Explains newly found geometric features of Bezier curves and surfaces called "rib and fan.
- Author: Joo-Haeng Lee
- Affiliation: ETRI
- Date: 2007-12-07
Simulation of segregated flow over the 2 d cylinder using star ccm+Burak Turhan
In this thesis numerical simulation for classical case of flow over a cylinder is accomplished for 2D models using commercial CFD code Star CCM+ with k-ϵ model approach. The results are validated by comparing the Drag coefficients to the previously published data. The simulation is carried out to for Reynolds number 3900 to investigate the turbulence modeling on separation from curved surfaces of two different sizes of a circular cylinder, a cylinder with triangular cross section and a rectangular cross section. Investigation of different turbulence models and Mesh convergence is carried out.
The investigation of the turbulence model of the circular cylinder is carried out by the drag coefficient obtained by four different turbulence models such as K-Epsilon Turbulence, K-Omega Turbulence, Reynolds Stress Turbulence and Spalart-Allmaras Turbulence. Drag coefficient found out by different turbulence model is compared with the experimental value of a previously published data. The Mesh Convergence have been carried out by implementing different base mesh size in a decreasing order and the convergence is obtained when the drag coefficient becomes constant
Simulation of segregated flow over the 2 d cylinder using star ccm+Burak Turhan
In this thesis numerical simulation for classical case of flow over a cylinder is accomplished for 2D models using commercial CFD code Star CCM+ with k-ϵ model approach. The results are validated by comparing the Drag coefficients to the previously published data. The simulation is carried out to for Reynolds number 3900 to investigate the turbulence modeling on separation from curved surfaces of two different sizes of a circular cylinder, a cylinder with triangular cross section and a rectangular cross section. Investigation of different turbulence models and Mesh convergence is carried out.
The investigation of the turbulence model of the circular cylinder is carried out by the drag coefficient obtained by four different turbulence models such as K-Epsilon Turbulence, K-Omega Turbulence, Reynolds Stress Turbulence and Spalart-Allmaras Turbulence. Drag coefficient found out by different turbulence model is compared with the experimental value of a previously published data. The Mesh Convergence have been carried out by implementing different base mesh size in a decreasing order and the convergence is obtained when the drag coefficient becomes constant
Horizontal axis wind turbine blade- 1way FSI analysisVishnu R
Combination of CFD and FEA analyses to assess the mechanical response of a wind turbine blade spinning clockwise as a consequence of wind blowing along the -z direction
DESIGN AND ANALYSIS OF MULTI- STAGE STEAM TURBINE BLADE AND SHAFT ASSEMBLYIjripublishers Ijri
The blades are designed in such a way as to produce maximum rotational energy by directing the flow of the steam along
its surface. The blades are made at specific angles in order to incorporate the net flow of steam over it in its favor. The
blades may be of stationary or fixed and rotary or moving or types, and Shaft designed to work in extreme conditions,
hear it has to bear the temperature which is coming from the steam and loads(weight and centrifugal force) of the blades
assembly and other assembly parts.
The aim of the project is to reduce maintenance, product cost and improving quality / life.
Initially literature survey will be done to understand rectification methodology and approach.
3D models of blades set’s shaft will be prepared according to C.M.M data.
Fluid Structural Modal Coupled Numerical Investigation of Transonic Flutterin...IJERA Editor
Flutter is an unstable oscillation which can lead to destruction. Flutter can occur on fixed surfaces, such as blades, wing or the stabilizer. By self-excited aeroelastic instability, flutter can lead to mechanical or structural failure of aircraft engine blades. The modern engines have been designed with increased pressure ratio and reduced weight in order to improve aerodynamic efficiency, resulting in severe aeroelastic problems. Particularly flutter in axial compressors with transonic flow can be characterized by a number of aerodynamic nonlinear effects such as shock boundary layer interaction, rotating stall, and tip vortex instability. Rotating blades operating under high centrifugal forces may also encounter structural nonlinearities due to friction damping and large deformations. In the future work a standard axial flow compressor blade will be taken for analysis, both Subsonic and Transonic range are taken for analysis. Fluid and Structure are two different domains which will be coupled by full system coupling technique to predict the fluttering effect on the compressor blade. ANSYS is a commercial simulation tool, which will be deployed in this work to perform FSI (Fluid Structure Interaction) and FSI coupled Modal to predict the flutter in the compressor blades
Fluid Structural Modal Coupled Numerical Investigation of Transonic Flutterin...IJERA Editor
Flutter is an unstable oscillation which can lead to destruction. Flutter can occur on fixed surfaces, such as blades, wing or the stabilizer. By self-excited aeroelastic instability, flutter can lead to mechanical or structural failure of aircraft engine blades. The modern engines have been designed with increased pressure ratio and reduced weight in order to improve aerodynamic efficiency, resulting in severe aeroelastic problems. Particularly flutter in axial compressors with transonic flow can be characterized by a number of aerodynamic nonlinear effects such as shock boundary layer interaction, rotating stall, and tip vortex instability. Rotating blades operating under high centrifugal forces may also encounter structural nonlinearities due to friction damping and large deformations. In the future work a standard axial flow compressor blade will be taken for analysis, both Subsonic and Transonic range are taken for analysis. Fluid and Structure are two different domains which will be coupled by full system coupling technique to predict the fluttering effect on the compressor blade. ANSYS is a commercial simulation tool, which will be deployed in this work to perform FSI (Fluid Structure Interaction) and FSI coupled Modal to predict the flutter in the compressor blades
Improving the Hydraulic Efficiency of Centrifugal Pumps through Computational...IJERA Editor
The design and optimization of turbo machine impellers such as those in pumps and turbines is a highly complicated task due to the complex three-dimensional shape of the impeller blades and surrounding devices. Small differences in geometry can lead to significant changes in the performance of these machines. We report here an efficient numerical technique that automatically optimizes the geometry of these blades for maximum performance. The technique combines, mathematical modeling of the impeller blades using non-uniform rational B-spline (NURBS), Computational fluid dynamics (CFD) with Geometry Parameterizations in turbulent flow simulation and the Globalized and bounded Nelder-Mead (GBNM) algorithm in geometry optimization.
A very private, introductory notes on reinforcement learning.
Focusing to understand DQN by Google DeepMind.
Mainly based on the nice article
"DEMYSTIFYING DEEP REINFORCEMENT LEARNING"by Tambet Matiisen on
http://neuro.cs.ut.ee/demystifying-deep-reinforcement-learning/
Horizontal axis wind turbine blade- 1way FSI analysisVishnu R
Combination of CFD and FEA analyses to assess the mechanical response of a wind turbine blade spinning clockwise as a consequence of wind blowing along the -z direction
DESIGN AND ANALYSIS OF MULTI- STAGE STEAM TURBINE BLADE AND SHAFT ASSEMBLYIjripublishers Ijri
The blades are designed in such a way as to produce maximum rotational energy by directing the flow of the steam along
its surface. The blades are made at specific angles in order to incorporate the net flow of steam over it in its favor. The
blades may be of stationary or fixed and rotary or moving or types, and Shaft designed to work in extreme conditions,
hear it has to bear the temperature which is coming from the steam and loads(weight and centrifugal force) of the blades
assembly and other assembly parts.
The aim of the project is to reduce maintenance, product cost and improving quality / life.
Initially literature survey will be done to understand rectification methodology and approach.
3D models of blades set’s shaft will be prepared according to C.M.M data.
Fluid Structural Modal Coupled Numerical Investigation of Transonic Flutterin...IJERA Editor
Flutter is an unstable oscillation which can lead to destruction. Flutter can occur on fixed surfaces, such as blades, wing or the stabilizer. By self-excited aeroelastic instability, flutter can lead to mechanical or structural failure of aircraft engine blades. The modern engines have been designed with increased pressure ratio and reduced weight in order to improve aerodynamic efficiency, resulting in severe aeroelastic problems. Particularly flutter in axial compressors with transonic flow can be characterized by a number of aerodynamic nonlinear effects such as shock boundary layer interaction, rotating stall, and tip vortex instability. Rotating blades operating under high centrifugal forces may also encounter structural nonlinearities due to friction damping and large deformations. In the future work a standard axial flow compressor blade will be taken for analysis, both Subsonic and Transonic range are taken for analysis. Fluid and Structure are two different domains which will be coupled by full system coupling technique to predict the fluttering effect on the compressor blade. ANSYS is a commercial simulation tool, which will be deployed in this work to perform FSI (Fluid Structure Interaction) and FSI coupled Modal to predict the flutter in the compressor blades
Fluid Structural Modal Coupled Numerical Investigation of Transonic Flutterin...IJERA Editor
Flutter is an unstable oscillation which can lead to destruction. Flutter can occur on fixed surfaces, such as blades, wing or the stabilizer. By self-excited aeroelastic instability, flutter can lead to mechanical or structural failure of aircraft engine blades. The modern engines have been designed with increased pressure ratio and reduced weight in order to improve aerodynamic efficiency, resulting in severe aeroelastic problems. Particularly flutter in axial compressors with transonic flow can be characterized by a number of aerodynamic nonlinear effects such as shock boundary layer interaction, rotating stall, and tip vortex instability. Rotating blades operating under high centrifugal forces may also encounter structural nonlinearities due to friction damping and large deformations. In the future work a standard axial flow compressor blade will be taken for analysis, both Subsonic and Transonic range are taken for analysis. Fluid and Structure are two different domains which will be coupled by full system coupling technique to predict the fluttering effect on the compressor blade. ANSYS is a commercial simulation tool, which will be deployed in this work to perform FSI (Fluid Structure Interaction) and FSI coupled Modal to predict the flutter in the compressor blades
Improving the Hydraulic Efficiency of Centrifugal Pumps through Computational...IJERA Editor
The design and optimization of turbo machine impellers such as those in pumps and turbines is a highly complicated task due to the complex three-dimensional shape of the impeller blades and surrounding devices. Small differences in geometry can lead to significant changes in the performance of these machines. We report here an efficient numerical technique that automatically optimizes the geometry of these blades for maximum performance. The technique combines, mathematical modeling of the impeller blades using non-uniform rational B-spline (NURBS), Computational fluid dynamics (CFD) with Geometry Parameterizations in turbulent flow simulation and the Globalized and bounded Nelder-Mead (GBNM) algorithm in geometry optimization.
A very private, introductory notes on reinforcement learning.
Focusing to understand DQN by Google DeepMind.
Mainly based on the nice article
"DEMYSTIFYING DEEP REINFORCEMENT LEARNING"by Tambet Matiisen on
http://neuro.cs.ut.ee/demystifying-deep-reinforcement-learning/
Spatial AR: Toward Augmentation of Ambient and Effective Interaction ChannelJoo-Haeng Lee
기존의 모바일 증강현실 기술은 실세계와 가상세계를 연결하는 새로운 상호작용 채널을 제공하고자 하지만 장치 의존성 면에서 상호작용을 제약하는 태생적인 한계를 보이고 있다. 프로젝터를 사용하여 정보, 인터페이스, 콘텐츠를 실세계 사물과 그 주변에 직접 투사하여 증강하고자 하는 공간증강현실은 이러한 기존의 모바일 증강현실이 갖는 문제점을 해결하고자 한다. 특히, 오감과 물리법칙에 기반한 실세계 상호작용을 가능한 그대로 유지하면서 새로운 인터액션 채널을 제공하여 실질적인 증강의 효과를 주고자 한다. 이러한 증강 상호작용은 실사물을 손으로 직접 만지며 작업하는 예술가와 노약자들에게도 도움을 줄 수 있어야 한다. 본 슬라이드에서는 위의 언급을 시각적으로 표현하고 있다.
New geometric interpretation and analytic solution for quadrilateral reconstr...Joo-Haeng Lee
Poster presentation for ICPR 2014 paper.
Title: New geometric interpretation and analytic solution for quadrilateral reconstruction
Author: Joo-Haeng Lee (ETRI)
New geometric interpretation and analytic solution for quadrilateral reconstr...Joo-Haeng Lee
Accepted as poster presentation for ICPR 2014, Stockholm, Sweden on August 24~28, 2014.
[Revised Version]
Title: New geometric interpretation and analytic solution for quadrilateral reconstruction
Author: Joo-Haeng Lee
Affiliation: Human-Robot Interaction Research Team, ETRI, KOREA
Abstract:
A new geometric framework, called generalized coupled line camera (GCLC), is proposed to derive an analytic solution to reconstruct an unknown scene quadrilateral and the relevant projective structure from a single or multiple image quadrilaterals. We extend the previous approach developed for rectangle to handle arbitrary scene quadrilaterals. First, we generalize a single line camera by removing the centering constraint that the principal axis should bisect a scene line. Then, we couple a pair of generalized line cameras to model a frustum with a quadrilateral base. Finally, we show that the scene quadrilateral and the center of projection can be analytically reconstructed from a single view when prior knowledge on the quadrilateral is available. A completely unknown quadrilateral can be reconstructed from four views through non-linear optimization. We also describe a improved method to handle an off-centered case by geometrically inferring a centered proxy quadrilateral, which accelerates a reconstruction process without relying on homography. The proposed method is easy to implement since each step is expressed as a simple analytic equation. We present the experimental results on real and synthetic examples.
[Submitted Version]
Title: Generalized Coupled Line Cameras and Application in Quadrilateral Reconstruction
Abstract:
Coupled line camera (CLC) provides a geometric framework to derive an analytic solution to reconstruct an unknown scene rectangle and the relevant projective structure from a single image quadrilateral. We extend this approach as generalized coupled line camera (GCLC) to handle a scene quadrilateral. First, we generalize a single line camera by removing the centering constraint that the principal axis should bisect a scene line. Then, we couple a pair of generalized line cameras to model a frustum with a quadrilateral base. Finally, we show that the scene quadrilateral and the center of projection can be analytically reconstructed from a single view when prior knowledge on the quadrilateral is available. ...
화홍문 사진 모음 및 편액에 대한 CLC 기반의 사각형 복원 (An Application of CLC on a framed picture ...Joo-Haeng Lee
수원 화성 화홍문 편액에 선분카메라쌍 (CLC) 기반의 사각형 복원 기법을 적용해 보았습니다. 사진들은 인터넷에서 수집했습니다.
Applied CLC-based rectangle reconstruction on a framed picture of Hwahongmun, Hwaseong Fortress, KOREA.
Inverse Perspective Projection of Convex QuadrilateralsJoo-Haeng Lee
Presenter: Joo-Haeng Lee
Affiliation: ETRI
Venue: ACDDE 2011 (Asian Conference on Design and Digital Engineering)
- VR and Multimedia Workshop
- Session VRM-2 Paper ID 116
Comment:
- The talk was given at ACDDE 2011.
- The full paper was published in ETRI Journal: Joo-Haeng Lee "an analytic solution to projector pose estimation problem, " 34(6), 2012.
- Paper link: http://etrij.etri.re.kr/Cyber/BrowseAbstract.jsp?vol=34&num=6&pg=978
- The dual problem for the camera was solved and presented in ICPR 2012: Joo-Haeng Lee, "Camera calibration from a single image based on coupled line cameras and rectangle constraint."
Camera Calibration from a Single Image based on Coupled Line Cameras and Rect...Joo-Haeng Lee
ICPR 2012 Paper Abstract
Title: Camera Calibration from a Single Image Based on Coupled Line Cameras and Rectangle Constraint
Author: Lee, Joo-Haeng (ETRI)
Scheduled for presentation during the Regular Session "Poster Shotgun (04): CV" (TuPSAT2), Tuesday, November 13, 2012, 08:30−09:00, Multi-Purpose Hall
21st International Conference on Pattern Recognition, November 11-15, 2012, Tsukuba International Congress Center, Tsukuba, Japan
This information is tentative and subject to change. Compiled on February 13, 2013
Note on Coupled Line Cameras for Rectangle Reconstruction (ACDDE 2012)Joo-Haeng Lee
The presentation file for the talk in ACDDE 2012.
http://www.acdde2012.org/
It deals with the research result published in ICPR 2012 with the title as "Camera Calibration from a Single Image based on Coupled Line Cameras and Rectangle Constraint"
https://iapr.papercept.net/conferences/scripts/abstract.pl?ConfID=7&Number=70
Book Formatting: Quality Control Checks for DesignersConfidence Ago
This presentation was made to help designers who work in publishing houses or format books for printing ensure quality.
Quality control is vital to every industry. This is why every department in a company need create a method they use in ensuring quality. This, perhaps, will not only improve the quality of products and bring errors to the barest minimum, but take it to a near perfect finish.
It is beyond a moot point that a good book will somewhat be judged by its cover, but the content of the book remains king. No matter how beautiful the cover, if the quality of writing or presentation is off, that will be a reason for readers not to come back to the book or recommend it.
So, this presentation points designers to some important things that may be missed by an editor that they could eventually discover and call the attention of the editor.
Expert Accessory Dwelling Unit (ADU) Drafting ServicesResDraft
Whether you’re looking to create a guest house, a rental unit, or a private retreat, our experienced team will design a space that complements your existing home and maximizes your investment. We provide personalized, comprehensive expert accessory dwelling unit (ADU)drafting solutions tailored to your needs, ensuring a seamless process from concept to completion.
Hello everyone! I am thrilled to present my latest portfolio on LinkedIn, marking the culmination of my architectural journey thus far. Over the span of five years, I've been fortunate to acquire a wealth of knowledge under the guidance of esteemed professors and industry mentors. From rigorous academic pursuits to practical engagements, each experience has contributed to my growth and refinement as an architecture student. This portfolio not only showcases my projects but also underscores my attention to detail and to innovative architecture as a profession.
Dive into the innovative world of smart garages with our insightful presentation, "Exploring the Future of Smart Garages." This comprehensive guide covers the latest advancements in garage technology, including automated systems, smart security features, energy efficiency solutions, and seamless integration with smart home ecosystems. Learn how these technologies are transforming traditional garages into high-tech, efficient spaces that enhance convenience, safety, and sustainability.
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You could be a professional graphic designer and still make mistakes. There is always the possibility of human error. On the other hand if you’re not a designer, the chances of making some common graphic design mistakes are even higher. Because you don’t know what you don’t know. That’s where this blog comes in. To make your job easier and help you create better designs, we have put together a list of common graphic design mistakes that you need to avoid.
Can AI do good? at 'offtheCanvas' India HCI preludeAlan Dix
Invited talk at 'offtheCanvas' IndiaHCI prelude, 29th June 2024.
https://www.alandix.com/academic/talks/offtheCanvas-IndiaHCI2024/
The world is being changed fundamentally by AI and we are constantly faced with newspaper headlines about its harmful effects. However, there is also the potential to both ameliorate theses harms and use the new abilities of AI to transform society for the good. Can you make the difference?
4. Basic Theory RFD Rib-and-Fan Decomposition A Bézier curve/surface can be decomposed into Ribs: curves/surfaces Fans: vector fields Reference Joo-Haeng Lee and Hyungjun Park, “Ribs and Fans of Bézier Curves and Surfaces,” Computer-Aided Design and Applications,2 (2005), pp.125-134. (Proc. of CAD’05, Bangkok, Thailand)
5. RFD of a Bézier Curve Definition Decomposition Rib Fan Control points of ribs Control vectors of fans
30. Properties of RFD of Bézier Curves Three properties of RFD of Bézier curves: Composite Fan Rib-Invariant Deformation Fan continuity in subdivision Reference Joo-Haeng Lee and Hyungjun Park, “Geometric Properties of Ribs and Fans of a Bézier Curve,” J. of Comp. Sci. & Tech, 21(2), pp.279—283, 2006.
32. Composite Fan > Decomposition Control vectors of a composite fan Key idea: degree elevation of fans
33. Composite Fan > Construction Construction of a Bézier curve of degree n Generally, it requires specification of (n+1) control points We propose a new method using A base line segment Defined by 2 end-points Equivalent to the rib of degree 1 A composite fan Defined by (n-1) control vectors
39. Rib-Invariant Deformation Motivation Ribs as guides or constraints in the course of curve deformation An example of use-case “The rib of degree d should be invariant during the deformation of a curve of degree n.”
42. Rib-Invariant Deformation Procedure Specify d the degree of a invariant rib Initially, we have an under-constrained linear system Known: (d-1) control points of the rib of degree d Unknown: (n-1) control points of the curve of degree n Specify (n-d) control points of the given curve Now, we have a (d-1)x(d-1) linear system Known: (d-1) control points of the rib of degree d Unknown: (d-1) control points of the curve of degree n Solve the linear system To compute the unknown control points of the curve of degree n
45. Fan Continuity Subdivision of a Bézier curve of degree n Cncontinuity at the joint Motivation What happens to the ribs and the fans of subdivided segments, especially in the sense of continuity?
46. Fan Continuity Ribs and fans of the subdivided curves Ribs C0 continuity at most Hence, we are not interested in them Fans Fans of the subdivided curves are directionally continuous at the joint Moreover, they directionally coincide with the subdivided fans
48. Fan Continuity > Example (1) Fans of subdivided curves Subdivision of the topmost fan
49. Fan Continuity > Example (2) Fans of subdivided curves Subdivision of the topmost fan
50. Geometric Morphology Summary We present techniques to generate a sequence of curves that represent the morphological development and transformation of Bézier curves based on the rib-and-fan decomposition (RFD). Reference Joo-Haeng Lee and Hyungjun Park, “A Note on Morphological Development and Transformation of Bézier Curves based on Ribs and Fans,” ACM Symposium on Solid and Physical Modeling (2007), pp. 379-385, Beijing, China, 2007.
51. Morphology Definition 1 (morphology) the branch of biology that deals with the structure of animals and plants2 (morphology) studies of the rules for forming admissible words3 (morphology, sound structure, syllable structure, word structure) the admissible arrangement of sounds in words4 (morphology, geomorphology) the branch of geology that studies the characteristics and configuration and evolution of rocks and land forms WordNet 1.7.1, Edition. Copyright 2001 by Princeton University. All rights reserved.This electronic edition published by Hanmesoft Corp. All rights reserved.
53. Morphological Development Morphological Development From a simple linear line segment: i.e., parameter domain or a base rib To a high-degree Bézier curve with a complex shape and features MorphologicalRegression Vice versa
54. Morphological Development Common Formulation Input A given Bézier curve Development Path Interpolating end conditions at 0 and 1 Intermediate trajectory determines the developmental pattern of a curve .
55. Morphological Development Three Methods of Development Linear Interpolation Trajectory: Straight Line Composite Fans (DCF) Piecewise Linear Interpolation Trajectory: Poly Line Fan Lines (DFL) Smooth Curve Trajectory: Bézier Curve Fan Curves (DFC)
72. Morphological Development Characteristics of Intermediate Shapes Proposed Method (TFL/TFC) Features appears gradually Intermediate curves are relatively smooth Analogous to morphological development in biology Linear Interpolation (TLI) Early appearance of shape features in immature curves More likely to have wiggles and cusps
74. Morphological Transformation Metamorphosis 1 (metamorphosis, metabolism) the marked and rapidtransformation of a larva into an adult that occurs in some animals 2 (transfiguration, metamorphosis) a striking change in appearance or character or circumstances 3 (metamorphosis) a completechange of physical form or substance especially as by magic or witchcraft WordNet 1.7.1, Edition. Copyright 2001 by Princeton University. All rights reserved.This electronic edition published by Hanmesoft Corp. All rights reserved.
75. Morphological Transformation Common Formulation Input Two curves Output One-parameter family of curves representing the intermediate shapes .
76. Morphological Transformation Three Methods TLI Linear Interpolation Trajectory: Straight Line TCE Cubic Blending and Linear Extrapolation Trajectory: Straight Line TDE Development, Quadratic Blending, and Extrapolation Trajectory: Curve
89. Morphological Transformation > TDE Development + Quad Blend + Extrapolation Control of over-growth Revision of extrapolation ratio Selection of base transformation
97. Morphological Transformation > TDE > Ex 1 Linear TDE (1,1; ß=3.0) TDE (4,4; ß=3.0) TDE (1,1; ß=2.4) TDE (4,4; ß=2.4) Dev + Quad Blend
98.
99. Morphological Transformation > TDE > Ex 2 Linear TDE (1,1; ß=3.0) TDE (3,3; ß=3.0) TDE (1,1; ß=2.5) TDE (3,3; ß=2.5) Dev + Quad Blend
100.
101. Inspiration from Biology Evolutionary Developmental Biology* (evolution of development or informally, 'evo-devo') is a field of biology that compares the developmental processes of different animals in an attempt to determine the ancestral relationship between organisms and how developmental processes evolved. The discovery ofgenes regulating development in model organisms allowed for comparisons to be made with genes and genetic networks of related organisms. * WikiPedia
102. Inspiration from Biology Different Developmental Process * Life: The Science of Biology (William K. Purves, et al., 2004)
103. Inspiration from Biology Different Developmental Process * Life: The Science of Biology (William K. Purves, et al., 2004)
104. Inspiration from Biology Different Developmental Process Recapitulation theory (Earnst Haeckel, 1866) * http://en.wikipedia.org/wiki/Ontogeny_recapitulates_phylogeny
105. Inspiration from Biology Evolutionary Tree or Phylogenetic Tree * Life: The Science of Biology (William K. Purves, et al., 2004)
106. Inspiration from Biology Evolutionary Tree: Plantae * Life: The Science of Biology (William K. Purves, et al., 2004)
107. Inspiration from Biology Evolutionary Tree: Animalia * Life: The Science of Biology (William K. Purves, et al., 2004)
108. Morphological Transformation Characteristics of Intermediate Shapes Proposed Method (TDE) Intermediate curves are neutral to given curves Analogous to evolutionary developmental biology Further control by choosing the degrees of the initial shapes Linear Interpolation (TLI, TCE) Simultaneous mixture of features of two curves Static shape change No further control except re-parameterization
109. Concluding Remarks Novel approach to deal with geometric morphology of Bézier curves based on ribs and fans Analogous to biological phenomena Morphological development in biology Evolutionary developmental biology Development Developmental patterns are generated along trajectories based on intrinsic, internal structure of Bézier curves such as fan lines and fan curves Transformation Based on the assumption that inter-curve transformation happens in the early developmental stage rather than the mature curves alone Extrapolation of immature shapes to control size
110. Concluding Remarks Future works Extension Bézier surfaces B-spline Interpretation/simulation of natural phenomena Evolution Morphological diversity Evolution of Geometry Geometric Gene?
111. Concluding Remarks Future works Extension to Bézier surfaces Extension to piece-wise curves/surfaces Interpretation/simulation of natural phenomena Comparison with other methods
112. Q & A Thank you! Questions/Comments E-mail: joohaeng@gmail.com