Data Quality Evaluation & Orbit Identification from SCATTEROMETER Data Products Using Modern Computing Techniques By:- Mudit J Dholakia (14MTPOS001) Under the guidance of Dr. C K Bhensdadia(Head, Department of Computer Engineering, DDU-Nadiad) Mrs. Anuja Sharma (Scientist-’SF’, IAQD/SIPA/SPDCG/SAC/Ahmedabad)
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Data quality evaluation & orbit identification from scatterometer
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Data Quality Evaluation & Orbit Identification from SCATTEROMETER Data Products Using
Modern Computing Techniques
By:- Mudit J Dholakia (14MTPOS001)
Under the guidance of
Dr. C K Bhensdadia(Head, Department of Computer Engineering, DDU-Nadiad)
Generalised Reference for ellipsoidal geometries (X,Y,Z)
3-D computations are highly complex and requires heavy resource
IBEX[13] Interstellar Boundary Explorer High efficiency
Orbit change detection without scientific backing is not reliable
OKID[14] Orbit identification Keysfor near surface windsAccuracy is best of its kind
Bigger the geometry higher the computation.
VirtulMeteorology[15] Automated accomodation of orbits
Used for scientific calibration
Not feasible fo real time evaluation
Presentation Roadmap
1
Introduction
2
Problem
3
LiteratureSurvey
4
Proposal
Proposal
• Orbit Identification(OI)• Fuzzy Logic based OI
• Pattern based OI
• DQE using flag bit-4• A neural network based approach
Fuzzy Logic based Orbit Identification
Motivation for approach 1: Fuzzy
• OAT Derived Match data• Time
• Latitude
• Longitude
• Attitude
• Roll
• Pich
• Yaw
• Position(x,y,z)
• Velocity(x,y,z)
Motivation for approach 1: Fuzzy
Motivation for approach 1: Fuzzy
Orbit Identification using fuzzy logic[18]
Boon of the approach
Consideration of South pole crossing
Pattern based Orbit Identification
Overview
• Pattern Based Identification is used for automatic retrieval of orbits from SAR images depending upon contents of images known as features (i.e. a black chirp in the proposed case).
• Scanning consideration describes the process of accessing the interested patterns.
• Simplicity of Action is the outcome of the proposal.
Analysis of Signal Images
Proposal of Identification• A normal C program with I/O & file
operations.
• Scanning Geometry• Pixels in beams
• Number of scans
• Asymptotic Complexity• O(m*n)
• m is number of scans
• n is number of pixels per scan
Flag Based DQE(Neural Network Based DQE)
Globe according to flag bit-4
A grid of 2 classes
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Presentation Roadmap
1
Introduction
2
Problem
3
LiteratureSurvey
4
Proposal
5
Implementation
Implementation
• Prerequisites
• Experiment-1 • Fuzzy logic based OI
• Experiment-2• Pattern Based OI
• Experiment-3• Flag DQE using Artificial Neural
Network
Prerequisites
• Matlab R2013a
• JDK+Netbeans
• C editor & compiler
• Jasper Engine
• HDFView
Experiment-1Fuzzy Logic based Orbit Identification
• If time1 then orbit1
• If time2 then orbit2
• If time3 then orbit3
• If time4 then orbit4
• If time5 then orbit5
*Using north pole crossing time
Experiment-1Fuzzy Logic based Orbit Identification
Experiment-1Fuzzy Logic based Orbit Identification
• If time1 then orbit1
• If time2 then orbit2
*Using equator crossing time
Experiment-1Fuzzy Logic based Orbit Identification
Experiment-1Fuzzy Logic based Orbit Identification
• If time1 then orbit1
• If time2 then orbit2
• If time3 then orbit3
*Using south pole crossing time
Experiment-1Fuzzy Logic based Orbit Identification
Experiment-2Pattern based Orbit Identification
Sensor Signal Data Orbit Count ProgramResultant Fine-tuned
Orbit Statistics
Experiment-3Neural Network Based DQE
Presentation Roadmap
1
Introduction
2
Problem
3
Literature Survey
4
Proposal
5Implementation
5
Results
Results
• Pattern based Orbit Identification
• Neural Network based DQE
• Retrospective GRID-GUI
• Added clarity to reports
Pattern Based Orbit Identification Results
Neural Network based DQEResults
Retrospective GRID-UI
Retrospective GRID-UI
Clarity in Reports
Clarity in Reports
Clarity in binning
Clarity in binning
Overall System Overview
Statistics
Presentation Roadmap
1
Introduction
2
Problem
3
Literature Survey
4
Proposal
5Implementation
5
Results
Conclusion
Conclusion
• Conclusion
• Future work
• Bibliography
Conclusion
• A Fuzzy Logic(FL) based orbit identification(OI) has been proposed in this work. To select theattributes a preprocessed data set of Orbit Attitude Records are selected assuming extraction ofLevel-0 and some processing steps have already been performed. Selection of time and latitudehas been justified using Geo-mathematical criteria. Then a short introduction to fuzzy systems isgiven and using that approach the idea is implemented using matlab. This work has made a markin Data Quality Evaluation Modeling. This work is useful for the researchers to develop themodern terrain clustering systems.
• In traditional systems this redundancy leads to waste of computational efforts. Instead, thisapproach provides past knowledge, using which the new data can be segmented as well asanalyzed (using further integration) and improvements to the upcoming observation systems canbe carried-out. Moreover, it also reduces modeling complexity to compute the correlationbetween two images based on geometry, i.e. existing image of DQE and the image which iscurrently computed. It also improves the speed of a spatial data analysis system. Using secondapproach also orbit identification task has been implemented with modeling complexity of O(n).This makes a clear sense to computational geo-informatics about the patterns which areimportant aspect of consideration which was neglected earlier. Binning also improves theanalytical standard for the better understanding of anomalies in data , indirectly in sensors.
Conclusion
• At the end work has been concluded with the initial startup for futurework, i.e. Neural Network based DQE. The Neural Network basedapproach has been tested on randomly selected data products fromthe source NRSC even though surveying the current system with bestaccuracy. Making some more efforts towards the highest accuracythis approach also can show at least a technique other thanconventional technique of flag based DQE . Concluding with theretrospective DQE implementation to bridge the gap described inproblem definition this work encourages many researchers to workfor DQE and OI using modern computing techniques.
Future Work
• General Model Development
• Applicability to wider scope can be designed
• No parallel processes have been defined, thus work can be initiatedfor such faster models
• GRID_UI needs many improvements for the final application, i.e.deliverable
• More powerful soft computing with highest accuracy can be used forbetterment of DQE system.
Paper:1
A Novel Approach of Orbit Identification from Level-0 Data based on Level-1B convention for Scatterometer
using Fuzzy LogicMudit J Dholakia, Anuja Sharma, Dr. C. K. Bhensdadia
XPLORE COMPLIANT ISBN :- 978-1-4673-7807-9CD ISBN:- 978-1-4673-7805-5
PRINT ISBN :- 978-1-4673-7806-2
IEEE INTERNATIONAL CONFERENCE ON SYSTEMS AND CONTROL (ISCO)KARPAGAM COLLEGE OF ENGINEERING ,COIMBATORE,TAMIL NADU
Paper:2
Pattern Based Orbit Identification for SCATTEROMETER Level-0 Signal Images
Mudit J Dholakia, Anuja Sharma, Dr. C. K. Bhensdadia
Journal title: Procedia Computer Science
DOI information: 10.1016/j.procs.2016.03.049
INTERNATIONAL CONFERENCE ON CLOUD COMPUTING AND VIRTUALIZATION (ICCCV)
THAKUR COLLEGE OF ENGINEERING,KANDIVALI,MUMBAI,MAHARASHTRA
IN ASSOCIATION WITH ELSEVIER PROCEEDIA COMPUTER SCIENCE ,ELSEVIER B.V. AMSTERDAM, NETHERLANDS
Paper:3
Analytical Approach for identification of orbits from
SCATTEROMETER Level-0 Noise ImagesMudit J Dholakia, Anuja Sharma, Dr. C. K. Bhensdadia
International Journal of Applied Information Systems (IJAIS) – ISSN : 2249-086803.049
INTERNATIONAL CONFERENCE ON CLOUD COMPUTING AND VIRTUALIZATION (ICCCV)
THAKUR COLLEGE OF ENGINEERING,KANDIVALI,MUMBAI,MAHARASHTRA
IN ASSOCIATION WITH ELSEVIER PROCEEDIA COMPUTER SCIENCE ,ELSEVIER B.V. AMSTERDAM, NETHERLANDS
Paper:4
Pattern Based Orbit Identification for SCATTEROMETER Level-0 Signal Echo Window Images
Mudit J Dholakia, Anuja Sharma, Dr. C. K. Bhensdadia
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