New system identification model for predictive functional control with observer for an intelligent pneumatic actuator.

NEW SYSTEM IDENTIFICATION MODEL FOR PREDICTIVE FUNCTIONAL
CONTROL WITH OBSERVER FOR AN INTELLIGENT PNEUMATIC ACTUATOR

KHAIRUDDIN BIN OSMAN

UNIVERSITI TEKNOLOGI MALAYSIA

© Universiti Teknikal Malaysia Melaka

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PSZ 19: 16 (Pind. 1/07)

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Author's full name

: KHAIRUDDIN BIN OSMAN

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_:3_0_J_U_LY
_ l 9--'8' -l_ __ _ _ _ _ _ _ _ _ _ _ _ __

Title

: NEW SYSTEM IDENTIFICATION MODEL FOR PREDICTIVE
FUNCTIONAL CONTROL WITH OBSERVER FOR AN INTELLIGENT
PNEUMATIC ACTUATOR

Academic Session

: 2014/2015 - 2
-- - - - - - -- - - - - - -- - ---

I declare that this thesis is classified as :

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NOTES

IR. DR. AHMAD 'ATHIF BIN MOHD FAUDZI

(NEW IC NO./PASSPORT NO.)

NAME OF SUPERVISOR

Date : 30 MARCH 2015


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Philosophy (Electrical Engineering)"

Signature
Name of Supervisor I : Ir. Dr. Ahmad 'Athifbin Mohd Faudzi
Date

30 March 2015


Mセ@

' ,,

Signature
--·---··--·------················-··--·-···---·--··--··--···
Name of Supervisor II: Prof. Dr. Mohd Fua'ad bin Rahmat
Date

3 0 March 2015

© Universiti Teknikal Malaysia Melaka

BAHAGIAN A - Pengesahan Kerjasama*
Adalah disahkan bahawa projek penyelidikan tesis ini telah dilaksanakan melalui kerjasama
antara _ _ _ _ _ _ _ _ _ _ dengan _ _ _ _ __ _ __ _
Disahkan oleh:
Tandatangan

Tarikh :


Nama
Jawatan
(Cop rasmi)

* Jika p eny ediaan tesis/projek melibatkan kerjasama.
BAHAGIAN B - Untuk Kegunaan Pejabat Sekolah Pengajian Siswazah
Tesis ini telah diperiksa dan diakui oleh:
N ama dan Alamat Pemeriksa Luar

Prof. Dr. Mohd Nasir Taib
Faculty Electrical Engineering,
Universiti Teknologi Mara (UiTM),
40450 Shah Alam,
Selangor.

Nama dan Alamat Pemeriksa Dalam

Prof. Madya Dr. Yahaya bin Md Sam
Fakulti Kejuruteraan Elektrik,

UTM Johor Bahru.

Disahkan oleh Timbalan Pendaftar di Sekolah Pengajian Siswazah:

Tandatangan :
Nama

Tarikh :

ASRAM BIN SULAIMAN

@

SAIM

© Universiti Teknikal Malaysia Melaka

NEW SYSTEM IDENTIFICATION MODEL FOR PREDICTIVE FUNCTIONAL
CONTROL WITH OBSERVER FOR AN INTELLIGENT PNEUMATIC ACTUATOR


KHAIRUDDIN BIN OSMAN

A thesis submitted in fulfilment of the
requirements for the award of the degree of
Doctor of Philosophy (Electrical Engineering)

Faculty of Electrical Engineering
Universiti Teknologi Malaysia

MARCH2015

© Universiti Teknikal Malaysia Melaka

11

I declare that this thesis entitled "New System Identification Model for Predictive

Functional Control with Observer for an Intelligent Pneumatic Actuator" is the result of
my own research except as cited in the references. The thesis has not been accepted for
any degree and is not concurrently submitted in candidature of any other degree.


Signature
Name

: Khairuddin bin Osman

Date

: 30 March 2015

© Universiti Teknikal Malaysia Melaka

iii

Specially dedicated to:
My kind parents for their priceless support and motivation.

iv

ACKNOWLEDGEMENT


Praise to the Almighty...

First of all, thanks to our Creator for the continuous blessing and for giving me
the strength and chances in completing this thesis.
Special thanks to my project supervisor, Ir. Dr. Ahmad ‘Athif bin Mohd Faudzi
and co-supervisor, Prof. Dr. Mohd Fua’ad bin Rahmat, for their guidance, support and
helpful comments in doing this research.

My family deserves special mention for their constant support and for their role
of being the driving force towards the success of my project. My sincere appreciation
also goes to everyone whom I may not have mentioned above who have helped directly
or indirectly in the completion of my PhD thesis.

I would also like to thank Universiti Teknologi Malaysia (UTM), Ministry of
Education (MOE) Malaysia under Skim Latihan Akademik IPTA (SLAI), Universiti
Teknikal Malaysia Melaka (UTeM) and Okayama University for their support. Thanks
to them.

v


ABSTRACT

This thesis presents System Identification (SI) model development and controller
design using Predictive Functional Control with Observer (PFC-O) algorithm for realtime control of Intelligent Pneumatic Actuator (IPA). An application of Ankle-Foot
Rehabilitation Exerciser (AFRE) device uses the IPA system. The plant mathematical
model in discrete transfer functions was approximated using the MATLAB system
identification toolbox for open-loop input-output experimental data. The SI process was
conducted through a series of activities including observation and data gathering, Auto
Regressive with Exogenous Input (ARX) model structure selection, model estimation,
model validation and the implementation of PFC-O algorithm designed to prove the
operation of IPA is acceptable. PFC-O algorithm was selected as a new control strategy
for IPA to overcome the real-time nonlinearities and uncertain characteristics. PFC-O
algorithm was used for position control, force control and realized compliance control
for stiffness characteristic through MODBUS communication protocol. Performance
assessment of the controller was programmed into MATLAB and validated through two
real-time experiments: Personal Computer (PC) based (using National Instrument (NI)
devices) and embedded based (using Programmable System on Chip (PSoC)
microcontroller). The results between simulation, theoretical calculation and both realtime experiment matched closely and achieved the control objectives. Towards the
AFRE application, the IPA can be configured through MATLAB Graphical User
Interface (GUI) via personal computer where user can adjust the required Range of
Motion (ROM) and resistance in real-time. The AFRE system testing was conducted
successfully on selected subjects for various ROM and resistance using the proposed
algorithm. The significant finding demonstrates that the new PFC-O control algorithm
reduces the control effort and gives better performance in terms of tracking accuracy as
compared to the existing control algorithm.

vi

ABSTRAK

Tesis ini membentangkan pembangunan model Pengenalpastian Sistem (SI) dan
reka bentuk Kawalan Fungsian Ramalan dengan Pemerhati (PFC-O) algoritma untuk
kawalan masa nyata Penggerak Pneumatik Pintar (IPA). Aplikasi peranti Senaman
Pemulihan Buku Lali-Kaki (AFRE) menggunakan sistem IPA itu. Model matematika
dalam

rangkap

pengenalpastian

pindah
sistem

diskret
MATLAB

telah

dianggarkan

untuk

menggunakan

gelung-buka

kotak

alat

masukan-keluaran

data

eksperimen. Proses SI telah dijalankan melalui satu siri aktiviti termasuk pemerhatian
dan perhimpunan data, pemilihan struktur model Auto Regresif bersama Input Luaran
(ARX), penganggaran model, pengesahan model dan implimentasi PFC-O algoritma
direka untuk membuktikan operasi IPA boleh diterima. PFC-O algoritma dipilih sebagai
strategi kawalan baru untuk IPA bagi mengatasi parameter tak lelurus masa sebenar dan
ciri-ciri yang tidak menentu. PFC-O algoritma digunakan untuk kawalan kedudukan,
kawalan kuasa dan sifat kawalan kelembutan direalisasikan melalui protokol komunikasi
MODBUS. Penilaian prestasi pengawal diprogramkan ke MATLAB dan disahkan
melalui dua ujikaji masa nyata: berdasarkan Komputer Peribadi (PC) (dengan
menggunakan

peranti

Instrumen

Nasional

(NI))

dan

berdasarkan

terbenam

(menggunakan mikropengawal Sistem Atur Cara pada Cip (PSoC)). Keputusan antara
simulasi, pengiraan teori dan ujikaji kedua-dua masa nyata dipadankan dan mencapai
objektif kawalan. Bagi mencapai aplikasi AFRE, IPA boleh dikonfigurasikan menerusi
grafik Antara Muka Pengguna (GUI) MATLAB melalui komputer peribadi di mana
pengguna boleh menyesuaikan Julat Pergerakan (ROM) yang diperlukan dan rintangan
dalam masa nyata. Ujian sistem AFRE yang telah dijalankan ke atas subjek yang dipilih
untuk pelbagai ROM dan rintangan berjaya menggunakan algoritma yang dicadangkan.
Penemuan penting menunjukkan kawalan algoritma PFC-O baru dapat mengurangkan
usaha kawalan dan memberikan prestasi yang lebih baik dari segi ketepatan pengesanan
berbanding dengan pengawal algoritma sedia ada.

vii

TABLE OF CONTENTS

CHAPTER

1

2

TITLE

PAGE

DECLARATION

ii

ACKNOWLEDGEMENT

iv

ABSTRACT

v

ABSTRAK

vi

TABLE OF CONTENTS

vii

LIST OF TABLE

xi

LIST OF FIGURES

xii

LIST OF ABBREVIATIONS

xv

LIST OF SYMBOLS

xvii

LIST OF APPENDICES

xix

INTRODUCTION

1

1.1

Research Background

1

1.2

Problem Statement

4

1.3

Research Objectives

5

1.4

Scope of Work

5

1.5

Contribution of the Work

6

1.6

Organization of the Thesis

6

LITERATURE REVIEW

8

2.1

Introduction

8

2.2

Pneumatic Cylinders

8

viii
2.3

System Identification and Controller
Selection

2.4

2.5

3

4

15

Ankle Rehabilitation and its Associated
Challenges

21

Summary

26

RESEARCH METHODOLOGY

27

3.1

Introduction

27

3.2

Research Process Flow

27

3.3

Summary

30

MODEL AND CONTROL ALGORITHM
STRATEGIES

31

4.1

Introduction

31

4.2

Intelligent Pneumatic Actuator (IPA) System

4.3

4.4

Operations

31

System Identification Technique

34

4.3.1

Position Model

37

4.3.2

Force Model

39

Predictive Functional Control with Observer
(PFC-O) Design

42

4.4.1

Predictive Functional Control (PFC)

42

4.4.2

Observer

46

4.5

Stiffness Characteristic

48

4.6

Embedded Controller Algorithm with Stiffness
Characteristics

50

4.6.1

Simplification of Algorithm

50

4.6.2

Control Stability Test

54

4.6.3

Profiling Algorithm Execution
Performance

4.7

Summary

55
58

ix
5

INTELLIGENT PNEUMATIC ACTUATOR
SYSTEM ANALYSIS

59

5.1

Introduction

59

5.2

Experimental Setup

59

5.3

IPA System Experiments

64

5.3.1

Models Tracking Analysis

64

5.3.2

Stiffness Characteristics with Deflection
Analysis

5.3.3

Position Control with Loading Effects
Analysis

5.4

5.5

67

5.4.1

Position Control

68

5.4.2

Force Control

71

Embedded System Validations

5.5.2

75

Stiffness Characteristics with Deflection
Analysis

6

66

Model Validations

5.5.1

5.6

65

75

Position Control with Loading Effect

Analysis

78

Summary

87

ANKLE-FOOT REHABILITATION EXERCISER
SYSTEM

88

6.1

Introduction

88

6.2

Design and Development of AFRE

89

6.2.1

Characteristics

89

6.2.2

Prototype

90

6.2.3

MODBUS Communication Protocol

93

6.2.4

Graphical User Interface (GUI)

98

6.3

AFRE System Experiments

99

6.3.1

Testing with Measurement Tool

99

6.3.2

Testing with Selected Subjects

100

x

6.4

6.5

7

6.3.2.1 Fixed Movement

101

6.3.2.1 Two-way movement

102

Data Collection for AFRE System

103

6.4.1

Testing with Measurement Tool

103

6.4.2

Testing with Selected Subject

104

6.4.2.1 Fixed movement

104

6.4.2.2 Two-way movement

105

Summary

109

CONCLUSIONS AND FUTURE WORKS

110

7.1

Conclusions

110

7.2

Suggestions for Future Works

111

REFERENCES
Appendices A – C

113
124 – 132

xi

LIST OF TABLE

TABLE NO.

TITLE

4.1

Valve Configuration

5.1

Comparison of the simulated performances for position
control

5.2

69

71

Comparison of the simulated performances for force
control

5.4

32

Comparison of simulated and experimental
performance for position control using PFC-O

5.3

PAGE

73

Comparison of simulated and experimental performance
for force control using PFC-O

74

5.5

Comparison of deflection results

77

5.6

Comparison of horizontal payloads for
experimental PFC-O performances

5.7

6.1

81

Comparison of vertical payloads for experimental PFC-O
performances

84

Comparison of the subject’s profile

101

xii

LIST OF FIGURES

FIGURE NO.

TITLE

PAGE

2.1

IPA system and its parts

14

2.2

Ankle rehabilitation trends

26

3.1

Model development flow chart

28

4.1

IPA schematic operations

33

4.2

Process model for SI and its implementation

35

4.3

Response of system to step input signal

38

4.4

Position Model views

39

4.5

Response of system to PRBS signal

40

4.6

Force Model views

41

4.7

Block diagram of PFC-O for plant model

48

4.8

Coil Spring illustration

49

4.9

Block diagram for control system with stiffness
characteristic

50

4.10

PFC controller stage

51

4.11

Observer stage

53

4.12

Eigenvalues of the closed-loop control system

55

4.13

PSoC CY8C27243

56

4.14

Measurement of effective algorithm execution time

57

4.15

Measurement of effective algorithm sampling time

58

5.1

National Instrument (NI) devices connection

60

5.2

Test panel monitoring

61

xiii
5.3

New wiring instruction to SCB-68 M series devices
terminal

62

5.4

Embedded system communication

63

5.5

Real experiment setup using NI devices

65

5.6

Pneumatic actuator with mass

66

5.7

Loading effect experimental setup

67

5.8

Simulation step responses for position

68

5.9

Simulation multi-step responses for position

69

5.10

Position step responses

70

5.11

Position multi-step responses

70

5.12

Simulation step responses for force

72

5.13

Simulation multi-step responses for force

72

5.14

Force step responses

73

5.15

Force multi-step responses

74

5.16

Stiffness characteristic responses

76

5.17

Position step response for different stiffness

76

5.18

Deflection analysis responses

77

5.19

Experimental position step response for PFC-O under
horizontal loads

5.20

Experimental position multi-step response for PFC-O
under horizontal loads

5.21

6.1

83

PFC-O force outputs during positional multi-step
experiment under horizontal loads

5.24

82

Experimental position multi-step response for PFC-O
under vertical loads

5.23

80

Experimental position step response for PFC-O under
vertical loads

5.22

79

85

PFC-O force outputs during positional multi-step
experiment under vertical loads

86

Movements of the ankle-foot (Dai et al., 2011)

89

xiv
6.2

Position foot and angle movement of dorsiflexion-plantar
flexion (Ortega et al., 2012)

90

6.3

AFRE system design with dimension using SolidWorks

91

6.4

Real AFRE system and its part

91

6.5

Top level function

94

6.6

Turn on IPA control algorithm (servomechanism on)

95

6.7

Write set point to IPA (position, stiffness)

96

6.8

Flow Chart 4 - Read feedback data from IPA
(position, pressure)

97

6.9

AFRE GUI

99

6.10

Validation with measurement tool

100

6.11

Real physical picture for each subject

101

6.12

Comparison of data embedded and measurement
responses

103

6.13

Fixed movement results

105

6.14

Two-way movement result for subject 1

106

6.15

Two-way movement result for subject 2

107

6.16

Two-way movement result for subject 3

108

6.17

Summary of maximum performance of the subjects

109

xv

LIST OF ABBREVIATIONS

IPA

-

Intelligent Pneumatic Actuator

PASS

-

Pneumatic Actuator Seating System

PI

-

Proportional-Integral

SI

-

System Identification

PFC-O

-

Predictive Functional Control with observer

NI

-

National Instrument

PSoC

-

Programmable System on Chip

CPM

-

Continuous Passive Motion

ROM -

-

Minimum Range of Motion

GUI

-

Graphical User Interface

HME

-

Human Muscle Enhancer

ISAC

-

Intelligent Soft Arm Control

MP

-

Myo-Pneumatic

PLC

-

Programmable Logic Controller

ADC

-

Analog to Digital Converter

PC

-

Personal Computer

USB

-

Universal Serial Bus

CAD

-

Computer Aided Design

CAM

-

Computer Aided Manufacturing

PRSD

-

Planetary Roller Spindle Drive

LED

-

Light Emitting Diode

PRBS

-

Pseudo Random Binary Sequence

PAM

-

Pneumatic Artificial Muscle

ARX

-

Auto-Regressive with Exogenous Input

xvi
MGA

-

Modified Genetic Algorithm

MRE

-

Mixed-Reality Environment

RLS

-

Recursive Least Squares

ARMA

-

Auto-Regressive Moving-Average

PID

-

Proportional-Integral-Derivative

MPC

-

Model Predictive Control

DMC

-

Dynamic Matrix Control

MAC

-

Model Algorithm Control

GPC

-

Generalized Predictive Control

EPVA

-

Electro-Pneumatic Valve Actuator

CARMA

-

Controlled Auto-Regressive Moving Average

DOF

-

Degrees of Freedoms

ROM

-

Range of Motion

PPAFO

-

Powered Portable Devices Ankle-Foot Orthosis

KAFO

-

Knee Ankle Foot Orthosis

DAQ

-

Data Acquisition

ARMAX

-

Auto-Regressive Moving Average with Exogenous
Input

OE

-

Output-Error

BJ

-

Box-Jenkins

FPE

-

Final Prediction Error

MLS

-

Maximum Length Sequence

PWM

-

Pulse-Width Modulation

AIC

-

Akaike's Information Criteria

PSO

-

Particle Swarm Optimization

I2C

-

Inter-Integrated Circuit

UART

-

Universal Asynchronous Receiver/Transmitter

Sim

-

Simulation

Emb

-

Embedded

xvii

LIST OF SYMBOLS

Fd

-

force data

P1, P2

-

pressure data

A1, A2

-

cross-sectional areas

d

-

time delay

na

-

number of poles

nb

-

number of zeros

V

-

loss function,

na

-

number of approximated parameter,

N

-

number of sample

y

-

true value

ˆ
y

-

approximate value

y

-

mean value

Δt

-

bit interval or clock pulse time

xk

-

the state model

uk

-

the input model

yk

-

the measured output model

i

-

value of n

yk

-

the most recent measured output

Ψ

-

time constant

F

-

force reference

ks

-

coefficient of stiffness

n1

-

one coincidence horizon

Kob

-

gain observer

δ

-

deflection

xviii
W

-

the force exerted on a body by gravity

g

-

gravitational acceleration

np

-

PSoC 11-bit delta-sigma

x', y'

-

the mobile coordinate system

OS

-

Overshoot

TS

-

Settling Time

TR

-

Rise Time

ess

-

Steady State Error

IAE

-

Integral Absolute Error

xix

LIST OF APPENDICES

APPENDIX

TITLE

PAGE

A

List of Publications

124

B

List of Awards

130

C

Calculation

131

1

CHAPTER 1

INTRODUCTION

1.1

Research Background

Actuators that can process information from an input given and control the
output independently are highly demanded in applications of mechatronics. Pneumatic
actuating system is normally chosen because of their advantages of high power-toweight ratio, lightweight, comparative low cost, easy maintenance and having a simple
structure. Moreover, pneumatic actuators are safe and reliable. They are relatively small
in size compared to hydraulic actuators. They have fast response, and at high
temperatures and in nuclear environments, they have the added advantages over
hydraulic actuators. Pneumatic systems have many attributes that make them attractive
for use in difficult environments: gases are not subjected to the temperature limitations
of hydraulic fluids; the actuator exhaust gases need not be collected, so fluid return lines
are unnecessary and long term storage is not a problem because pneumatic systems are
virtually dry and have no organic materials.
Pneumatic systems were first created in the 16th century. Since then, many
developments have been done to the pneumatic actuators to suit the different automation
and industrial purposes according to the desired accuracy and performance and to the
amount of force that is needed for each particular application. In the 20th century,
complex and intelligent pneumatic systems have been developed. The intelligent
pneumatic plant used in this research was taken from previous researches by