cad course master in aerospace and mechanical engineering · master in aerospace and mechanical...

150
1 Computer Aided Design CAD course Master in Aerospace and Mechanical Engineering

Upload: vuongminh

Post on 08-Apr-2018

236 views

Category:

Documents


2 download

TRANSCRIPT

Page 1: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

1

Computer Aided Design

CAD course

Master in Aerospace and Mechanical Engineering

Page 2: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

2

Computer Aided Design

Service...

Eric Béchet (it's me !) Engineering studies in Nancy (Fr.) Ph.D in Montréal (Can.) Academic career in Nantes as Post-doc then ass. Prof. in

Metz (Fr.)then Liège...

Christophe Leblanc Assistant ( Ph.D. student ) at our university

Website http://www.cgeo.ulg.ac.be/CAO

Contacts : [email protected]

Page 3: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

3

Computer Aided Design

Procedures

12 Ex-Cathedra lectures (~2h except for the 1st) Practical sessions

On the NX CAD software (5 4h-sessions) Programming (8 2h-sessions)

Practical assessment : practical works (pw) are rated.

Final test about theory (tt) – Jan./Sept. The practical sessions, the project and the final

test are all mandatory, with over 8/20 to pass. The final mark m=pw/3 + 2tt/3, over 10 to pass & get the credits for the course.

Page 4: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

4

Computer Aided Design

Procedures Lectures are given on Tuesday, 2 PM – Lecture

room is O1 ( B37 bldg.) Begins today (exceptionally lasts 4h !), then

Sept. 26, Oct. 3, 10, 17, 24; Nov. 7, 14, 21, 28, Dec. 5, 14, 19

Practical work begins Sept. 26th after the course (check website for more dates & info) It is organized by groups of around 20 students

formed in accordance with availabilities. Any question : I am available mostly Fridays,

appointment via email or phone : 04-366-9165Office : Bldg B52 +2/438

Page 5: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

5

Computer Aided Design

Outline (1st few classes)

Introduction Brief history Some basics about solid modeling

Parametric forms Curves Surfaces

Implicit forms Plane curves et surfaces Implicit volume modeling

Page 6: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

6

Computer Aided Design

Outline (whole course)

Interpolation and polynomial approximation Cubic splines Bézier curves B-Splines Curves and rational surfaces In-depth B-REP models

Page 7: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

7

Computer Aided Design

Introduction

CAD/CAM – Computer Aided Design / Computer Aided Manufacturing Development since the 1950s-1960s

Iso Schoenberg (at U-Wisconsin) – splines (40's) First « interactive » CAD graphic engine at the MIT

(I. Sutherland, Sketchpad) – 60's James Ferguson (at Boeing) – splines (60's) Paul De Casteljau (at Citroën) – Bézier curves (50's) Pierre Bézier (at Renault) – '' '' Carl De Boor (at GM / U-Wisconsin) – B-Splines (70's)

Catia, Unigraphics (now Siemens NX) date back to the mid-70’s, emergence of 3d modeling kernels on mainframes.

Huge expansion in the 80’s with cheap personal computers becoming ubiquitous.

Page 8: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

8

Computer Aided Design

Introduction

Sketchpad (Ivan Sutherland) – 1963

Page 9: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

9

Computer Aided Design

Introduction

Old mathematical and theoretical bases Practical framework has been developed

because of industrial needs. In return, it has contributed at the theoretical

level.

Page 10: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

10

Computer Aided Design

Basics

Page 11: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

11

Computer Aided Design

Solid modeling

Many types of CAD systems First systems (such as Sutherland's) were aides for

drafting in 2D With the evolution of computers, 3D capabilities

were added Wireframe representation Surface modeling Then, real 3D modelers came over.

Today, most CAD system incorporate all capabilities.

One can start with surface design, from which a 3D model can be built, which yields at the end the 2D technical drawings that may be printed on paper.

Page 12: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

12

Computer Aided Design

Solid modeling

More generally, what are the geometric queries that a solid modeler is expected to respond to ?

Eg. « Is a given point inside or outside a volume, on a

face or an edge, or even on an existing vertex ? » « Generate a set of points located on the boundary

of the solid » « Compute the union of two solids » « Build one solid from a set of intersecting

surfaces »

...

Page 13: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

13

Computer Aided Design

Solid modeling

3D modelers, many types of representation for volumes Two families

Volumetric models By construction

Half spaces (level-sets) Composition of primitive objects (CSG)

By decomposition Exhaustive enumeration

and structured meshes Models defined by boundaries

Definition of the volume by the enumeration of its boundariesB-Rep

Page 14: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

14

Computer Aided Design

Solid modelling

Fundamental properties of solid models Power of expression

Degree in the capability to represent all real solids, without approximation.

ValidityAmong the possible representations within the model, are some representations invalid ?

Page 15: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

15

Computer Aided Design

Solid modelling

Fundamental properties of solid models Non-ambiguity and uniqueness

Does a representation in the model correspond to one or several real solids ? / Can a real solid be represented in different ways ?

ConcisionTo represent a particular solid, do we need many primitives or operations ?

The wireframerepresentationis ambiguous

Page 16: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

16

Computer Aided Design

Solid modelling

Fundamental properties of solid models Is the set of operations closed or open with respect to the

model ?During the application of an operation onto a model, can we obtain a non-valid solid, (are every operations valid ?) or a solid that is non representable ?

Calculation cost and applicabilityIs the construction of a solid within the selected model costly ?

Does the selected model address the issue raised by the user ?

Page 17: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

17

Computer Aided Design

CSG model

Description of a solid with the help of simpler primitives and elementary operations is ubiquitous in CAD modeling : CSG model (Constructive Solid Geometry) Internal representation

is in the form of a binary tree Leaves are geometric primitives Nodes are operations

« union », « difference »,« intersection »

Possible to :« move », « complement », « change scale » etc...

Wik

iped

ia

Page 18: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

18

Computer Aided Design

Solid modeling

Characteristics of the modeling by half-spaces / CSG

Power of expression: depends on the set of available half-spaces (planes, quadratic surfaces, etc.) or primitivesIt is not possible to represent a single surface limited by 4 curves (a patch) , for example.

Validity : The half spaces are infinite (limited by planes for example). A combination can give an infinite volume i.e. not acceptable under the assumption that solids are finite and “closed” volumes.

Ambiguity/uniqueness : each valid combination of half-spaces determines an unique solid → non ambiguous.A given solid can be represented by several different combination of half-spaces (non uniqueness)

Page 19: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

19

Computer Aided Design

Solid modeling

Concision : the model by half-spaces is relatively concise.

Closedness of the set of operations : we focus here on boolean operations of union and intersection, these always give a valid description → closed set of operations

Calculation cost and applicability

The operation of modeling itself is not costly (update of a tree). The extraction of useful information can be much more difficult e.g. calculation of surfaces... or very simple such as collision detection (inside / outside test for a point)

Page 20: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

20

Computer Aided Design

Solid modeling CSG models

User-friendliness Widely used in the interface shown by the CAD software

to the user In general many CAD software

integrate some sort of history of the constructionof the model (cf model tree in Catia)

Page 21: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

21

Computer Aided Design

Solid modeling

Modeling by spatial decomposition Division in regular cells Exhaustive enumeration of non empty cells

M. M

änty

Page 22: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

22

Computer Aided Design

Solid modeling

Modeling by spatial decomposition Cells of variable size Recursive division of a cell containing the whole

solid in smaller cells located along the boundary of the solid, until a prescribed error is reached.

Page 23: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

23

Computer Aided Design

Solid modeling

Modelling by spatial decomposition Quadtree (2D)

Each node has 4 children. Each children has a different representation in function of

the “filling” of the area

1 2

3 4

Page 24: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

24

Computer Aided Design

Solid modeling

Modelling by spatial decomposition Quadtree (2D)

Each node has 4 children. Each children has a different representation in function of

the “filling” of the area

1

2.1

4

2.2

2.3 2.4

3.1 3.2

3.3 3.4

Page 25: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

25

Computer Aided Design

Solid modeling

Modelling by spatial decomposition Boolean operations : union, complement,

difference, intersection

U =

U =

U =

U =

U =

U =

Union

U

=

=

=

=

=

=

Intersection

U

U

U

U

U

=

=

=

=

=

=

difference

\

\

\

\

\

\

=\

=

=

=

complement

_

_

_=\

Page 26: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

26

Computer Aided Design

Solid modeling

Modelling by spatial decomposition Octree (3D) – analogy : voxels

Each node has 8 children. Often used in medical images as means of efficient

storage Effective means of geometric

location in 3D space

Page 27: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

27

Computer Aided Design

Solid modeling

Characteristics of the modelling by spatial decomposition

Power of expression: By definition, it's an approximation as soon as the boundaries of the object are not aligned with the cells

Validity : always valid Ambiguity/uniqueness

Every description corresponds to an unique solid → non ambiguous.

A given solid is represented by a single way for the same root cell (uniqueness)

→ However, since the representation is approximative, we can consider that many real solids can lead to the same representation.

Page 28: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

28

Computer Aided Design

Solid modeling

Concision : For a precise representation, the model can become very heavy thus it is not very concise

Closedness of the set of operations : we speak here about boolean operations of union and intersection, that systematically give a valid description → closed set of operations

Calculation cost and applicability

Such models are easy to manipulate but with a limited applicability due to high calculation costs (large quantity of data). However some operations are efficient , collision (inside/outside) test for instance.

Page 29: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

29

Computer Aided Design

Solid modeling

Description by meshes It is a variant of the exhaustive decomposition that

is respecting to a certain extent the boundaries of the object

Cells are not regularly organized anymore Used mainly for scientific computations

Page 30: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

30

Computer Aided Design

Solid modeling

B-Rep model « Boundary representation » Model based on the representation of surfaces Model of exchange (STEP format) and definition The “natural” set of operators is richer than for CSG

Extrusion, chamfer etc ... Does not inherently carry the history of construction

of the model (whereas CSG usually does)

Page 31: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

31

Computer Aided Design

Solid modeling

B-Rep model Consists of two type of information

GeometricGeometric information is used for defining the spatial position, the curvatures, etc...

That's what we will see in the next couple of lectures – Nurbs curves and surfaces

TopologicalThis allows to make links between geometrical entities.

Two types of entities Geometric entities: surface, curve, point Topological entities : volume, face, edge, vertex

A topological entity “lies on” a geometric entity, which is its geometrical support

Page 32: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

32

Computer Aided Design

Solid modeling

B-Rep model Simplified hierarchical model vertex-edge-face-

volume

ff

f

v

ev v

Page 33: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

33

Computer Aided Design

Solid modeling

B-Rep model Simplified hierarchic model vertex-edge-face-volume

v1

v2

v3

v4

a1

v8

v5

v6

v7

e2

e3

e4 f

1

f1 e

1 e

2 e

3 e

4

f2 … … … ...

f3 … … … ...

...

e1 v

1 v

2

e2 v

2 v

3

e3 v

3 v

4

e4 v

4 v

1

...

v1 x

1 y

1 z

1

v2 x

2 y

2 z

2

v3 x

3 y

3 z

3

...

Composed of

Composed of

Volume 1

Composed of

Page 34: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

34

Computer Aided Design

Solid modeling

B-Rep model Complete hierarchical structure found in most solid

modelers

Volume « shells » Boundary Face

face « loops » Boundaryedge

edge Boundary

vertex

vertex G.S. Expressed inparametric coordinates u,v or t

If it exists, the geometric support (G.S.) is expressed in cartesian coordinates x,y,z

« Composed of »

« is related to »

1:n 1:n

1:{1 if manifold , 2 otherwise }

1:n 1:n

1:{2 if manifold, n otherwise }

1:2

1:n

Page 35: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

35

Computer Aided Design

Solid modeling

Characteristics of the B-REP modelling Power of expression: Allows to represent any solid if we

dispose of appropriate surfaces/curves (NURBS) Validity : Every B-REP is not necessarily valid

Topological validity (see the Euler Poincaré relations in the sequel)

Geometric validity Ambiguity/uniqueness : Every valid B-REP represents an

unique solid → non ambiguous.There are many different ways to represent a given solid (non uniqueness)

Page 36: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

36

Computer Aided Design

Solid modeling

Concision : Generally concise Closedness of the set of operations : In general,

operations made on B-REPs do not necessarily yield regular models of real solids (in particular for boolean operations)

Euler operators do maintain the topological validity, but not necessary the geometric validity

Calculation cost and applicability

boolean operators are costly, but other modelling operators may be easier to implement using a B-REP representation. In general, modelling operators are more rich than for CSG

Page 37: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

37

Computer Aided Design

Solid modeling

Validity of the model The boundary of a face is made up of edges that are not

allowed to intersect each other

invalid

Page 38: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

38

Computer Aided Design

Solid modeling

Validity of the model The faces of a model can only intersect in common

edges or vertices.

Invalid

Pyramid on base

Page 39: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

39

Computer Aided Design

Solid modeling

How to represent individual entities ? CSG

Primitives (Leaves of the CSG tree) → equations ??? Operators (Nodes " " " ) → How ?

B-REP Vertices → trivial (coordinates) Edges → straight line or ??? Faces → Planar or ??? Volumes → Indirectly Need to define a geometric support.

Page 40: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

40

Computer Aided Design

Point

Point Defined in an euclidean space (2D or 3D)

Notion of distance between two points is trivial. Sometimes defined in a non euclidean space (e.g.

parametric space, in 1D = curve or 2D=surface ) Ex : points of a curve localized on a parametric surface. Notion of distance between two points is not trivial on a

curve or a surface. Sometimes, use of homogeneous coordinates (4th

coordinate) 4 dimensions + one equivalence relation → 3D Perspective division to come back to euclidean 3D space. Rational curves and surfaces.

Page 41: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

41

Computer Aided Design

Point

Homogeneous coordinates and class of equivalence Coordinates x, y, z and w (weight) All points (4D) located on a line passing through the

origin O(0,0,0,0) are equivalent. Particularly, a point located on the plane w=1.

Change from homogeneous coordinates to euclidean coordinates by perspective division:

(xyzw)≡(

x /wy /wz /w

1)≡(

x /wy /wz /w )

Page 42: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

42

Computer Aided Design

Curve

Curve : 1D manifold in a space of higher dimension Plane curves (2D)

Position, tangent, curvature Skew curves (3D)

Position, tangent, curvature, torsion

Page 43: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

43

Computer Aided Design

Curve

Meaning of curvature k Deviation rate of the curve in comparison with a

straight line. Radius of curvature is the inverse of the curvature We can define a vector n that is normal at the

tangent and point to the center of curvature : it is the normal vector

n

t

Page 44: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

44

Computer Aided Design

Curve

Meaning of torsion t Deviation of the curve in comparison with a plane

formed by the tangent and the normal vector... For a plane curve, torsion is zero. We can define a vector normal to normal vector and

also to the tangent : it is the binormal vector b b points to the torsion center

nt

b

Page 45: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

45

Computer Aided Design

Continuity

Geometrical continuity : Given two « independent » curves : They are discontinuous

of continuity G0 (position p)

of continuity G1 (p+tangent t)

of continuity G2 (p+t+curvatures)

... G

Page 46: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

46

Computer Aided Design

Surfaces

2D manifold in 3D space Tangent plane (defined by two linearly independent

vectors tangent to the surface) Normal vector Several curvatures may be defined

Gaussian (or total) curvature and average curvature Principal curvatures

Page 47: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

47

Computer Aided Design

Different representations of curves and surfaces

Page 48: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

48

Computer Aided Design

Modes of representation

There are many Parametric form Explicit form Implicit form Etc. (eg. solution of partial differential equations –

PDEs … )

Page 49: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

49

Computer Aided Design

Parametric representation

Page 50: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

50

Computer Aided Design

Parametric representation

Use of scalar parameters to “walk” on the curve/surface The number of those scalars determine the dimension

of the entity and the mapping from one space (the parametric space to the other (usually cartesian) space.

0 – Point , 1 (u) – Curve , 2 (u,v) – Surface

3 (u,v,w) – Volume ( transformation used for finite elements) We associate to those scalars some function for each

of the space coordinates ( x,y in the plane; x,y,z in 3D)

P⃗ (u)={x= f (u)y=g (u)z=h(u)

or P⃗ (u , v)={x= f (u , v)y=g (u , v)z=h(u , v)

Page 51: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

51

Computer Aided Design

Parametric representation

Parametric curves

Page 52: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

52

Computer Aided Design

Parametric representation

For a curve, the representation takes the following form:

u is a real parameter. We obtain all the points of the curve by varying u. The parametrization is not unique ! The parameter u can be limited (limits of the curve)

P u={x= f uy=g uz=h u x

y0

1

2 3 4

5

67

8

Page 53: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

53

Computer Aided Design

Parametric representation

Continuity of the parametrization A parametric curve is said to be C

k if the

parametrization P(u) is Ck (i.e. the kth derivative is

continuous) However : a parametric curve of class C

may have an

angular point... (i.e. some continuity of the parametrization does not necessarily involve the same geometric continuity of the resulting curve !)

P u={x=u3

y=u2

x

y

P 'u=0 ={00

Page 54: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

54

Computer Aided Design

Parametric representation

Regularity of the parametrization A parametric curve P(u) is regular if the first

derivative P'(u) does not vanish at any place on all the interval of definition.

On the contrary, points where P'(u) vanishes, are called singular points.

A given curve can admit two parametric forms such that one is regular and the other one isn't...

Example : curve y=x2 with two parametric forms P(u) and Q(v)

P u={ x=uy=u2

Q v={x=v3

y=v6P 'u=0 ={10 Q '

v=0 ={00

Page 55: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

55

Computer Aided Design

Parametric representation

Regularity and continuity of the parametrization A curve of geometric continuity G

k can be described by

a parametrization that is non- Ck

A curve of parametrization Ck may not be G

k

A curve admitting singular points can be Gk and/or C

k.

A regular curve is not necessary Ck and/or G

k.

To conclude : Parametric continuity, geometric continuity, and

regularity are all relatively independent notions!

Page 56: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

56

Computer Aided Design

Parametric representation

Ck -equivalent parametric forms

Two parametric forms P(u) and Q(v) of the same curve are C

k - equivalents if there is a bijective

function j of class Ck whose reciprocal is also of

class Ck and such that:

v=u P u=Q u

Page 57: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

57

Computer Aided Design

Parametric representation

Length of a regular curve It is a measure that is independent of the

parametrization (provided that those are C1-

equivalent)

L=∫a

b

∣P 'u∣du= ∫

c=a

d=b

∣Q 'v∣dv

Page 58: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

58

Computer Aided Design

Parametric representation

Natural parametrization It is a parametrization s such that :

s is also named curvilinear abscissa along the curve.

It can be built from any regular parametrization u of the curve :

L AB=s B−sA x

yA

s=0.1

B

su =∫A

u

∣P ' t ∣dt

Page 59: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

59

Computer Aided Design

Parametric representation

Parametrization of a circle in the plane :

Natural parametrization of the same circle...

r{x=r cos uy=r sin u

, u∈[0, 2 [

{x=r cos

sr

y=r sinsr

, s∈[0, 2 r [ s=r u

Page 60: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

60

Computer Aided Design

Parametric representation

Differential geometry for parametric curves Position P :

Tangent vector T :

Normal vector N :

Binormal vector B :

T u=dPds

=dPdu

⋅duds

=P '

∣P '∣

P u=x u y u z u P '

=dPdu

P ''=

d 2 P

du2

N (u)=Norm(u)

∣Norm(u)∣ with Norm(u)=P ''

−( P ''⋅T )T

B u=T u×N u

x

y

TN

z B

(It is not defined when Norm(u) = 0 !)

Page 61: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

61

Computer Aided Design

Parametric representation

Frenet's frame and equations

2D

3D [d T s

dsd N s

dsd Bs

ds]=[

0 s 0−s 0 s

0 −s 0 ]⋅[T sN sBs ]

T s

N s

B s

s

[d T s

dsd N s

ds]=[ 0 s

− s 0 ]⋅[T sN s]

Works only with s : the curvilinear abscissa !

Page 62: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

62

Computer Aided Design

Parametric representation

Curvature k :

Torsion t:

= d 2 T

ds2 ,dTds

,T

2 = P ''' , P '' , P '

∣P '×P ''∣

2

|k|=|dTds |=

|P '×P ''|

|P '|3

u=T 'u⋅N u

∣P 'u ∣

u=N '

u⋅B u

∣P 'u∣

Curvature vector

=N u u

Page 63: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

63

Computer Aided Design

Parametric representation

Parametric surfaces

Page 64: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

64

Computer Aided Design

Parametric representation

A parametric surface is represented as :

u,v are two real parameters All the points of the surface can be

obtained by varying u and v. Again, the parametrization is not unique ! The interval of definition is limited (limits the

surface)

P u , v ={x= f u , v y=g u , v z=hu , v

x

y z

u,v

u=cst

v=cst

Page 65: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

65

Computer Aided Design

Parametric representation

A curve can be defined on the surfaceParametric space « Ambient » space

The equations seen for parametric curves are valid in this particular case. x

y z

t

u=cst

v=cst

P u , v : {x= f u , v y=g u , v z=hu , v

t :{x= f u t , v t y=g u t , v t z=hu t , v t

uvt : {u=u t

v=v t

Page 66: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

66

Computer Aided Design

Parametric representation

Regularity and continuity of the parametrization A parametric surface is of class C

k if the mapping

P(u,v) onto R3 is of class Ck.

A parametrization is regular if and only if (iff)

The points on the parametric space for which it is not the case are called singular points.

Ck–equivalent parametric forms follow the same

definitions as for curves

∂ P∂u

u0 , v0×∂ P∂ v

u0 , v0≠0 ∀u0 , v0∈D⊂ℝ2

Page 67: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

67

Computer Aided Design

Parametric representation

Differential geometry for parametric surfaces

Position P :

Unit tangent vectors T u and T v :

These vectors are, in general, not orthogonal ! Tangent plane (parametric form)

or

T uu , v=

∂ P∂u

⋅∣∂ P∂ u ∣

−1

=P u

∣P u∣T v

u , v =∂ P∂ v

⋅∣∂ P∂ v ∣

−1

=Pv

∣Pv∣

P u , v=[x u , vy u , v z u , v ] Pu

=∂ P∂ u

Puv=

∂2 P

∂u∂v⋯

Pt u0 , v0a ,b=P u0 , v0a⋅T u

u0 , v0b⋅T vu0 , v0

a ,b∈ℝ2

P⃗t(u0 , v0)(a ,b)=P⃗ (u0 , v0)+a⋅P⃗u

(u0 , v0)+b⋅P⃗v(u0 , v0)

Page 68: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

68

Computer Aided Design

Parametric representation

Normal vector N :

N (u , v)=Norm(u , v)

|Norm(u , v)| with Norm(u , v)=T u

×T v or Pu×P v

u ,v

u=cst

v=cst

T u

T v

N

Page 69: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

69

Computer Aided Design

Parametric representation

Area of a surface

1st fundamental form Other notation of the area of a surface

du P u

dv P v

dS

A=∬Ω

dS

dS=∣du⋅Pu×dv⋅Pv

∣=∣Pu×P v

∣dudv

∣a×b∣2=a⋅a⋅b⋅b−a⋅b2

A=∬D

eg− f 2dudv

Lagrange's identity

dS=√(e g− f 2)dudv with e=Pu

⋅Pu , f =Pu⋅Pv , g=Pv

⋅Pv

Page 70: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

70

Computer Aided Design

Parametric representation

Length of a curve on a surface

Γ⃗uv(t): {u=u(t )

v=v (t )Γ⃗(t ):{

x= f (u(t ) , v (t ))y=g (u(t ) , v (t ))z=h(u(t) , v (t ))

Γ'=

dP (u(t ) , v (t ))dt

P u , v : {x= f u , v y=g u , v z=hu , v

Pu=∂ P u , v

∂u

Pv=∂ P u , v

∂ v

't =u'

t Puu t , v t v '

t Pvut , v t

Γ'=∂ P (u(t ) , v (t ))

∂ududt

+∂ P (u(t) , v (t ))

∂ vdvdt

Derivative of the curve expressed in the parametric space of the surface Derivative of the surface (in 3D)

Page 71: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

71

Computer Aided Design

Parametric representation

L=∫a

b

∣ ' t ∣dt=∫

a

b

∣ 't ∣

2

dt

't =u'

t Puu t , v t v '

t Pvut , v t

∣'t ∣2

=e u' t 22 f u '

t v 't g v '

t 2

with e=Pu⋅Pu , f =Pu

⋅Pv , g=P v⋅Pv

Page 72: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

72

Computer Aided Design

Parametric representation

If we set

that is equivalent to :

( we have )

, we get a quadratic form :

ds=√e u'(t )2

+2 f u'(t )v '

(t)+g v '(t)2 dt

L=∫sa

s b

ds=sb −sa

ds=√e du2+2 f dudv+g dv2

e u't 2

2 f u't v '

t g v 't 2=u'

t v ' t e f

f g u't

v 't

L=∫a

b

u't v '

t e ff g u

't

v 't dt

Page 73: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

73

Computer Aided Design

Parametric representation

Angle between two curves ...

cosα=

(u1'(t 1) v1

'(t1))( e f

f g )(u2

'(t 2)

v2'(t 2))

√(u1'(t1) v1

'(t1))( e f

f g )(u1

'(t1)

v1'(t1))(u2

'(t 2) v2

'(t 2))( e f

f g )(u2

'(t2)

v2'(t 2))

Γ1'(t1)⋅Γ2

'(t 2)=∣Γ1

'(t1)∣∣Γ2

'(t 2)∣cosα=(u1

'(t 1) v1

'(t 1))( e f

f g )(u2

'(t 2)

v2'(t 2))

Page 74: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

74

Computer Aided Design

Parametric representation

The first fundamental form is the application :

It is a symmetric bilinear form that allows to measure real distances from variations in the parametric space...

The matrix M1 is a representation of the metric tensor,

often noted

M1 also is related to the Jacobian matrix

of the transformation (u,v) → (x,y,z) (it is JTJ ).

j1(d Γ1uv , d Γ2

uv)=(du1 dv1)( e f

f g )(du2

dv2)=(du1 dv1 ) M1(

du2

dv2)

L=∫a

b

√j(d Γuv , d Γ

uv)dt cosα=

j(d Γ1uv , d Γ2

uv)

√j(d Γ1uv , d Γ1

uv)j(d Γ2

uv , d Γ2uv)

A=∬D√det M1 dudv ( =∬

D

det J dudv under some conditions)

with e=Pu⋅Pu , f =Pu

⋅P v , g=P v⋅Pv

J=(∂ x /∂u ∂ x /∂ v∂ y /∂u ∂ y /∂ v∂ z /∂ u ∂ z /∂ v )

g ij , i , j=u , v

Page 75: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

75

Computer Aided Design

Parametric representation

Curvatures...

Normal curvature :

Geodesic curvatureor relative curvature w/r to the surface :

Simple or total curvature of the 3D curve :

kn

kg

k

Page 76: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

76

Computer Aided Design

Parametric representation

Curvature vectors

Necessarily, we do have :

Differentiating yields :

N

P(u,v)

n

k

kn

kg

T

k=d Tds

=k⋅n=kn+k g

Center of curvature

(e.g. from Frenet's relations)

N⋅T=0

d Tds

⋅N +T⋅d Nds

=0

kn=d Tds

⋅N=−T⋅d Nds

=−d P (u , v)

ds⋅

d Nds

=−d P⋅d N

ds2 =l du2

+2 mdudv+n dv2

e du2+2 f dudv+g dv2

l=−dPdu

⋅d Ndu

m=−12(

dPdu

⋅d Ndv

+dPdv

⋅d Ndu

) n=−dPdv

⋅d Ndv

with

G=N×Tkn=kn⋅N k g=kg⋅G

(kg=d Tds

⋅G ) (ds=

√e du2+2 f dudv+g dv2)

Page 77: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

77

Computer Aided Design

Parametric representation

This can be rewritten by noting that

and

, and integrating by parts

where e.g. for l :

l=−dPdu

⋅d Ndu

m=−12(

dPdu

⋅d Ndv

+dPdv

⋅d Ndu

) n=−dPdv

⋅d Ndv

dPdu

⋅N=0dPdv

⋅N=0

l=d 2 P

du2 ⋅N m=d 2 Pdu dv

⋅N n=d 2 P

dv2 ⋅N

UV=∫U dV +∫V dU

U=dPdu

dV=dNdu

⋅du

Page 78: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

78

Computer Aided Design

Parametric representation

Curvatures and the second fundamental form The second fundamental form is the application

Normal curvature of a curve on a surface :

Geodesic curvature (curvature in the tangent plane) Measures the deviation of the curve in comparison with a

geodesic

j2(d Γ1uv , d Γ2

uv)=(du1 dv1)( l m

m n )(du2

dv2)=(du1 dv1 ) M2(

du2

dv2)

with l=N⋅Puu , n=N⋅Pvv , m=N⋅Puv

kn=j2(d Γ

uv , d Γuv)

j1(d Γuv , d Γ

uv)

kn=j2(d Γ

uv , d Γuv)

ds2

Page 79: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

79

Computer Aided Design

Parametric representation

Definition of the geodesic It is a curve with a minimal length on a surface.

In the plane, those are lines On a sphere, great circles By definition, the geodesic has no geodesic curvature.

Relations between « simple » curvature, geodesic curvature and normal curvature is obtained from the curvature vectors

The geodesic curvature is therefore readily obtained from the others (except for the sign, which is same as )

k2=kn

2+kg

2

kg2=k

2−kn

2

k=kn+k g kn=kn⋅N k=k⋅n k g=kg⋅(N×T )=kg⋅G

d Tdu

⋅G

Page 80: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

80

Computer Aided Design

Parametric representation

A circle of radius R in the plane

Curvature k = 1/R

Geodesic curvature kg= 1/R

Normal curvature kn= 0

A big circle on a sphere or radius RCurvature k

= 1/R

Geodesic curvature kg= 0

Normal curvature kn= 1/R

In the previous slides, k is the curvature of the curve in 3D (not in the parametric space !!!)

Page 81: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

81

Computer Aided Design

Parametric representation

Curvatures of the surface

The normal curvature kn at a point only depends on the

local orientation of Γ on the surface. If we sweep through all the orientations, this curvature passes by a minimum k

min then a maximum k

max for two perpendicular directions.

These directions and the particular values of kn are

respectively called principal directions and principal curvatures of the surface. They do not depend on the parametrization of the surface...

They are the solution of an eigenvalue problem. The Shape operator (also called Weingarten Map)

plays a key role here, see what follows.

kn=j2(d Γ

uv , d Γuv)

j1(d Γuv , d Γ

uv)

Page 82: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

82

Computer Aided Design

Parametric representation

Shape operator

Here, N is the normal to the surface, p is a point on the surface, w is a tangent vector to the surface at p. is a directional derivative along a unit vector w (in the surface) :

it is equal to .This operator gives back a vector in the tangent plane.

If one works in an orthonormal basis, eigenvectors are easy to compute as the operator is symmetric...

Let's build such an orthonormal basis from the natural one :

W p(w )=−∇w⋅N

∇w

P u=∂ P∂u

P v=∂ P∂ v

N=N (u , v )=P u

×Pv

‖P u×Pv‖

t1=Pu

‖Pu‖

t 2=N×t1=P v

−(Pv⋅t 1)t1

‖P v−(Pv

⋅t 1)t1‖

wu∂∂u

+w v∂∂ v

w=wu⋅Pu+wv⋅Pv

Page 83: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

83

Computer Aided Design

Parametric representation

It is easy to show that one can switch from one basis to the other using coefficients of the 1st fundamental form …

One can also switch the other way back, working on coefficients rather than on vectors e.g. for any vector

One gets

t1=Pu

‖Pu‖=

Pu

√et 2=

e P v− f Pu

√e √eg− f 2=

e Pv− f P u

√e √h

[ t1

t 2]=1

√e√h [ √h 0− f e ][P

u

P v]

w⃗=w1 t1+w2 t 2=wu P u+wv Pv

[wu

wv]=

1

√e √h [√h − f0 e ][w1

w2]=Φ [w1

w2]

Page 84: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

84

Computer Aided Design

Parametric representation

Now back to the shape operator : we will start with a vector expressed in the orthonormal frame (w

1,w

2) , convert it to the parametric basis (w

u,w

v),

take the directional derivative of the

normal n and then project back to the orthonormal frame.

Here, is precisely the matrix of the

coefficients of the second fundamental form...

wu∂∂u

+w v∂∂ v

W p(w )=−[ t1

t 2][nu nv]Φ [w1

w2]=−Φ

T [Pu

P v][nu nv]Φ [w1

w2]−[P

u

P v ][nu nv ]

Page 85: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

85

Computer Aided Design

Parametric representation

In the orthonormal basis

In the original basis

(Weingarten Equation)

W p(w)=ΦT [ l m

m n ]Φ[w1

w2]=

1e h [ √h 0

− f e ][l mm n ][√h − f

0 e ][w1

w2]

=1eh [ h l (e m− f l)√h

(e m− f l )√h f 2 l+e2 n−2e f m][w1

w2]

~W p(w)=ΦW p(w)Φ−1 [wu

wv]=Φ(Φ

T [ l mm n ]Φ)Φ

−1[wu

wv]

=ΦΦT [ l m

m n ][wu

wv ]=1h [

g − f− f e ][ l m

m n ][wu

wv ]=[ e ff g ]

−1

⋅[ l mm n ][wu

wv ]

Page 86: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

86

Computer Aided Design

Parametric representation

Eigenvalues and eigenvectors of the shape operator

The shape operator gives the normal curvature for a given orientation (i.e. the derivative of the unit normal vector with respect to a small increment along that orientation on the surface)

One can work either in the original frame (non orthonormal)

Or the orthonormal frame, for which the matrix is symmetric and the 2D eigenvectors are orthogonal

(L−k I )(dudv)=(00) with L=M 1

−1 M 2=~W p(w ) det (L−k I )=0

(W p(w)−k I )(dt1

dt 2)=(00) det (W p(w)−k I )=0

Page 87: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

87

Computer Aided Design

Parametric representation

The eigenvectors are obtained using any of the relations:

Just use the other relation if the basis contains a null vector for one of the values of :

(dudv )⋅(

l−k em−k f )=0 (du

dv )=α⋅(m−k fk e−l ) , α>0: du2

+dv2=1

(dudv )⋅(

m−k fl−k g )=0 (du

dv )=α⋅( l−k gk f −m) , α>0: du2

+dv2=1

k

(M 2−k M 1)(dudv )=(00) ( l−k e m−k f

m−k f n−k g )(dudv)=(00)

Page 88: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

88

Computer Aided Design

Parametric representation

ExampleP u , v=

uv

cos uPu

u , v=10

−sin u Pvu , v=

010

N (u , v)=Pu

×P v

∣Pu×P v∣

=(−sin u

01 )⋅ 1

√1+sin2 u

Puuu , v=

00

−cos uPvv

u , v =000

Puvu ,v=

000

Page 89: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

89

Computer Aided Design

M1=Pu⋅Pu Pu

⋅Pv

Pu⋅Pv Pv

⋅P v=1sin2 u 00 1

(L−k I )(dudv)=(00) with L=M 1

−1 M 2

M2=(N⋅Puu N⋅Puv

N⋅Puv N⋅Pvv)=(−cos u

√1+sin2 u0

0 0)

Parametric representation

Page 90: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

90

Computer Aided Design

Parametric representation

Numerical application : u=0 and v=0

M1−1=1 0

0 1

L=M 1−1 M 2=−1 0

0 0

M1=1sin2 u 00 1=1 0

0 1

M2=(−cos u

√1+sin2 u0

0 0)=(−1 00 0)

1=−1 c1=102=0 c2=01

c1

c2

o

C13D=(Pu , Pv)⋅(10)

C 23D=(Pu , Pv)⋅(01)

Page 91: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

91

Computer Aided Design

Parametric representation

Umbilical points Points whose normal curvature k

n is independent of

the orientation of Γ . Locally, the surface looks like a plane or a sphere.

In this case, the following relations hold for the matrices M

1 and M

2 :

le=

mf=

ng

if f ≠0

le=

ng

if f =0 and m=0

kn=le=kmin=kmax= const.

Principal directions are arbitrary.

Page 92: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

92

Computer Aided Design

Parametric representation

Gaussian curvature and average curvature Invariants (do not depend on the parametrization)

M=minmax

2=

12

trace L=12

e ng l−2 f m

e g− f 2

kT=kminkmax=det (L)=det (M 2)

det (M 1)=

l n−m2

e g− f 2

L=M 1−1 M 2

Page 93: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

93

Computer Aided Design

Parametric representation

Local nature of the surface k

T>0 the surface is locally an ellipsoid – elliptic point

kT<0 : hyperbolic paraboloid – saddle point –

hyperbolic point

kT=0 and k

M<>0 : parabolic cylinder – parabolic

point

kT=0 and k

M=0 : no information – locally plane

Page 94: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

94

Computer Aided Design

Christoffel symbols

Complete developments. Christoffel symbols Expression of the first derivatives along a

curve...

Lets differentiate that expression again...

Γ ' (t )=u ' Pu+v ' P v

u'=

du(t )dtPu=

∂ P (u , v)∂u

Pv=∂ P (u , v)

∂ vv '=

dv (t)dt

Page 95: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

95

Computer Aided Design

Christoffel symbols

The terms are in the tangent plane The terms can be expressed as

linear combinations of tangential and normal components :

The are the Christoffel symbols (often written in textbooks ) and the are the coefficients of the second fundamental form.

(Γ ' (t)=u ' Pu+v ' P v) '

Γ" (t )=u" Pu+u ' (u ' Puu+v ' Puv)+v " Pv+v ' (u ' P vu+v ' P vv)

=u" Pu+v " Pv+u ' 2 Puu+u ' v ' Puv+u ' v ' P vu+v ' 2 P vv

u" Pu+v " P v

P ij , i , j={u , v }

P ij=C iju Pu+C ij

v P v+Lij N

C ijk

Lij

Gauss formula

Γijk

Page 96: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

96

Computer Aided Design

Christoffel symbols

Using Einstein's notation (summation over repeated indices ):

How to compute and ? Multiply by

P ij=C ijk P k+Lij N , i , j , k=u , v

C ijk Lij

P l , l=u , v

P ij⋅P l=C ijk P k⋅P l+Lij N⋅P l

0

Coefficients of the 1st fundamental form = = metric tensorg kl

P ij⋅P l⋅(g kl )−1=C ij

k g kl⋅g kl−1

C ijk=P ij⋅P l⋅g lkC ij

k=P ij⋅P l⋅(g kl )

−1

Conventional notation of the inverse of the metric tensor

Page 97: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

97

Computer Aided Design

Christoffel symbols

Now, multiply by

One recovers the formula seen before:

P ij=C ijk P k+Lij N

N

P ij⋅N=C ijk P k⋅N +Lij N⋅N

0

1

Lij=P ij⋅N

Lij≡M 2 M2=(N⋅Puu N⋅Puv

N⋅Puv N⋅Pvv)

Page 98: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

98

Computer Aided Design

Christoffel symbols

Use of Christoffel symbols and the second fundamental form Let us return to the expression

Now replace by and use the Einstein notation again :

Now substitute

Γ" (t )=u" Pu+v " Pv+u ' 2 Puu+u ' v ' Puv+u ' v ' P vu+v ' 2 P vv

u , v ui , i=1,2

Γ" (t )=(ui)

" P i+(ui)

'⋅(u j

)' P ij

P ij=C ijk P k+Lij N

Γ" (t )=((uk)"+C ij

k(ui

)'⋅(u j

)')P k+(u

i)

'⋅(u j

)' Lij N

Total tangential component Normal component

Page 99: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

99

Computer Aided Design

Christoffel symbols

Used to express curvatures (or second derivatives) in the 3D euclidean space from curvatures (or second derivatives) expressed in the parametric space.

Normal curvature: based on the normal component

If we have an arc-length parametrization :

if not : need to adjust

One recovers the formula :

kn=Lij(u

i)

'(u j

)'

ds2 =Lij(u

i)'(u j

)'

g kl (uk)'(ul

)'

kn=Γ"⋅N =Lij(ui)'(u j

)'

( =j2(d Γuv , d Γ

uv))

(ui)

'⋅(u j

)' Lij N

kN=j2(d Γ

uv , d Γuv)

j1(d Γuv , d Γ

uv)

Page 100: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

100

Computer Aided Design

Christoffel symbols

Geodesic curvature : based on the tangential components

If the curve is parametrized by arc-length :

Therefore, the tangential component of is orthogonal to and to N as well. There is a proportionality factor between and .This factor is the geodesic curvature

((uk)

"+C ij

k(ui

)'⋅(u j

)')P k

Γ"⋅Γ '=0=((uk)

"+C ij

k(ui

)'⋅(u j

)')P k⋅Γ '+(ui

)'⋅(u j

)' Lij N⋅Γ '

Γ '⋅Γ '=1 Γ '⋅Γ"=0=0

Γ"Γ '

Γt "

Γt " N×Γ '

Page 101: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

101

Computer Aided Design

Christoffel symbols

Therefore, , valid only if the parametrization of is normal (arc-length)

If not, need to adjust ...

Some developments* leads to the following identity :

Again, this expression makes only use of derivatives in the parametric space...

kg=[N ,Γ ' ,Γ" ]Γ

kg=√det (M 1)[−C11

2 u ' 3+C 22

1 v ' 3−(2C12

2−C 11

1)u ' 2 v '+(2C12

1−C22

2)u ' v ' 2

+u " v '−v " u ' ]

((u ' v ' )M1(u 'v ' ))

3/2

Γt "=kg (N ×Γ ' ) Γt "⋅(N×Γ ' )=kg(N×Γ ' )⋅(N×Γ ' )

kg=(N×Γ ' )⋅Γt "=(N×Γ ' )⋅Γ"

kg=[N ,Γ ' ,Γ" ]

ds3 =[N ,Γ ' ,Γ " ]

(g kl (uk)

'(ul

)' )

3/2

* see e.g.“Modern Differential Geometry of Curves and Surfaces with Mathematica”, 2nd ed. Boca Raton, FL: CRC Press, pp. 501-518, 1997.

Page 102: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

102

Computer Aided Design

Christoffel symbols

Equations of a geodesic

Need to set that the geodesic curvature is equal to zero.

One obtains a set of differential equations May be used to actually compute an approximation

of the geodesic since it is usually impossible to solve that coupled system of ODEs algebraically.

Page 103: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

103

Computer Aided Design

Parametric representation

Darboux frame and equations

s is the curvilinear abscissa

T s={∂ x s∂ s

,∂ y s∂ s

,∂ z s∂ s }

Su , v

s

uvs:{u=u s

v=v s s: {

x s= f u s , v sy s=g u s , v sz s=hu s , v s

P⃗ (u , v): {x= f (u , v)y=g (u , v)z=h(u , v)

N s= N u s , v s

G⃗ (s)=N⃗×T⃗

Darboux frame

T s

G s N s

Page 104: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

104

Computer Aided Design

Parametric representation

Darboux frame and equations

[d T s

dsd G s

dsd N s

ds]=[

0 g s n s−g s 0 − g s−n s g s 0 ]⋅[

T sG sN s]

S u , v

s

Darboux frame

T s

G sN s

Geodesic torsion (or relative torsion)

Page 105: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

105

Computer Aided Design

Parametric representation

Geodesic torsion

is identically zero iff the curve is along a direction of principal curvature (line of curvature)

Geodesic curvature

is identically zero iff the curve is a geodesic

Page 106: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

106

Computer Aided Design

Parametric representation

In an euclidean space: The shortest line between two points has simple

curvature k equal to zero (= straight line) The minimal surface carried by a curve is of

average curvature kM equal to 0 everywhere

In a non euclidean space (on a surface): The (or one of the) shortest line between two points

on the surface has a geodesic curvature kg equal to

zero (it's a geodesic)

Page 107: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

107

Computer Aided Design

Parametric representation

A good reference on « shape interrogation » Shape interrogation is the ability to get information

from geometric models

N. M. Patrikalakis and T. Maekawa, Shape Interrogation for Computer Aided Design and Manufacturing, Springer Verlag, February 2002. ISBN 3-540-42454-7

(Available as a PDF electronic copy at the library)

Page 108: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

108

Computer Aided Design

Parametric representation

Some results of differential geometry

Gauss-Bonnet's theorem

is Euler's characteristic of surface S

∫S

kT dA+∫∂S

kg ds=2π χ(S )

S

=2 =0=−2

=−4=1

Page 109: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

109

Computer Aided Design

Parametric representation

Application of Gauss-Bonnet's theorem For a polyhedron, we have (Euler's formula) :

We want to approximate a sphere with hexagons ( H ) and pentagons ( P ).

Each pentagon (hexagon) has 5 (6) nodes, shared by 3 faces Each pentagon (hexagon) has 5 (6) edges, shared by 2 faces So the total number of nodes N is ( 5P+6H )/3 Total number of edges E is ( 5P+6H )/2, total number of faces F

is P+H

The sphere is compact and its gaussian curvature is 1/R2

so P=12 … 12 pentagons are necessary and as many hexagons as we want to make soccer ball.

S =N−EF

S =N−EF=5P6H /3−5P6H /2PH=P /6

∫S

T dA∫∂ S

G ds=1

R2∫S

dA=4=2 S

Page 110: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

110

Computer Aided Design

Parametric representation

Page 111: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

111

Computer Aided Design

Explicit curves and surfaces

Page 112: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

112

Computer Aided Design

Explicit forms

Curve as a function

We can swap x, y and z according to needs

y= f x z= f x , y

xOK !

y= f x

y

x

y

xOK !

x= f y

y

KO !

Page 113: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

113

Computer Aided Design

Explicit forms

Polar coordinates Sometimes used. Circle is readily represented :

r =1

Page 114: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

114

Computer Aided Design

Explicit forms

Definition of an explicit surface Depend on reference axis No multiple definitions i.e. unique value of z for a

position (x,y) For a given axes system, only one definition No closed curves /surfaces in one time

Unit circle – we must split it up at least in :

and y=1−x2 y=−1−x2

Page 115: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

115

Computer Aided Design

Implicit representation

Page 116: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

116

Computer Aided Design

Implicit forms

Ex. Unit circle : Infinity of representations of a

given curve Invariance by the multiplication by a constant

We can take absolute value too

... but the form is then not differentiable etc...

f x , y=0

x2 y2

−1=0

k⋅ f x , y=0 ⇔ f x , y=0 ∀ k≠0

∣ f x , y ∣=0 ⇔ f x , y =0

f =0

Page 117: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

117

Computer Aided Design

Implicit forms

Advantages of an implicit form

For a point we know : If it is on the curve : If it is not on the curve : In some cases, we may know if it is inside or

outside the volume delimited by the curve:

If , P is inside the circle

But : has no meaning Multiplication by negative k : interior exterior

P [ x p , y p]

f x p , y p=0f x p , y p≠0

f ( x p , y p)<0 or f ( x p , y p)>0

x p2 y p

2−10

∣x p2 y p

2−1∣0

Page 118: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

118

Computer Aided Design

Implicit forms

Normal forms / Contour line / level sets Particular case of implicit forms such that :

, is the signed distance to the curve In this case, for a point ,

is the distance from the point to the curve. d<0 means usually that the point is inside.

Case of the unit circle :is the distance to the circle.

Unique representation !(except the sign of the distance function – but it indicateswhere is the interior)

x , y =d dx p , y pP [ x p , y p]

x , y= x2 y2

−1

0

0

=0

Page 119: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

119

Computer Aided Design

Implicit forms

Normal forms A normal form is a distance function, we have :

For the circle :

∣∇∣=∣∂

∂ x∂

∂ y∂

∂ z∣=∣

2 x

2 x2 y2

2 y

2 x2 y2

0∣= x2

x2 y2

y2

x2 y2

=1

∣∇ x , y ∣=1

Page 120: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

120

Computer Aided Design

Implicit forms

Normal forms Ellipse ? We can « flatten » a circle :

Set

x* , y*= x*2

y*2−1

y*=2 y ; x*

=x

x , y= x22 y 2−1

0

0

=0

∣∇e∣=∣x

x24 y2

4y

x24 y2

0∣= x2

16 y2

x24 y2 ≠1

Page 121: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

121

Computer Aided Design

Implicit forms

The normal form associated with a curve (or a surface in 3D) is usually nontrivial.

To get it nevertheless: Use of a numerical approximation (spatial discretization) We know the position of the curve or the surface: The normal form is reconstructed in the considered

domain by solving the « Eikonal » equation (from greek « image »):

{|⃗∇ j|=1 in Ωj=0 on Γ

j=0 on Γ

int

ext

Page 122: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

122

Computer Aided Design

Implicit forms

Resolution of the Eikonal equation It is a non-linear, hyperbolic equation « Fast Marching » method

Cf . J.A. Sethian, Fast Marching Methods, SIAM Review (41) 2, pp 199-235, 1999

Consist in a step-by-step construction of the distance field, from the initial front where d = 0.

J.A

. S

etia

n

Page 123: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

123

Computer Aided Design

Implicit forms

Resolution algorithm at first order on a regular grid

Known value in a point = 0 a) Calculation of test points J.A

. S

etia

n

Page 124: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

124

Computer Aided Design

Implicit forms

First order resolution algorithm on a regular grid

b) Among test points, wechoose the one of lowest value

c) We fix it and (re)calculate new test points

J.A

. S

etia

n

Page 125: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

125

Computer Aided Design

Implicit forms

Resolution algorithm at first order on a regular grid

c) We fix it and we recalculate... Here a test point has been computedtwice : we keep the lowest value

b) Among test points, wechoose the one of lowest value

J.A

. S

etia

n

Page 126: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

126

Computer Aided Design

Implicit forms

The former procedure is repeated until all grid points have been fixed.

The result is a (possibly signed) distance field known at each grid point. Interpolation inside square patches makes it continuous.

One can extract an iso-value (e.g. for 0) and consider it as the surface of interest

Also, one may actually modify the field (with transport equations for instance) to change the shape and position of the surface.

Page 127: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

127

Computer Aided Design

Implicit forms

There are algorithms of order 2 or higher It is also possible to solve that equation efficiently

on non regular grids ( unstructured meshes) Example : mesh

Page 128: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

128

Computer Aided Design

Implicit forms

There are algorithms of order 2 or higher It is also possible to solve that equation efficiently

on non regular grids ( unstructured meshes) Example : iso-distance curves

Page 129: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

129

Computer Aided Design

Implicit forms

There are high-performance algorithms to update discretized level-sets Resolution of partial differential equations

cf. J.A. Sethian « Level-Sets Methods and Fast Marching Methods, Evolving interfaces in computational geometry ... », Cambridge University Press, 1999.

Alternative representation of the geometry really useful for real objects (i.e. non perfect)

eg. Medical imaging, « historical » artifacts , etc... But also evolving interfaces (fluid surface, cracks in

solids)

Page 130: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

130

Computer Aided Design

Implicit forms

Transport equation of a level-set

We solve that using explicit time-stepping Normal speed is given (known) Below, the speed is depending on the density ...

∂j

∂ t+V n⋅∇ j⋅⃗n=0

N.

Par

agio

s

Page 131: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

131

Computer Aided Design

Implicit forms

Example of geometries based on « level-sets »

Page 132: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

132

Computer Aided Design

Implicit forms

Example of geometries based on « level-sets »

M.Y

. W

ang

Page 133: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

133

Computer Aided Design

Implicit forms

Some words on differential geometry...

Page 134: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

134

Computer Aided Design

Implicit forms

Normal (ext.) to the curve / surface We use the gradient

Tangent vector for a planar implicit curve Use of a permutation

of the gradient

∇=[∂x , y , z

∂ x∂x , y , z

∂ y⋮

]N =

∣∇∣

is equal to 1 if j is a signed distance ( a normal form )

T =Tan

∣∇∣

Tan =[−∂x , y , z

∂ y∂x , y , z

∂ x]

Page 135: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

135

Computer Aided Design

Implicit forms

Curvature of a planar implicit curve Use of the Hessian matrix

Alternative

notation

H =[∂

2

∂ x2

∂2

∂ x∂ y

∂2

∂ y∂ x∂

2

∂ y2 ]=−T

T∗H ∗T

∣∇∣=

1Ro

=0

Ro

Osculating circle

=−Tan

T∗∇ Tan ×Tan ⋅n3

∣Tan ∣3

Basis vector (along z)

Page 136: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

136

Computer Aided Design

Implicit forms

Demonstration of the equation of the curvature From Frenet equations :

we have :

and so :

now,

=−d N s

ds⋅T s [

d T sds

d N sds

]=[ 0 s−s 0 ]⋅[T s

N s]

=−∂N s∂ x

dxds

∂N s∂ y

dyds ⋅T s

∇ N=[∂Nx

∂ x∂N y

∂ x∂Nx

∂ y

∂N y

∂ y] T s =[

dxdsdyds

]=−T sT

∗∇ N s∗T s

Page 137: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

137

Computer Aided Design

Implicit forms

We have :

Quod Erat Demonstrandum, QED

=−T sT∗∇ N s∗T s=−T

T∗H ∗T

∣∇∣

∇ N=∇ ∇

∣∇∣=∣∇∣∇ ∇ −∇ ∣∇∣∇

∣∇∣2

∇ ∇ =H ∇⋅T=∣∇∣⋅N⋅T=0

Page 138: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

138

Computer Aided Design

Implicit forms

Curvature of a surface There are 2 curvatures :

Gaussian curvature ( = total curvature ) kT

Average curvature kM .

These are related to principal curvatures kmin

and

kmax

(curvature measured along principal

directions) :

Along principal directions T1 and T

2 , curvatures are

extrema ( kmin

or kmax

)

min ,max=M±M2−T M=

minmax

2T=minmax

Page 139: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

143

Computer Aided Design

Implicit forms

Direct expression of principal directions Complicated but explicit formulas exist

Cf.Erich Hartmann, On the curvature of curves and surfaces defined by

normalforms, Computer Aided Geometric Design 16, pp. 355-376, 1999.

Numerical expression of the curvatures Cf. sequel...

Page 140: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

144

Computer Aided Design

Implicit forms

Numerical expression of the curvatures Conjugate transpose Hessian matrix (matrix of the

cofactors) :

H =[∂

2

∂ x2

∂2

∂ x∂ y∂

2

∂ x∂ z

∂2

∂ y∂ x∂

2

∂ y2

∂2

∂ y∂ z

∂2

∂ z ∂ x∂

2

∂ z ∂ y∂

2

∂ z2]=[

, xx , xy , xz

, yx , yy , yz

, zx , zy , zz]

H*=[

, yy , zz− , zy , yz , yz , zx− , yx , zz , yx , zy− , yy , zx

, xz , zy− , xy , zz xx , zz− , xz , zx , xy , zx− , xx , zy

, xy , yz− , xz , yy , yx , xz− , xx , yz , xx , yy− , xy , yx]

Page 141: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

145

Computer Aided Design

Implicit forms

Expression of curvatures of an implicit surface

T=∇

T∗H*

∗∇

∣∇∣4

M=∇

T∗H ∗∇−∣∇∣

2

⋅traceH

2∣∇∣3

Page 142: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

146

Computer Aided Design

Implicit forms

Implicit curves in 3D

Page 143: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

147

Computer Aided Design

Implicit forms

Curve in 3D Intersection of two implicit surfaces

TN

B

{ x , y , z =0 } ∩ { x , y , z =0 }

Page 144: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

148

Computer Aided Design

Implicit forms

Tangent

Curvature For planar curves : By substituting ... (we must take the norm , because

that vector is not along n3 anymore)

Tan ,=∇ x , y , z ×∇ x , y , z

T ,=Tan ,∣Tan ,∣

=1 if we deal with two normal forms that are “orthogonal”

=∣Tan ,T∗∇ Tan , ×Tan ,∣

∣Tan ,∣3

=− Tan

T∗∇ Tan ×Tan ⋅n3

∣Tan ∣3

Page 145: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

149

Computer Aided Design

Implicit forms

Torsion The formulas are obtained from the definition of the

torsion for the parametric curves We set :

Note : the curvature, written with the same kind of notation, is :

T *=Tan ,=∇x , y , z ×∇ x , y , z

T **=T *

∗∇ T *

T ***=T *

∗∇ ∇ T * ∗T * TT *

∗∇ T *∗∇ T *

=T * ,T ** ,T ***

∣T *×T **∣

2

=∣T *

×T **∣

∣T *∣3

Page 146: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

150

Computer Aided Design

Implicit forms

Volume operations on contour lines (level-sets) We can represent a volume as the set of points

such as

Manipulations of volumes Union, intersection, etc...

≤0

Page 147: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

151

Computer Aided Design

Implicit forms

Compounds of level-sets Union

Intersection

Complement

Difference

u=1∪2

i=1∩2

d=1∖2=1∩2

u x , y =min [1 x , y ,2 x , y]

i x , y=max [1 x , y ,2 x , y]

d x , y=max [1 x , y ,−2 x , y]

c=

c x , y =−x , y

Page 148: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

152

Computer Aided Design

Implicit forms

Disc

Square 4 half planes !

d x , y= x2 y2

−1

1

2

3 4

c1 x , y= y

2 x , y =− y2

3 x , y=−x0.2

4 x , y =x−1.8

Region of interest

Page 149: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

153

Computer Aided Design

Implicit forms

1

2

3 4

c

Region of interest

Use of intersections for the square :

Finally, difference between and

sq=1∩2∩3∩4

d x , y= x2 y2

−1

sq x , y=max [1,2,3,4]

dsq

f x , y=max [sq ,−d ]

f=sq∖d

f x , y =max [1,2,3,4,−d ]

Page 150: CAD course Master in Aerospace and Mechanical Engineering · Master in Aerospace and Mechanical Engineering. 2 ... the project and the final ... Catia, Unigraphics

154

Computer Aided Design

Implicit forms

Disadvantges of an implicit representation Obtaining points on the curve/surface :

Resolution of a set of non-linear equations Not very robust, and slow No parametrization , no « explicit » orientation

Discretization of the curve/surface(« rasterization ») From a point, use of specific algorithms (“marching

cubes”) Not always possible and/or robust