PROCEEDING

ICARES 2014

November 13-14, 2014 Sheraton Mustika I otei

Yogyakarta. Indonesia

Organized by:

IndonesiOi Section ]nim .:>4[u'I.liu:! T4!t:il[1ulo31' School of Elecmcal Chapl\!J" n! mm~ AI!("{I'!ip<l(:1,! C I! n t !'!' f" . N 'Hl~itl1l Eng i /l \;! l: r 1 f1 g . ilnd El~t:trtJnic SyslCms ! 11 ::s l 1 t u • It . (1 r Te[kOtll Univl,i.l'sily. S Q C i e l~' Il n diE. E E Al~ro!IDUlk~ &. Sj)JlCIl? Bnndung, lllda!nesill G e (J S,.,I e n Ct~ & Rt"fito t Ii' n"O\PAN.lodu ne-~lll ) Sp.n!:tl.tl~ So~ii!1y

ISBN: 978-14799~6188-7

2014 IEEE INTERNATIONAL CONFERENCE ON AEROSPACE ELECTRONICS AND REMOTE SENSING

fo r de taiIin forma tion: http://indoa.essBTss. org/icares

icares20 l·l·C!!) yahoo.cOI11

Sponsors:

IndOlle.:$l13 ~~ctH:l1l .I!l.UU Chtlpter CJf IEEE Aorosptlw <I [ld ~lec Ironic SJ'S~ ems 5oci'HY I'Ind IE ·E.E Gc tI !ldl:! t~C ·1: & RL'mll tt!' Surl. irlf,l Sm:let)'

Technical en-Sponsors: -Satellite Te-chlllolog)"Center , NllLi{JllallIistitIJt~ Il( Aerorunlrics &. SP~C-8 (LAPAN , Illdofll'~ii!l)-

- Singapore Sec lion Joint Chllpter lEE E A~nlspace and Electronic Systems Society .& lEEE Gea-science ,m.d Re moti" SeIl1ilng Srn::iety--South Austflll lll Section Joint ChajJt~r ol IEEE Aewsp:ice 3.l'Id EIei:rrun[c S)~teIT15 Society llild IEEE Control SY$t.emS Sm.:i·t'ty-

-lEEE Gem;CiE'llCe and Re mote -Sens.ing Society J aj)<ill ChaptC'.'l'--IEEE Geoscience IlIlO RenlDte Sensing Society Mawysia: Ch'lpter-

-lREE· Ge(l~dem:e and Remme Sen$iog-Sor:iety Gujarat Chilpter. lndia--lntematlG.nnl Centre for Radii' Science, India-

Support~d by:

ST Electronics ,VECTRONtC _ ~ Aerospace

,...::j1 .... ~lIlr~ .... ......m.-

ABOUT

IcARES 2014

This 2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology (ICARES 2014) will be a platform for disseminating timely information both in the sensor technology, smaller satellites and launch vehicles as well as in the processing of information. The event shall become a unique opportunity for the AES (Aerospace and Electronic Systems), GRS (Geoscience and Remote Sensing) and other IEEE chapters to exchange views and disseminate new trends and advances in the respected fields.

Sponsored by Indonesia Section Joint Chapter of IEEE Aerospace and Electronic Systems Society (AESS) and IEEE Geoscience & Remote Sensing Society (GRSS), and the IEEE Communications Society Indonesia Chapter, ICARES has a strong foundation of bringing together industry and academia. In 2014, Yogyakarta will become the foundation of Aerospace Electronic and Remote Sensing Technology by hosting ICARES 2014.

Copyright Statement Copyright and Reprint Permission: Abstracting is permitted with credit to the source.

Libraries are permitted to photocopy beyond the limit of U.S. copyright law for private use of patrons those articles in this volume that carry a code at the bottom of the first page,

provided the per-copy fee indicated in the code is paid through Copyright Clearance Center, 222 Rosewood Drive, Danvers, MA 01923. For reprint or republication permission, email to

IEEE Copyrights Manager at pubs permissions@ieee.org. All rights reserved. Copyright ©2014 by IEEE.

TABLE OF CONTENT

COMMITTEES........................................................................................... iv

PROGRAM................................................................................................ vii

AUTHOR INDEX.......................... .............................................................. xiii

PAPERS LIST. .. . . .. . . . .. . . .. . . . . .. . . .. . . .. . . . .. . . .. .. . . .... . . . . .. . . . .. . . .. . . .. .. . . .. . . . .. . . .. . . .. . . .. . . . . xvi

iii

COMMITTEES

Organizing Committee

General Chair Wahyudi Hasbi, Satellite Technology Center, National Institute of Aeronautics & Space (LAPAN, Indonesia)

Conference Chair Arief Hamdani Gunawan, Telkom Indonesia

Vice Chairs Muhammad Ary Murti, School of Electrical Engineering, Telkom University Saleh Dwi Mardiyanto, School of Electrical Engineering, Telkom University

Secretary Ratna Mayasari, School of Electrical Engineering, Telkom University Trasma Yunita, School of Electrical Engineering, Telkom University Nurati Firdaus Muharom, Satellite Technology Center, National Institute of Aeronautics & Space (LAPAN,

Indonesia)

Publication Rita Purnamasari, School of Electrical Engineering, Telkom University Asep Mulyana, School of Electrical Engineering, Telkom University Akhmad Hambali, School of Electrical Engineering, Telkom University

Publicity Afief Dias Pambudi, School of Electrical Engineering, Telkom University Efri Suhartono, School of Electrical Engineering, Telkom University

Exhibition Dian Yudistira, Satellite Technology Center, National Institute of Aeronautics & Space (LAPAN, Indonesia) Rinto Andri Wiendiarto, Satellite Technology Center, National Institute of Aeronautics & Space (LAPAN,

Indonesia) Unggul Sa trio Yudho Torno, Satellite Technology Center, National Institute of Aeronautics & Space (LAPAN,

Indonesia) Moh. Farid Huzain, Satellite Technology Center, National Institute of Aeronautics & Space (LAPAN,

Indonesia)

Technical Program Committee

TPC Chair Dr. Arifin Nugroho, Telkom University, Indonesia Dr. Rina Pudji Astuti, Telkom University, Indonesia

TPCMember Prof. Alessandra Budillon, University of Naples Parthenope, Italy Prof. Antonios Tsourdos , Cranfield University , United Kingdom Prof. Chao Wang , Institute of Remote Sensing and Digital Earth, Chinese Academy of Sciences , P.R. China Prof. Chris Baker , The Ohio State University , USA Prof. Christopher Gomez, University of Canterbury, New Zealand Prof. Daniele Riccio , Universita degli Studi di Napoli Federico II , Italy Prof. Gerard Parr , University of Ulster , United Kingdom Prof. Hans Braun , RST Radar Systemtechnik AG , Germany Prof. Herve Borrion , University College London , United Kingdom

iv

Prof. Hussam AI-Bilbisi , University of Jordan , Jordan Prof. Jocelyn Chanussot, Grenoble Institute of Technology, France Prof. Josaphat Tetuko Sri Sumantyo, University of Chiba, Japan Prof. Koo Voon Chet, Multimedia University Malaysia Prof. Krzysztof Kulpa , Warsaw University of Technology , Poland Prof. Kye-Yak See, Nanyang Technological University, Singapore Prof. Laksana Handoko Indonesian Institute of Sciences (LIPI), Indonesia Prof. Lu Yilong, Nanyang Technological University, Singapore Prof. Malek Hussain , Kuwait University , Kuwait Prof. Martti Hallikainen , Aalto University , Finland Prof. Maurizio Di Bisceglie, University of Sannio, Italy Prof. Maurizio Migliaccio, Universita Napoli Parthenope, Italy Prof. Minhui Zhu , Chinese Academy of Sciences , P.R. China Prof. Muhamad Asvial, University of Indonesia Prof. Nickolai Kolev , Naval Academy , Bulgaria Prof. Oleg Stukach, Tomsk Polytechnic University, Russia Prof. Peter Edenhofer , University of Bochum , Germany Prof. Peter Hoogeboom, Delft University of Technology, The Netherlands Prof. Ray Sheriff, University of Bradford, United Kingdom Prof. Robert Luckner,TU Berlin,Germany Prof. Rick S. Blum, Lehigh University, USA Prof. Shih Yuan Lin, National Chengchi University, Taiwan Prof. Soewarto Hardhienata,Indonesian National Institute for Aeronautics & Space (LAPAN), Indonesia Prof. Steven Gao, School of Engineering and Digital Arts, University of Kent, United Kingdom Prof. Udo Renner, TU Berlin, Germany Prof. Uwe Stilla , Technische Universitaet Muenchen , Germany Prof. Wei Hong, Southeast University, China Prof. Zulkifly Abbas, Universiti Putra Malaysia, Malaysia Dr. Aishwarya Narain, Nascent Info Technologies Pvt. Ltd, India Dr. Alban Duverdier, Centre National D'Etudes Spatiales (CNES), France Dr. Alberto Refice, Consiglio Nazionale delle Ricerche, Italy Dr. Alexander Kocian, Consiglio Nazionale delle Richerche, Italy Dr. Chan Yee Kit, Multimedia University Malaysia Dr. Charles Livingston , DRDC , Canada Dr. Christoph Gierull , DRDC Ottawa , Canada Dr. Chung-Chi Lin, European Space Agency jESTEC, The Netherlands Dr. Claudio Sacchi, University of Trento, Italy Dr. Daniele Perissin, Politecnico di Milano, Italy Dr. Diego Cristallini , Fraunhofer FHR, Germany Dr. Dinesh Sathyamoorthy, Science & Technology Research Institute for Defence, Malaysia Dr. Endra Pitowarno, Electronics Engineering Polytechnic Institute of Surabaya, Indonesia Dr. Fabio Bovenga, Research National Council of Italy, Italy Dr. Ferdinando Nunziata, Universita di Napoli Parthenope, Italy Dr. Gianfranco Fornaro, CNR-IREA, Italy Dr. Heroe Wijanto, University of Telkom, Indonesia Dr. Hubert Cantalloube, ONERA , France Dr. Haria Thibault, Vodafone Group R&D , United Kingdom Dr. Ilias Andrikopoulos, Space Hellas S.A., Greece Dr. Jens Klare, Fraunhofer FHR , Germany Dr. Joachim Boukamp , Cassidian , Germany Dr. Kai Daniel , TU Dortmund University , Germany Dr. Keith Morrison , Cranfield University , United Kingdom Dr. Les Novak , Consultant , USA Dr. Lloyd Wood, University of Surrey, United Kingdom

v

Dr. Marco Chiani, University of Bologna, Italy Dr. Marco Martorella,University of Pisa, Italy Dr. Matteo Pardini , German Aerospace Center (DLR) , Germany Dr. Matthias Weill, Fraunhofer FHR , Germany Dr. Mohammed Jahangir , Aveillant Ltd , United Kingdom Dr. Nicolas Bertaux, Fresnel Institute, France Dr. Paolo Pampaloni, IFAC-CNR, Italy Dr. Paul Scerri , CMU , USA Dr. Pauline Chan , University of Bradford , United Kingdom Dr. Ridanto Eko Putro, School of Aeronautics, Bandung Institute of Technology, Indonesia Dr. Sachin Kumar Agrawal, Indian Institute of Technology lIT Delhi, India Dr. Salvatore Maresca , NATO Science and Technology Organization Centre for Maritime Research and

Experimentation , Italy Dr. Salvatore Stramondo, Istituto Nazionale di Geofisica e Vulcanologia, Italy Dr. Shiv Mohan, ISRO, India Dr. Simone Morosi, University of Florence - CNIT, Italy Dr. Sithamparanathan Kandeepan, RMIT University , Australia Dr. Sithamparanathan Kandeepan, RMIT University, Australia Dr. Stefano Coraluppi , Compunetix Inc., USA Dr. Stefano Perna , Universita degi Studi di Napoli "Parthenope", Italy Dr. Stephen Hayward , QinetiQ ltd , United Kingdom Dr. Tri K Priyambodo, Gajah Mada University, Indonesia Dr. Tuong-Thuy Vu, The University of Nottingham, Malaysia Dr. Vinod Mishra , ARL , USA Dr. Yee-Jin Cheon, Korea Aerospace Research Institute, Korea Dr. Zhong Xionghu, Nanyang Technological University, Singapore

vi

Time

08.00-09.00

09.00-09.15

09.15-09.20

09.20-09.30

09.30-10.00

10:00-10: 15

10.50-11.00

11.00-11.30

11.30.12.00

12.00-13.00

13:00-14:30

14.30-15.00

15:00-17:00

17.00-17.30

19.00-20.00

Time

08.00-08.30

08:30-09:45

09.45-10.15

10: 15-11: 15

11.15-12.30

12:30-13:30

13:30-14:30

14.30-15.00

15:00-16:45

16.45-17.00

PROGRAM

Day One: Thursday, November 13, 2014

Program

On-Site Registration

Traditional Dance

ICARES-2014 General Chairman Report

Indonesia Section Joint Chapter of IEEE AESS/GRSS Opening Remarks

Keynote 1

Photo Session

Break & Exhibition Tour

Keynote 2

Keynote 3

Lunch Break

Session I

Aircraft & UAV

Coffee Break & Exhibition

Session II

Aerospace Electronics System

Keynote 4

Gala Dinner

Day Two: Friday, November 14, 2014

Program

Registration

Session III

Satellite Mission

Coffee Break & Exhibition

Session IV

Satellite Technology

Lunch Break

Session V

UAV, Attitude & Control

Session VI

Remote Sensing Science & Technology I

Coffee Break & Exhibition

Session VII

Remote Sensing Science & Technology II

Closing Statement

vii

Room

East Lobby

Mustika Room

Mustika Room

Mustika Room

Mustika Room

Mustika Room

East Lobby

Mustika Room

Mustika Room

Androwino Bistro

Mustika Room

East Lobby

Mustika Room

Mustika Room

Swimming Pool Side

Room

East Lobby

Mustika Room

East Lobby

Mustika Room

Androwino Bistro

Mustika Room

Mustika Room

East Lobby

Mustika Room

Mustika Room

KEYNOTE SESSION

Thursday, November 13, 2014 Mustika Room, Sheraton Mustika Yogyakarta

& '{l

," . L • . _ . .' , _ .... ," ., I

\ . \ \ �

Prof. Dr. Thomas Djamaluddin

Indonesia National Institute of Aeronautics & Space (LAPAN) Chairman

The Utilization of Aerospace Technology in Strengthening Indonesian Maritime Domain

Awareness

09.30-10.00

Prof. Wooil Moon

{VP of Professional Activities, IEEE-GRSS} Director, Laboratory of Satellite-Geophysics

University of Manitoba Faculty of Environment Earth and Resources Winnipeg, MB R3T 2N2

CANADA

New Geophysics Application Development for Polarimetric SAR

11.00-11.30

Prof. Wolfgang Martin Boerner

Professor Emeritus and Distinguished Radar Research Scientist USN Director-Em., UIC-ECE

Communications, Sensing & Navigation Laboratory CHICAGO-USA

The challenge for still unresolved development of Multi-band Equatorially Orbiting POLSAR

satellite sensors - an integral task for the major space-SAR technology centers world-wide

including LAPAN- and focused on the Indonesian Islands Archipelago

11.30.12.00

Dr. M. Ridwan Effendi

Commissioner of Indonesian Telecommunications Regulatory Authority

Mobile & Wireless Technology: Business & Industry Highlights in Digital Business Era

17.00-17.30

viii

TECHNICAL SESSION

Oral Sessions

Thursday, November 13-14, 2014

Session I Aircraft & UAV Mustika Room

1

2

3

4

5

6

A Utilit� Aircraft for Remote Sensing Missions with a High-Precision Automatic Flight Control S�stem

Robert Luckner (TU Berlin & Institute of Aeronautics and Astronautics, Germany); Lothar Dalldorff

(STEMME AG, Germany); Reinhard Reichel (UniversiUit Stuttgart, Germany)

UAV & Satellite Communications- Live Mission-Critical Visual Data

Harald Skinnemoen (AnsuR Technologies, Norway)

Position Tracking of a Hexacol2ter using a Geometric Backstel2l2ing Control Law - EXl2erimental Results

Guillermo P. Falconi and Florian Holzapfel (Technische Universitat Munchen, Germany)

Hexacol2ter Outdoor Flight Test Results of an Extended State Observer based Controller

Christian Heise, Guillermo P. Falconi and Florian Holzapfel (Technische Universitat Munchen, Germany)

Ol2timal Trajectories for RPAS with Discrete Controls and Discrete Constraints

Matthias Rieck, Maximilian Richter, Matthias Bittner and Florian Holzapfel (Technische Universitat

Munchen, Germany)

Real-time Simulation of Nonlinear Transmission Behavior in Electro-Mechanical Flight Control S�stems

Patrick Lauffs, Markus Hochstrasser and Florian Holzapfel (Technische Universitat Munchen, Germany)

Session II Aerospace Electronics System Mustika Room

Design And Iml2lementation of Pa�load Data Handling Based on Field Programmable Gate Arra�

1 Widya Roza and Deddy Amin (Satellite Technology Center National Institute of Aeronautics & Space

LAPAN, Indonesia); Eriko Nasemudin Nasser (National Institute of Aeronautics and Space, Indonesia)

New Ultra-Wideband Filters Based on Tuning Forks Shal2e and CSRRs

2 Ahmed Reja and Syed Ahmad (Jamia Millia Islamia, India); Asaad AI-Salih (Jamia Millia Islamia University,

India)

3 A Method for Determining the Dimension of Planar Monol2ole Triangular Antenna

Aloysius Adya Pramudita (Unika Atmajaya Indonesia, Indonesia)

Design of a Cubesat Coml2uter Architecture using COTS Hardware for Terrestrial Thermal Imaging

4 Chandrasekhar Nagarajan (Manipal lnstitute of Technology & Parikshit Student Satellite Team, India);

Rodney D'souza and Sukumar Karumuri (Manipal University, India); Krishna Kinger (Manipal lnstitute of

Technology, Manipal University, India)

ix

Visual Information to enhance Time Difference of Arrival Based Acoustic Localisation 5

Riad Azzam, R (Cranfield University, United Kingdom)

6 Design and Iml2lementation of LDPC Coding Technigue on FPGA for DVB-S

Rita Purnamasari, Heroe Wijanto and Iswahyudi Hidayat (Telkom University, Indonesia)

Statistical Prol2erties Prol2osed for Blind Classification OFDM Modulation Scheme

7 Afief Dias Pambudi (Telkom University, Indonesia); Suhartono Tjondronegoro (Institut Teknologi Bandung,

Indonesia); Heroe Wijanto (Telkom University, Indonesia)

Novel Two Position Ground Alignment Technigue for Stral2down Inertial Navigation S�stems

8 Sri Ramya Bhamidipati (3rd year liT Bombay, India); Venugopal Reddy Bogala, Chandrasekhar RS and

Narayana Murthy Bhvs (Research Center Imarat, India)

Session III Satellite Mission Mustika Room

Multi-objectives Ol2timization of Earth Observation Micro-Satellite Design Using Particle Swarm

1 Robertus Triharjanto and Ridanto Eko Poetro (Institut Teknologi Bandung, Indonesia); Soewarto

Hardhienata (Indonesian National Institute for Aeronautics & Space (LAPAN), Indonesia)

2 ASIGN - Mission-Critical Visual Communications for Integrated Sl2ace Al2l2lications

Harald Skinnemoen (AnsuR Technologies, Norway)

liNUSAT-1: The 1st Indonesian Inter-Universit� Nano-Satellite for Research and Education

Tri K Priyambodo (Universitas Gadjah Mada, Indonesia); Agfianto Putra (Gadjah Mada University,

Indonesia); M. Asvial (University of Indonesia, Indonesia); Ridanto Eko Poetro (Institut Teknologi Bandung,

3 Indonesia); Gamantyo Hendrantoro (Sepuluh Nopember Institut of Technology, Indonesia); Endra

Pitowarno (EEPIS ITS, Indonesia); Gunawan Prabowo (Indonesian National Institute of Aeronotics and

Space, Indonesia); Arifin Nugroho (Institut Teknologi Telkom, Indonesia); Son Kuswadi (Electronics

Engineering Polytechnics Institute of Surabaya, Indonesia)

4 Multi-Mission Low Earth Orbit Eguatorial Satellite for Indonesian Regions

Eriko Nasemudin Nasser (National Institute of Aeronautics and Space, Indonesia)

The Develol2ment of Multi-band Eguatorial Orbiting POLSAR Satellite Sensors 5

Wolfgang Boerner (UIC Chicago, USA)

x

Session IV Satellite Technology Mustika Room

Attitude Control of Bias Momentum Micro Satellite Using Magnetic and Gravity Gradient Torgue

1 Rosza Madina and Muhammad Mukhayadi (National Institute of Aeronautics and Space, Indonesia); Udo

Renner (TU Berlin, Germany)

2 High Performance On-Board Processing and Storage for Satellite Remote Sensing Al2l2lications

Sharon Lim (ST Electronics - Satellite Systems, Singapore)

ADCS Reguirements of Lal2an-A3 Satellite Based on Image Geometry Analysis

3 Patria Rachman Hakim (Indonesian National Institute of Aeronautics and Space, Indonesia); Wahyudi Hasbi

(National Institute of Aeronautics & Space (LAPAN), Indonesia); A. Hadi Syafrudin (National Institute of

Aeronautics and Space, Indonesia)

Generic Study of Solar Radiation and Solar Wind Sailing

4 Harijono Djojodihardjo (Universiti Putra Malaysia & Faculty of Engineering, Malaysia); Ali Yousefian

(Research Assistant, Malaysia); Riyadh Ibraheem Ahmed (Universiti Putra Malaysia, Malaysia)

Session V UAV, Attitude & Control Mustika Room

Modular Trajectory L Path Following Controller Using Nonlinear Error Dynamics 1

Simon Schatz and Florian Holzapfel (Technische UniversiUit Munchen, Germany)

An Analysis on the Lift Generation for Coanda Micro Air Vehicles

2 Harijono Djojodihardjo (Universiti Putra Malaysia & Faculty of Engineering, Malaysia); Riyadh Ibraheem

Ahmed (Universiti Putra Malaysia, Malaysia); Ali Yousefian (Research Assistant, Malaysia)

Attitude Control of a Multicol2ter using L1 augmented Quaternion based Backstel2l2ing

3 Venkata Sravan Akkinapalli, Guillermo P. Falconi and Florian Holzapfel (Technische UniversiUit Munchen,

Germany)

Reference Command Shal2ing for Al2l2roximate Dynamic Inversion based Model Reference Adal2tive

4 Control

Maximilian Muhlegg, Philipp Niermeyer and Florian Holzapfel (Technische UniversiUit Munchen, Germany)

xi

Session VI Remote Sensing Science & Technology I Mustika Room

Wavelet Transform Based New InterQolation Technigue for Satellite Image Resolution Enhancement

1 Pejman Rasti and liris Li.isi (University of Tartu, Estonia); Hasan Demirel (Eastern Mediterranean University,

Turkey); Rudolf Kiefer and Gholamreza Anbarjafari ( lMS Lab, Institute of Technology, University of Tartu,

Estonia)

A Real-Time Monocular Vision-based Frontal Obstacle Detection and Avoidance for Low Cost UAVs in GPS

Denied Environment 2

Ashutosh Natraj (University of Oxford & IBM, United Kingdom); Suman Saha (Oxford Brookes University,

United Kingdom); Sonia Waharte (University of Oxford, United Kingdom)

Investigation of MIMO and SAR Performance on Several AQQlications of UWB GPR 3

Delphine Marpaung and Yilong Lu (Nanyang Technological University, Singapore)

4 Wireless Sensor Networks for Microclimate Telemonitoring using Zig Bee and WiFi

Firdaus Firdaus (Universitas Islam Indonesia, Indonesia)

Session VII Remote Sensing Science & Technology II Mustika Room

Multi-scale Voxel-based Algorithm for UAV-derived Point-clouds of ComQlex Surfaces 1

Christopher Gomez (University of Canterbury, New Zealand); Akira Kato (University of Chiba, Japan)

Utilizing QuadcoQter as LARS Image Platform To Determine the Paddy SQectral and Growth Parameter

2 Khairulazhar Zainuddin and Sharifah Norashikin Bohari (Universiti Teknologi MARA Perl is, Malaysia);

Noorzalianee Ghazali (Universiti Teknologi MARA, Malaysia); Mohamad Azril Che Aziz (Universiti Teknologi

Mara(UiTM)Perlis & UiTM, Malaysia); Abd Manan Samad (Universiti Teknologi MARA Malaysia, Malaysia)

The combined technigue of regional atmosQherically correction

3 Arnis Asmat and Wan Noni Afida Ab Manan (University of Technology MARA, Malaysia); Shattri Mansor

(University Putra Malaysia (UPM), Malaysia)

Evaluation of soil erosion Qotential of a hilly terrain using hYQsometry and E30 model

4 Nibedita Sinha (Kharagpur liT & liT Kharagpur, India); Debasis Deb and Khanindra Pathak ( liT Kharagpur,

India)

DeveloQment of transferable rule-sets for urban areas using QuickBird satellite imagery

5 Helmi Shafri (Universiti Putra Malaysia, Malaysia); Anahita Tathiri (University of Putra, Malaysia); Alireza

Hamedianfar (UPM, Malaysia)

An ImQroved Local Similarity Measure Estimation for Change Detection in Remote Sensing Images

6 Maha Shadaydeh (Computer and Automation Research Institute (MTA SZTAKI), Hungary); Tamas Sziranyi

(Computer and Automation Research Institute (MTA SZTAKI) & BME, Hungary)

xii

AUTHORS INDEX

NO AUTHORS PAGE NUMBER

1. A. Hadi Syafrudin 142

2. Abd Manan Samad 210

3. Afief Dias Pambudi 89

4. Agfianto Putra 114

5. Ahmed Reja 55

6. Akira Kato 205

7. Ali Yousefian 147, 164

8. Alireza Hamedianfar 229

9. Aloysius Adya Pramudita 63

10. Anahita Tathiri 229

11. Arifin Nugroho 114

12. Arnis Asmat 216

13. Asaad AI-Salih 55

14. Ashutosh Natraj 189

15. Chandrasekhar Nagarajan 67

16. Chandrasekhar RS 94

17. Christian Heise 26

18. Christopher Gomez 205

19. Debasis Deb 223

20. Deddy Amin 48

21. Delphine Marpaung 196

22. Endra Pitowarno 114

23. Eriko Nasemudin Nasser 48, 121

24. Firdaus Firdaus 200

25. Florian Holzapfel 20,26,34,39,157,170,179

26. Gamantyo Hendrantoro 114

27. Gholamreza Anbarjafari 185

28. Guillermo P. Falconi 20,26,170

29. Gunawan Prabowo 114

30. Harald Skinnemoen 12, 107

31. Harijono Djojodihardjo 147, 164

32. Hasan Demirel 185

33. Helmi Shafri 229

34. Heroe Wijanto 83,89

35. liris LOsi 185

36. Iswahyudi Hidayat 83

37. Khairulazhar Zainuddin 210

38. Khanindra Pathak 223

39. Krishna Kinger 67

40. Lothar Dalldorff 1

xiii

4l. M. Asvial 114

42. Maha Shadaydeh 234

43. Markus Hochstrasser 39

44. Matthias Bittner 34

45. Matthias Rieck 34

46. Maximilian Muhlegg 179

47. Maximilian Richter 34

48. Mohamad Azril (he Aziz 210

49. Muhammad Mukhayadi 132

50. Narayana Murthy Bhvs 94

5l. Nibedita Sinha 223

52. Noorzalianee Ghazali 210

53. Patria Rachman Hakim 142

54. Patrick Lauffs 39

55. Pejman Rasti 185

56. Philipp Niermeyer 179

57. Reinhard Reichel 1

58. Riad Azzam, R 77

59. Ridanto Eko Poetro 99, 114

60. Rita Purnamasari 83

6l. Riyadh Ibraheem Ahmed 147, 164

62. Robert Luckner 1

63. Robertus Triharjanto 99

64. Rodney D'souza 67

65. Rosza Madina 132

66. Rudolf Kiefer 185

67. Sharifah Norashikin Bohari 210

68. Sharon Lim 137

69. Shattri Mansor 216

70. Simon Schatz 157

7l. Soewarto Hardhienata 99

72. Son Kuswadi 114

73. Sonia Waharte 189

74. Sri Ramya Bhamidipati 94

75. Suhartono Tjondronegoro 89

76. Sukumar Karumuri 67

77. Suman Saha 189

78. Syed Ahmad 55

79. Tamas Sziranyi 234

80. Tri K Priyambodo 114

8l. Udo Renner 132

82. Venkata Sravan Akkinapalli 170

83. Venugopal Reddy Bogala 94

84. Wahyudi Hasbi 142

85. Wan Noni Afida Ab Manan 216

xiv

86. Widya Roza

87. Wolfgang Boerner

88. Yilong Lu

xv

48

127

196

TABLE OF CONTENTS

No Title Page Paper number Number

1 A Method for Determining the Dimension of Planar Monopole Triangular 63 1570027785

Antenna

2 A Real-Time Monocular Vision-based Frontal Obstacle Detection and 189 1569991641

Avoidance for Low Cost UAVs in GPS Denied Environment

3 A Utility Aircraft for Remote Sensing Missions with a High-Precision 1 1569989441

Automatic Flight Control System

4 ADCS Requirements of Lapan-A3 Satellite Based on Image Geometry 142 1569994089

Analysis

5 An Analysis on the Lift Generation for Coanda Micro Air Vehicles 164 1570004019

6 An Improved Local Similarity Measure Estimation for Change Detection in 234 1569990529

Remote Sensing Images

7 ASIGN - Mission-Critical Visual Communications for Integrated Space 107 1570029409

Applications

8 Attitude Control of a Multicopter using L1 augmented Quaternion based 170 1569986737

Backstepping

9 Attitude Control of Bias Momentum Micro Satellite Using Magnetic and 132 1570023361

Gravity Gradient Torque

10 Design and Implementation of LDPC Coding Technique on FPGA for DVB-S 83 1570043619

11 Design And Implementation of Payload Data Handling Based on Field 48 1570027723

Programmable Gate Array

12 Design of a Cubesat Computer Architecture using COTS Hardware for 67 1569990115

Terrestrial Thermal Imaging

13 Development of transferable rule-sets for urban areas using QuickBird 229 1570010041

satellite imagery

14 Evaluation of soil erosion potential of a hilly terrain using hypsometry and 223 1570020737

E30 model

15 Generic Study of Solar Radiation and Solar Wind Sailing 147 1570003851

16 Hexacopter Outdoor Flight Test Results of an Extended State Observer 26 1569986265

based Controller

17 High Performance On-Board Processing and Storage for Satellite Remote 137 1570027709

Sensing Applications

18 liNUSAT-l: The 1st Indonesian Inter-University Nano-Satellite for 114 1570005783

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29 Reference Command Shaping for Approximate Dynamic Inversion based 179 1569987075

Model Reference Adaptive Control

30 Statistical Properties Proposed for Blind Classification O FDM Modulation 89 1570032617

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31 The combined technique of regional atmospherically correction 216 1570018331

32 The Development of Multi-band Equatorial Orbiting PO LSAR Satellite 127 1570000661

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35 Visual Information to enhance Time Difference of Arrival Based Acoustic 77 1570028837

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36 Wavelet Transform Based New Interpolation Technique for Satellite 185 1570030905

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37 Wireless Sensor Networks for Microclimate Telemonitoring using ZigBee 200 1570030797

and WiFi

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Wireless Sensor Networks for Microclimate Telemonitoring using ZigBee and WiFi

Firdaus Departmen of Electrical Engineering

Universitas Islam Indonesia Yogyakarta, Indonesia

firdaus@uii.ac.id

Ahriman, Rois Akbar, Eko Nugroho Departmen of Electrical Engineering

Universitas Islam Indonesia Yogyakarta, Indonesia

Abstract—Wireless Sensor Network is increasingly popular in the field of microclimate monitoring due to its promising capability. Wireless Sensor Network using many wireless communication protocols, such as Bluetooth, ZigBee, ultra wideband, and WiFi. WiFi has many advantages, i.e high data rate and long range distances, but it requires a high power. ZigBee uses less power, but it offers low data rate and short range distances. This paper presents the application of ZigBee and WiFi networks for microclimate monitoring. Data of air temperature and humidity are collected using ZigBee-WSN and then the data are transmitted from the observed area to the monitoring center using WiFi transceiver. Air temperature sensors have average error 1.9% and humidity sensors have average error 3.8%. This system needs ZigBee – WiFi interface that convert the data format from ZigBee protocol into TCP/IP protocol. Maximum distance communication of ZigBee protocol is ± 200m in the outdoor area with many obstacles. The interface system can communicate properly when the baud rate is 9600bps.

Keywords—zigbee; WiFi; interface; monitoring; micro-climate

I. INTRODUCTION Wireless Sensor Network (WSN) is increasingly popular in

the field of microclimate monitoring due to its promising capability.[1,2] Microclimate is the climate of a very small or restricted area such as a town, forest or garden, especially when this differs from the climate of the surrounding area. The main measured parameters are air temperature and humidity. Wireless Sensor Network using many wireless communication protocols, such as Bluetooth [3], ZigBee[4], UWB (ultra wideband) [5], and WiFi[6]. Each protocol has its own characteristics. UWB is designed for low-power, short-range and high speed. Operational range for UWB can reach 10 meters based on the IEEE 802.15.3 standard[7]. WiFi is based on the IEEE 802.11 specification. The data rate can reach 11 Mbps with distances up to 100 meters can be affordable and requires a great power[8]. ZigBee is a technology with low data rate, low cost, and small power used. ZigBee is classified to IEEE 802.15.4 standard. Data rates can reach 250kbps, the distance range between 10m – 70m [9].

The advantages of WiFi are high data rate and long range distances, however it requires a great current that is equal to 400mA on standby. ZigBee uses less current that is equal to

30mA during standby, but it result low data rate and short range distances. This system combine the ZigBee communication standard with WiFi communication standards in a telemonitoring system.

IEEE 802.15.4 standard defines that MAC layer has 4 basic frame: beacon frame, data frame, acknowledgment, and command frames. Beacon frame is used by a coordinator to transmit beacons. Data frame is used to store all data sent. Acknowledgment frame is used to confirm that data has received successfully, and MAC command frame is used to set up and configure the client. The PHY layer consists of 32 bits preamble which used to synchronize the system. Start of frame consists of 8 bits which used as a marker the end of the preamble. Frame length (8 bits) is used to explain the length of the PHY service data unit (PSDU), and MPOU ( <127 bytes) is used to handle and manage data received from the previous layer [10].

WiFi (802.11) data packets consist of application layer protocol that is used to provide the access to TCP/IP services. These protocols include the dynamic host configuration protocol (DHCP), domain name system (DNS), and hypertext transfer protocol (HTTP). Inter-host communication layer choose connection-oriented or connectionless broadcast and protocols at this layer are the Transmission Control Protocol (TCP) and User Datagram Protocol (UDP). Internetwork layer protocol is responsible for routing and encapsulation of data packets into IP packets and protocols that work at this layer are the Internet Protocol (IP), Address Resolution Protocol (ARP), Internet Control Message Protocol (ICMP), and Internet Group Management Protocol (IGMP)[11]. Network interface layer protocol is responsible for laying the network frames over the used media. TCP/IP can work with many transport technologies, ranging from transport technologies in the LAN (such as Ethernet and Token Ring), MAN and WAN (such as dial-up modems that run on top of the Public Switched Telephone Network (PSTN), Integrated Services Digital network (ISDN), and Asynchronous Transfer Mode (ATM)).

II. SYSTEM DESIGN The design of ZigBee and WiFi networks for microclimate telemonitoring is divided into three parts. The first part is the design of WSN using ZigBee protocol (Z-WSN) that consist

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five sensor nodes, the second part is the design of ZigBee and WiFi interface (Z2W), and the third part is the design of WiFi transceiver (W-TRx). The component of this monitoring system can be see at figure 1. Data of air temperature and humidity are collected using ZigBee-WSN and then the data are transmitted from the observed area to the monitoring center using WiFi transceiver. This system needs ZigBee – WiFi interface that convert the data format from ZigBee protocol into TCP/IP protocol.

Figure 1. Microclimate telemonitoring system using ZigBee

and WiFi networks

Z-WSN consist many sensor nodes that have function to collect the data (air temperature and humidity) from environment. Each sensor node consists of microcontroller as central processing unit, sensors, zigbee transceiver[12], and power supply using solar cells (Figure 2). Sensors convert the physical value of air temperature and humidity to electric signal then this signal are processed by microcontroller, and zigbee transceiver is used to communicate with other sensor nodes. The sensor nodes consist of an LM35DZ[13] temperature sensor, and a humidity sensor HSM 20-G[14].

Figure 2. Block diagram and the device of sensor node

in Z-WSN

There are 5 sensor nodes are used in this system, 1 sensor node as coordinator node (node-A) and 4 sensor nodes as member nodes (node-B, node-C, node-D, node-E). The topology of this network shows in figure 3. The development of software section within microcontroller for each node within Z-WSN can be saw in figure 4, it will contain the procedure in transmitting and receiving data. Figure 5 shows the procedure of processing data in coordinator node, this

node collect the data from others nodes and then sent the data to ZigBee and WiFi interface.

Figure 3. Topology of ZigBee-Wireless Sensor Networks

Figure 4. Flow chart of data collection using Xbee Pro2SB

Figure 5. Flow chart of data processing in coordinator node

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The second part is ZigBee and WiFi interface which convert the data from ZigBee protocol to TCP/IP protocol and applies vice versa. Block diagram of Z2W can be seen in Figure 5.

Figure 5. Block diagram and the device of zigbee and WiFi

networks interface for telemonitoring

ZigBee-WiFi interface consists of several parts: ZigBee transceiver, WiFi transceiver, serial interface circuit port (DB9), and a power supply. WiFi transceiver using WIZnet 110SR. MAX232 IC is used as a voltage level converter between WIZnet and XBee PRO. COM port on WIZnet 110SR can’t be connected directly to the microcontroller, it is required the driver to change the RS-232 signal voltage to TTL voltage levels. WIZnet configuration, that consist of many activities; setting the IP WIZnet, a port on the network, speed, data bits, parity, stop bits and flow in the series, is used to synchronize the microcontroller and WIZnet[15].

The flowchart of zigbee-WiFi interface when receiving data from the ZigBee Transceiver and send data to the Wi-Fi transceiver can be seen in Figure 6.

III. RESULT AND DISCUSSION This section will provide validation of the system that focused on investigation of sensor reading, transmitting and receiving performances. This section will be separated into several parts such as sensor testing, validation of ZigBee transmitting distances, and test of ZigBee and WiFi interface.

A. Test of Sensor Reading

There are 3 sensors that used in this test (sensor-1, sensor-2, and sensor-3). LM35DZ temperature sensor has the characteristic whereby every degree displayed is represented by the value of the output voltage of 10mV. The average of percentage error is 1.91% at sensor-1 and sensor-2, 2.01% at sensor-3. The detail of test results can be seen in Table 1.

Figure 6. Flow diagram of ZigBee to WiFi interface

Table 1. Results of temperature sensor testing

Temperature by Sensor (oC) Thermometer (oC) Sensor-1 Sensor- 2 Sensor-3

21.23 20.66 20.76 21 22.48 21.14 21.70 22 23.46 22.58 22.65 23 25.90 25.46 25.48 25 27.37 26.42 26.89 27 28.35 27.38 27.60 28

Humidity sensor (HSM 20-G) test is done by comparing the value of the humidity sensor readings with hygrometer readings. To get the value of different humidity, the test is done at different times and locations. Tests are carried out since noon, night and morning, while test locations are indoor and outdoor areas. The average error percentage of sensor readings are 6.5% at sensor-1, 1.54% at sensor-2 and 3.53% at sensor-3. The test results of humidity sensor can be seen in Table 2.

Table 2. Results of humidity sensor testing

Humidity by Sensor (%) Higrometer (%) Sensor-1 Sensor-2 Sensor-3

61.63 55.89 60.76 58 63.76 59.42 62.52 60 66.78 61.93 64.80 62 71.18 67.67 69.11 66 74.44 71.60 73.54 70 76.62 72.33 74.52 72

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B. Test of Z-WSN Transmitting Distance

The first step in this test is make point to point communication between node-A and node-B in outdoor environment with obstacles consideration, from this activity we can know that maximum distance of ZigBee transmitting is ±200m. Then, we built a network that consist of 5 nodes in mesh topology (figure 3). The distances between nodes show in figure 7 and table 3.

Figure 7. Node location on Z-WSN

Table 3. The distance between nodes in Z-WSN

Between node Distance (m) A and B 200 B and C 195 C and D 206 D and E 215 E and A 204 A and D 353 B and E 216 A and C 383 A and D 353

Node-B, node-C, node-D, and node-E sent the data through the mesh network to coordinator node. Node-A as a coordinator receives or collects the data from others nodes and there are no error. When one or two of the nodes (B/C/D/E) is down or off, the network will reroute the nodes connection, so coordinator node still receives the data from other nodes that still active. For the example, if node B is off, then node-A still records the data from node-C, node-D and node-E. When node B and node C are off, node A still receive the data from node D and node E.

When there are three sensor nodes and they form an equilateral triangle, the covered area is 17320.5 m2. When

there are four sensor nodes and they form two equilateral triangles, so the wide area will be doubled.

C. Test of ZigBee and WiFi Interface

ZigBee and WiFi Interface connect to the coordinator node (node-A). The test determine the capabilities and reliability of the system that has been created. Testing was conducted on the testing of the power supply circuit, and convert process from ZigBee protocol to WiFi protocol. Testing of power supply is done by measuring the output voltage (Vout) of the circuit that has been made. 5 volt power supply is used to supply the minimum system ATMega8, while power supply that used to supply XBee PROis 3,3 volt. The resulting of output voltage between 4.95 - 5.03 volts and 3.04 - 3.04 volts.

Testing of data connection from the ZigBee node to the WiFi node aimed to determine the stability of data transmission. This testing is done up to 12 hours. Based on the results of the testing that has been done, it was concluded that all devices on the system is on and functioning properly.

When the baudrate of zigbee and wifi interface be set at 4800 bps, the data which sent from the ZigBee transceiver can be received by monitoring center, but the received data does not match the data sent (table 4). During the experiments, when baudrate set at 9600 bps we can see that the received data is accordance with the sent data (table 4). While baudrate at 19200 bps, data transmission has an error.

Table 4. The sent and received data of zigbee and wifi interface

Baudrate = 9600 bps ZigBee to WiFi WiFi to ZigBee

Sent Received Sent Received 0 0 0 000

94 94 3 003 267 267 8 008 376 376 12 012 502 502 33 033 654 654 567 567

Baudrate = 4800 bps ZigBee to WiFi WiFi to ZigBee

Sent Received Sent Received 0 j Ø 0 000

299 EEjo 299 000 419 IEJo 419 000 582 - 582 000 790 EJ Ø 790 000 654 IJ Ø 654 000

Baudrate = 19200 bps ZigBee to WiFi WiFi to ZigBee

Sent Received Sent Received 0 0 0 000

36 IIP 3 000 78 IIP 8 000

145 IIP 12 000 256 IIP 33 000 345 IIP 567 000

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IV. CONCLUSION From the testing that has been done, it can be concluded as

follows. Network which has been designed is work properly, where ZigBee Wireless Sensor Networks can collect the data of air temperature and humidity from certain area, air temperature sensors have error 1.9% and humidity sensors have error 3.8%. Using mesh topology, when one of the node is off, then the others nodes can still sent the data. Data from Z-WSN then convert to TCP/IP format using ZigBee and WiFi interface. Finally, the data sent from monitored area to the monitoring center using WiFi transceiver based on point to point communication. Maximum distance communication of ZigBee protocol is ± 200m in the outdoor area with many obstacles. The zigbee and wifi interface can communicate properly when the baud rate is 9600.

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