in Cairo

Upload: khaled-emam

Post on 17-Feb-2017

181 views

Category:

Documents


3 download

TRANSCRIPT

Page 1: master defense

Master Thesis Defense

“Hardware-in-the-loop simulation of a servo cylinder test rig operating in a closed loop position control system

under the effect of a servo loading cylinder”

Submitted byKhaled Hossam Emam

Under Supervision ofDr. Eng. Taher M. Salah El din

Master Thesis Defense

Faculty of Engineering and Material Science Mechatronics Department

The German University in Cairo

Page 2: master defense

Master Thesis Defense

Khaled H. Emam Slide 2/58

Outline Introduction Mechanical Design Hydraulic Design Controller Design Data Acquisition Results Conclusion

Page 3: master defense

Master Thesis Defense

Khaled H. Emam Slide 3/58

Background and Motivation

Hydraulic drives are widely used in industry where high forces and heavy loading conditions should be manipulated.

In order to reach high dynamic response and high power to weight ratio, servo control techniques were applied to the hydraulic systems.

Due to the fact that electrohydraulic systems are complex non-linear system, a lot of research was dedicated to the are of control and response analysis.

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Page 4: master defense

Master Thesis Defense

Khaled H. Emam Slide 4/58

Thesis Objective Development and design of a test rig for electrohydraulic components and

systems to be used for research applications and practical courses for students.

Scope of the Thesis Implementing a Hardware In the Loop (HIL) simulator for position control of

a servo cylinder under the effect of loading servo cylinder.

This study is mainly based on “Salah el-din, T. (2010). "Enhancement of performance of an electrohydraulic servo system for mold oscillation control in continuous casting machines". Ph.D thesis. Cairo University, Faculty of Engineering, Egypt.”

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Page 5: master defense

Master Thesis Defense

Khaled H. Emam Slide 5/58

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Page 6: master defense

Master Thesis Defense

Khaled H. Emam Slide 6/58

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Photograph of Servo Cylinder Test Rig Institute of Fluid Power (TU Dresden)

Page 7: master defense

Master Thesis Defense

Khaled H. Emam Slide 7/58

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Photograph of Servo Cylinder Test Rig at EZDK Steel Plant

Page 8: master defense

Master Thesis Defense

Khaled H. Emam Slide 8/58

Working Plan Study the mechanical and hydraulic components for test rig assembly.

Closed loop Control analysis for both position controlled servo cylinder and force controlled loading servo cylinder, i.e. implementing a system model using Matlab/Simulink.

Considering the electrical and electronic interface between the hardware and software planes.

Calculation of controller parameters using classic control techniques and manual tuning on the test rig at EZDK steel plant.

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Page 9: master defense

Master Thesis Defense

Khaled H. Emam Slide 9/58

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Page 10: master defense

Master Thesis Defense

Khaled H. Emam Slide 10/58

1 Operating Cylinder2 Base Block3 Cross Block- operating side4 Operating Rod5 Tension Rod6 Oscillating Block7 Load Cell Adaptor 8 Load Cell9 Load Cylinder Rod

10 Loading Cylinder11 Cross Block- loading side

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Page 11: master defense

Master Thesis Defense

Khaled H. Emam Slide 11/58

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Parameter Loading Cylinder

Piston diameter[mm] 100

Piston rod diameter [ mm] 60

Stroke [mm] 100

Piston cross section area [m2] 0.005

Piston chamber volume at piston mid-stroke [m3] 2.5x10-4

Piston mass [kg] 18.5

Maximum operating pressure [MPa] 12

Coefficient of viscous friction [Ns/m] 4255

Parameters of Loading Cylinder

Page 12: master defense

Master Thesis Defense

Khaled H. Emam Slide 12/58

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Parameters of Operating Cylinder

Parameter Operating Cylinder

Piston diameter[mm] 160

Piston rod diameter [ mm] 100

Stroke [mm] 100

Piston cross section area [m2] 0.0122

Piston chamber volume at piston mid-stroke [m3] 6x10-4

Piston mass [kg] 58

Maximum operating pressure [MPa] 7

Coefficient of viscous friction [Ns/m] 12000

Page 13: master defense

Master Thesis Defense

Khaled H. Emam Slide 13/58

Three Stage Servo Valve Bandwidth of the three stage servo valve

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Operating Servo System – Servo Valve

Page 14: master defense

Master Thesis Defense

Khaled H. Emam Slide 14/58

Two Stage Servo Valve Bandwidth of the two stage servo valve

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Loading Servo System – Servo Valve

Page 15: master defense

Master Thesis Defense

Khaled H. Emam Slide 15/58

Introduction Mechanical Design

Hydraulic Design

Controller Design Data Acquisition Results Conclusion

Torque Motor

Flapper Valve

Control Spool

Page 16: master defense

Master Thesis Defense

Khaled H. Emam Slide 16/58

Introduction Mechanical Design

Hydraulic Design

Controller Design Data Acquisition Results Conclusion

Detailed System Model

Page 17: master defense

Master Thesis Defense

Khaled H. Emam Slide 17/58

Introduction Mechanical Design

Hydraulic Design

Controller Design Data Acquisition Results Conclusion

Detailed System Model

Page 18: master defense

Master Thesis Defense

Khaled H. Emam Slide 18/58

Introduction Mechanical Design

Hydraulic Design

Controller Design Data Acquisition Results Conclusion

Detailed System Model

0 0.005 0.01 0.015 0.02 0.025 0.03-0.5

0

0.5

1

1.5

2

2.5

3 x 10-4

time (sec)

Spoo

l Dis

plac

emen

t (m

m)

linear valve modeldetailed valve model

Page 19: master defense

Master Thesis Defense

Khaled H. Emam

Introduction Mechanical Design

Hydraulic Design

Controller Design Data Acquisition Results Conclusion

y = Main spool displacement

= damping ratio of the spool,

= Natural frequency of the valve

=Displacement proportionality coefficient between the control current and valve spool

= Proportional gain

= servo cylinder reference position

= servo cylinder actual position

= Reference loading force

= Actual loading force

Linear System Model

��+2 ζ 𝑠𝜔0𝑣 ��+𝜔0𝑣2 𝑦=𝜔0𝑣

2𝐾 0𝑣 𝑖

The dynamic model of the valve spool can be approximated to a second order transfer function without serious loss of accuracy

𝑖=𝐾 𝑝𝑜𝑝𝑒𝑟𝑎𝑡𝑖𝑛𝑔∗(𝑥𝑟−𝑥𝑎)𝑖=𝐾 𝑝𝑙𝑜𝑎𝑑𝑖𝑛𝑔∗(𝐹 𝑟−𝐹 𝑎)

The controller used is a proportional controller to compensate for the time lag and amplitude shift between the reference and command values

Slide 19/58

Page 20: master defense

Master Thesis Defense

Khaled H. Emam

Linear System Model The non-linear flow rate load characteristic (QL = f(y,PL)) is a function in two

variables. Taylor expansion of the function is applied for each variable taking the working point at .

Flow rate gain : Load gain :

The linearization is calculated at the working points (=0 & =0)

QL. linearized=KQ y . 𝑦+K Qp . PL

Introduction Mechanical Design

Hydraulic Design

Controller Design Data Acquisition Results Conclusion

Slide 20/58

Page 21: master defense

Master Thesis Defense

Khaled H. Emam

Linear System Model

The flow continuity equation for the cylinder chamber is given by:

𝑃 𝐿=𝑃 𝐴− 𝑃𝐵=2𝐸𝑉𝐶

¿

The piston equation of motion is as follows

where d is the Viscous Friction Coefficient

𝑚 x+d ��=𝑃𝐿 𝐴𝑐−𝐹 𝑙𝑜𝑎𝑑

where GLint is the Coefficient of internal leakage

is the cylinder cross-sectional area

Introduction Mechanical Design

Hydraulic Design

Controller Design Data Acquisition Results Conclusion

Slide 21/58

Page 22: master defense

Master Thesis Defense

Khaled H. Emam

Linear System Model

Hydraulic transfer function: Mechanical transfer function:

Introduction Mechanical Design

Hydraulic Design

Controller Design Data Acquisition Results Conclusion

Slide 22/58

Page 23: master defense

Master Thesis Defense

Khaled H. Emam

Linear System Model

𝐾𝑀=𝐴𝑑 ,𝑇𝑀=

𝑚d 1/𝐾 𝐹𝐵

𝐺𝑀 (𝑠 )= ��

𝑃𝐿− 𝐹𝐴

=𝐾𝑀

1+𝑠 .𝑇𝑀𝐺𝐻 (𝑠 )=𝑃 𝐿

KQ y −𝐴 . ��=𝐾𝐻

1+𝑠 .𝑇𝐻

𝐾𝐻=1

KQp+G∮ ¿ ,𝑇𝐻=𝑉

2 .𝐸 . 1KQ p+G∮ ¿¿

¿

Introduction Mechanical Design

Hydraulic Design

Controller Design Data Acquisition Results Conclusion

Slide 23/58

Page 24: master defense

Master Thesis Defense

Khaled H. Emam Slide 24/58

Introduction Mechanical Design

Hydraulic Design

Controller Design Data Acquisition Results Conclusion

Linear System Model

0 0.2 0.4 0.6 0.8 1-4

-3

-2

-1

0

1

2

3

4 x 10-3

time (sec)

Hydraulic Mould Oscillator

Pist

on D

ispl

acem

ent (

m)

linear valve modeldetailed valve model

• The Hydraulic Mold Oscillator is used as a model to validate results.

• Comparison between detailed and linear models shows convergence between results

Page 25: master defense

Master Thesis Defense

Khaled H. Emam

Linear System Model

Introduction Mechanical Design

Hydraulic Design

Controller Design Data Acquisition Results Conclusion

Slide 25/58

Forster, I. (1984). Electro-hydraulic Load Simulator. o+p Oil hydraulics and pneumatics, 8 (28).

Page 26: master defense

Master Thesis Defense

Khaled H. Emam

Introduction Mechanical Design

Hydraulic Design

Controller Design Data Acquisition Results Conclusion

Linear System ModelOperating side open loop transfer function

∴𝑮𝒙 (𝒔 )=𝐾 𝑣 .𝜔𝑜𝑣2 𝐾𝐻 .𝐾𝑀 . (𝐴𝐶 )𝑜𝑝 (𝐾𝑝 )𝑜𝑝 (𝐾𝑄 ) 𝑦

𝑠 (𝑠2+2𝑠 ζ 𝑠𝜔𝑜𝑣+𝜔𝑜𝑣2 ) (1+𝑠 𝑇𝐻+𝑠𝑇𝑀+𝑠2𝑇𝐻𝑇𝑀+𝐾 𝐻 𝐾𝑀 (𝐴𝐶 )𝑜𝑝

2 )The open loop characteristic equation is as follows:

411411 +6526.23+36.8171 +0.0922355 +0.00010812 +2402.82 =0

Slide 26/58

Page 27: master defense

Master Thesis Defense

Khaled H. Emam

Introduction Mechanical Design

Hydraulic Design

Controller Design Data Acquisition Results Conclusion

Linear System ModelOperating side - controller design

-300

-250

-200

-150

-100

-50

Mag

nitu

de (d

B)

101 102 103 104-450

-360

-270

-180

-90

Phas

e (d

eg)

Bode DiagramGm = 88.4 dB (at 108 rad/s) , Pm = 90 deg (at 0.00584 rad/s)

Frequency (rad/s)

Proportional gain limit is calculated using Routh-Hurwitz criterion, bode plot and root locus method.

Slide 27/58

Page 28: master defense

Master Thesis Defense

Khaled H. Emam

Introduction Mechanical Design

Hydraulic Design

Controller Design Data Acquisition Results Conclusion

Linear System ModelOperating side - controller design

-1200 -1000 -800 -600 -400 -200 0 200 400 600-1000

-500

0

500

1000Root Locus

Real Axis (seconds-1)

Imag

inar

y A

xis (

seco

nds-1

)

Slide 28/58

Page 29: master defense

Master Thesis Defense

Khaled H. Emam

Introduction Mechanical Design

Hydraulic Design

Controller Design Data Acquisition Results Conclusion

Linear System ModelOperating side - controller design

Proportional gain limit is calculated using Routh-Hurwitz criterion, bode plot and root locus

method.

This gain value shouldn’t exceed

PID tuning techniques were applied to optimize the gain value.

Slide 29/58

Page 30: master defense

Master Thesis Defense

Khaled H. Emam

Introduction Mechanical Design

Hydraulic Design

Controller Design Data Acquisition Results Conclusion

Linear System ModelLoading side open loop transfer function

𝐺𝐹 (𝑠)=𝑲 𝒑𝒍∗𝐾 𝑣 .𝜔𝑜𝑣2

𝑠2+2𝐷𝑣𝜔𝑜𝑣 𝑠+𝜔𝑜𝑣2 ∗𝐊𝐐𝐲∗( 𝐾 𝐻

1+𝑇𝐻 .𝑠 ∗𝐴𝑐𝑙)= 𝐾𝑣 .𝜔𝑜𝑣2 𝐴𝑐𝑙𝐾 𝐻𝐾 𝑝𝑙𝐾𝑄 𝑦

(1+𝑇𝐻 . 𝑠) (𝑠2+2𝑠𝐷𝑣𝜔𝑜𝑣+𝜔𝑜𝑣2 )

The characteristic equation of the open loop transfer function is as follows:

Slide 30/58

Page 31: master defense

Master Thesis Defense

Khaled H. Emam

Introduction Mechanical Design

Hydraulic Design

Controller Design Data Acquisition Results Conclusion

Linear System ModelLoading side - controller design

-300

-250

-200

-150

-100

-50

Mag

nitu

de (d

B)

101 102 103 104-450

-360

-270

-180

-90

Phas

e (d

eg)

Bode DiagramGm = 88.4 dB (at 108 rad/s) , Pm = 90 deg (at 0.00584 rad/s)

Frequency (rad/s)Slide 31/58

Page 32: master defense

Master Thesis Defense

Khaled H. Emam

Introduction Mechanical Design

Hydraulic Design

Controller Design Data Acquisition Results Conclusion

-5000 -4000 -3000 -2000 -1000 0 1000 2000-3000

-2000

-1000

0

1000

2000

3000Root Locus

Real Axis (seconds-1)

Imag

inar

y A

xis

(sec

onds-1

)

Linear System ModelLoading side - controller design

Slide 32/58

Page 33: master defense

Master Thesis Defense

Khaled H. Emam

Introduction Mechanical Design

Hydraulic Design

Controller Design Data Acquisition Results Conclusion

Linear System ModelLoading side - controller design

The range of gain values for loading servos system is shown to be less than

PID tuning techniques were applied to optimize the gain value.

Slide 33/58

Page 34: master defense

Master Thesis Defense

Khaled H. Emam

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Slide 34/58

Page 35: master defense

Master Thesis Defense

Khaled H. Emam

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

ADCH1 Not connected DACH1 Servovalve#1 Command Signal

ADCH2 Not connected DACH2 Not connected

ADCH3 Not connected DACH3 To DS-1104#2

ADCH 4 Not connected DACH4 To DS-1104#2

ADCH5 Position Sensor #1 WLH100 DACH5 Not connected

ADCH6 Servovalve#1 Feedback DACH6 Not connected

ADCH7 Not connected DACH7 Not connected

ADCH8 Not connected DACH8 Not connected

Slide 35/58

Page 36: master defense

Master Thesis Defense

Khaled H. Emam

ADCH1 From DS-1104#1 DACH1 Servovalve#3 Command

ADCH2 From DS-1104#1 DACH2 Not connected

ADCH3 Servovalve#3 Feedback Signal DACH3 Not connected

ADCH4 Not connected DACH4 Not connected

ADCH5 Pressure Transducer EDS300 DACH5 Not connected

ADCH6 Position Transducer#3 WLH100 DACH6 Not connected

ADCH7 Not connected DACH7 Not connected

ADCH8 Not connected DACH8 Not connected

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Slide 36/58

Page 37: master defense

Master Thesis Defense

Khaled H. Emam

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Parameters:• = 1• Amplitude=3.5mm• Freq. = 3Hz

Experiment 1:

0 0.5 1 1.5 2-0.4

-0.3

-0.2

-0.1

0

0.1

0.2

0.3

0.4

0.5

time (sec)

Spoo

l Dis

plac

emen

t (m

m)

Servo Valve Yactual

Servo Valve Yreference

Slide 37/58

Page 38: master defense

Master Thesis Defense

Khaled H. Emam

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Parameters:• = 1• Amplitude=3.5mm• Freq. = 3Hz

0 0.5 1 1.5 246

47

48

49

50

51

52

53

54

time (sec)

Pist

on D

ispl

acem

ent (

mm

)

Operating Cylinder Xactual

Operating Cylinder Xreference

Slide 38/58

Page 39: master defense

Master Thesis Defense

Khaled H. Emam

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Parameters:• = 25• Amplitude=3.5mm• Freq. = 3Hz

Experiment 2:

0 0.5 1 1.5 2-1

-0.5

0

0.5

1

1.5

time (sec)

Spoo

l Dis

plac

emen

t (m

m)

Servo Valve Yactual

Servo Valve Yreference

Slide 39/58

Page 40: master defense

Master Thesis Defense

Khaled H. Emam

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Parameters:• = 25• Amplitude=3.5mm• Freq. = 3Hz

0 0.5 1 1.5 246

47

48

49

50

51

52

53

54

time (sec)

Pist

on D

ispl

acem

ent (

mm

)

Operating Cylinder Xactual

Operating Cylinder Xreference

Slide 40/58

Page 41: master defense

Master Thesis Defense

Khaled H. Emam

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Parameters:• = 25• Amplitude=3.5mm• Frequency = 5Hz

Experiment 3:

0 0.5 1 1.5 2-1.5

-1

-0.5

0

0.5

1

1.5

2

2.5

time (sec)

Spoo

l Dis

plac

emen

t (m

m)

Servo Valve YactualServo Valve Yreference

Slide 41/58

Page 42: master defense

Master Thesis Defense

Khaled H. Emam

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Parameters:• = 25• Amplitude=3.5• Frequency = 5 rad/s

0 0.5 1 1.5 246

47

48

49

50

51

52

53

54

time (sec)

Pist

on D

ispl

acem

ent (

mm

)

Operating Cylinder Xactual

Operating Cylinder Xreference

Slide 42/58

Page 43: master defense

Master Thesis Defense

Khaled H. Emam

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Parameters:• = 25• Amplitude=5mm• Frequency = 5Hz

Experiment 4:

0 0.5 1 1.5 2-2

-1

0

1

2

3

4

time (sec)

Spoo

l Dis

plac

emen

t (m

m)

Servo Valve Yactual

Servo Valve Yreference

Slide 43/58

Page 44: master defense

Master Thesis Defense

Khaled H. Emam

Parameters:• = 25• Amplitude=5mm• Frequency = 5Hz

0 0.5 1 1.5 244

46

48

50

52

54

56

time (sec)

Pist

on D

ispl

acem

ent (

mm

)

Operating Cylinder XactualOperating Cylinder Xreference

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Slide 44/58

Page 45: master defense

Master Thesis Defense

Khaled H. Emam

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Parameters:• = 32• Amplitude= 3.5mm• Frequency = 5Hz

Experiment 5:

0 0.5 1 1.5 2-1.5

-1

-0.5

0

0.5

1

1.5

2

time (sec)

Spoo

l Dis

plac

emen

t (m

m)

Servo Valve Yactual

Servo Valve Yreference

Slide 45/58

Page 46: master defense

Master Thesis Defense

Khaled H. Emam

Parameters:• = 32• Amplitude= 3.5mm• Frequency = 5Hz

0 0.5 1 1.5 246

47

48

49

50

51

52

53

54

time (sec)

Pist

on D

ispl

acem

ent (

mm

)

Operating Cylinder Xactual

Operating Cylinder Xreference

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Slide 46/58

Page 47: master defense

Master Thesis Defense

Khaled H. Emam

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Parameters:• = 45• Amplitude= 5mm• Frequency = 5Hz

Experiment 6:

0 0.1 0.2 0.3 0.4 0.5-2

-1

0

1

2

3

4

time (sec)

Spoo

l Dis

plac

emen

t (m

m)

Servo Valve Yactual

Servo Valve Yreference

Slide 47/58

Page 48: master defense

Master Thesis Defense

Khaled H. Emam

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Parameters:• = 45• Amplitude= 5mm• Frequency = 5Hz

0 0.1 0.2 0.3 0.4 0.544

46

48

50

52

54

56

time (sec)

Pist

on D

ispl

acem

ent (

mm

)

Operating Cylinder Xactual

Operating Cylinder Xreference

Slide 48/58

Page 49: master defense

Master Thesis Defense

Khaled H. Emam

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Parameters:• = 2.5• Force signal:

Amplitude= 45 kNFrequency = 0 Hz

0 0.005 0.01 0.015 0.0240

45

50

55

time (sec)

Forc

e (k

N)

Forceact

Forceref

Force control

Slide 49/58

Page 50: master defense

Master Thesis Defense

Khaled H. Emam Slide 50/40

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Parameters:• = 2.5• Force signal:

Amplitude= 45 kNFrequency = 0 Hz

Force control

0 0.005 0.01 0.015 0.02-0.07

-0.06

-0.05

-0.04

-0.03

-0.02

-0.01

0

time (sec)

Spoo

l Dis

plac

emen

t (m

m)

Servo Valve Yactual

Page 51: master defense

Master Thesis Defense

Khaled H. Emam

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Study case

Parameters:• Zero input signal• No load condition

Slide 51/58

Page 52: master defense

Master Thesis Defense

Khaled H. Emam

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Study case

0 0.2 0.4 0.6 0.8 1-2

-1.5

-1

-0.5

0

0.5

1

1.5

2

time (sec)

Spoo

l Dis

plac

emen

t (m

m)

Servo Valve Yactual

Servo Valve Yreference

Parameters:• = 32• Amplitude= 3.5mm• Frequency = 5Hz

Slide 52/58

Page 53: master defense

Master Thesis Defense

Khaled H. Emam

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

0 0.2 0.4 0.6 0.8 146

47

48

49

50

51

52

53

54

time (sec)

Pist

on D

ispl

acem

ent (

mm

)

Operating Cylinder Xactual

Operating Cylinder Xreference Parameters:

• = 32• Amplitude= 3.5mm• Frequency = 5Hz

Study case

Slide 53/58

Page 54: master defense

Master Thesis Defense

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Conclusion

The proposed design of the hardware in the loop test rig was discussed throughout the thesis.

The mechanical, hydraulic, electrical and electronic interfaces and the control algorithm were

presented throughout the study.

The experimental measurements validate the implemented software model and theoretical

calculations of the system.

The device can also be used to test the time response for standard directional

hydraulic valves without the need to connect a controller.

Slide 54/58

Page 55: master defense

Master Thesis Defense

Khaled H. Emam

Introduction Mechanical Design

Hydraulic Design

Controller Design

Data Acquisition Results Conclusion

Recommendation for future work

The test rig can be used to test the time response for standard directional hydraulic valves

without the need to connect a controller.

This study is considered the first step towards manufacturing a servo cylinder test rig in the

GUC.

Future work should be directed towards implementing the controller using modern control

approach or fuzzy logic control.

Slide 55/58

Page 56: master defense

Master Thesis Defense

Khaled H. Emam

Thanks for listeningYour questions & feedback are highly appreciated

Khaled Hossam [email protected]

Acknowledgement

Slide 56/58

Page 57: master defense

Master Thesis Defense

Khaled H. Emam

Proportional controller tuning:

0 0.1 0.2 0.3 0.4 0.50

0.5

1

1.5

time (sec)

Cyl

inde

r Stro

ke (m

m)

ISEIAEITSEITAEZiegler-Nichols

Slide 57/58

Page 58: master defense

Master Thesis Defense

Khaled H. Emam

PID -controller tuning:

0 0.1 0.2 0.3 0.4 0.50

0.2

0.4

0.6

0.8

1

1.2

1.4

1.6

time (sec)

Cyl

inde

r stro

ke (m

m)

ISEIAEITSEITAEZiegler-Nichols

Slide 58/58