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STiCM Select / Special Topics in Classical Mechanics P. C. Deshmukh Department of Physics Indian Institute of Technology Madras Chennai 600036 [email protected] STiCM Lecture 13: Unit 4 Symmetry and Conservation Laws Dynamical Symmetry in the Kepler Problem 1 PCD_STiCM

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  • STiCM

    Select / Special Topics in Classical Mechanics

    P. C. Deshmukh

    Department of Physics

    Indian Institute of Technology Madras

    Chennai 600036

    [email protected]

    STiCM Lecture 13: Unit 4

    Symmetry and Conservation Laws

    Dynamical Symmetry in the Kepler Problem

    1 PCD_STiCM

  • 2

    Unit 1 : Equations of Motion (Newton / Lagrange / Hamilton )

    Unit 2: Oscillators (Free/damped/driven), Resonances, Waves

    Unit 3: Polar Coordinate Systems

    Unit 4 : Dynamical Symmetry in the Kepler Problem

    Symmetry Conservation laws (Noether)

    PCD_STiCM

  • Unit 4: Learning goals: Recapitulate:

    Conservation of energy that is well-known in the Kepler-Bohr

    problem stems from the symmetry with regard to temporal

    translations (displacements on the time axis).

    Conservation of angular momentum, likewise, stems from the

    central field symmetry in the Kepler problem.

    Neither of these accounts for the fact that the Kepler ellipse

    remains fixed; that the ellipse does not undergo a ‘rosette’

    motion.

    GETTING CONSERVATION LAWS FROM THE EQUATION OF MOTION

    3 PCD_STiCM

  • This unit will discover the ‘dynamical’

    symmetry of the Kepler problem and

    its relation with the constancy

    (conservation) of the LRL vector,

    which keeps the orbit ‘fixed’.

    Motivation: Connection between symmetry &

    conservation laws has important

    consequences on issues at the very frontiers

    of physics and technology.

    Mechanics of

    Flights into Space 4 PCD_STiCM

  • 5

    Mechanics of Flights into Space

    Konstantin Tsiolkovsky

    (1857-1935)

    Robert H. Goddard

    (1882-1945)

    Hermann

    Oberth

    (1894-1989)

    Dr. Vikram

    Sarabhai

    Father of India’s

    Space Program

    PCD_STiCM

  • 6

    Indian Space Research Organisation (ISRO)

    [1] Indian National Satellites (INSAT)

    - for communication services

    [2] Indian Remote Sensing (IRS) Satellites

    - for management of natural resources

    [3] Polar Satellite Launch Vehicle (PSLV)

    - for launching IRS type of satellites

    [4] Geostationary Satellite Launch Vehicle (GSLV)

    - for launching INSAT type of satellites. PCD_STiCM

  • 7

    Gravity plays the most important role in

    designing satellite trajectories,

    of course,

    and hence we study the Kepler TWO-BODY

    problem

    We must then adapt the formalism to

    understand the models, methods

    and applications of satellite orbits,

    etc. PCD_STiCM

  • 8

    Other than ‘energy’ and ‘angular momentum’, what else

    is conserved, and what is the associated symmetry?

    For given physical laws of nature, what

    quantities are conserved?

    Rather, if you can observe what physical quantities

    are conserved, can you discover the physical laws

    of nature?

    PCD_STiCM

  • 9

    How did Kepler deduce that planetary orbits are

    ellipses around the sun ?

    Kepler had no knowledge of :

    (a) differential equations

    (b) inverse square force

    (gravity).

    Johannes Kepler

    1571- 1630

    How would you solve this

    problem?

    PCD_STiCM

  • 10

    Kepler got his elliptic orbits not

    by solving differential

    equations for gravitational

    force, but by doing clever

    curve fitting of Tycho Brahe’s

    experimental data.

    How did Kepler deduce that planetary

    orbits are ellipses around the sun ?

    PCD_STiCM

  • 11

    Tycho Brahe (1546-1601):

    Danish astronomer appointed as the imperial astronomer under

    Rudolf II in Prague, which then came under the Roman empire.

    Brahe had his own “Tychonian” model of planetary motion:

    Brahe had planets revolve around the sun (like the Copernican

    system), and the sun and the moon going around the earth (like

    the system of Ptolemy).

    What was Brahe’s nose was made of ?

    PCD_STiCM

  • 12

    Tycho Brahe (1546-1601):

    He discovered the supernova in 1572, in

    “Cassiopeia’.

    Kepler and Brahe never could collaborate

    successfully.

    They quarreled, and Tycho did not provide Kepler

    any access to the high precision observational data

    he (Brahe) had complied.

    It was only on his deathbed, saying

    “……let me not seem to have lived in vain…….”

    that Brahe handed over his observational data to

    Kepler [Ref.:Sagan]. PCD_STiCM

  • 13

    Galileo Galilei 1564 - 1642

    Isaac Newton (1642-1727)

    Causality, Determinism, Equation of Motion

    ‘Dynamics’ came well AFTER KEPLER!

    Johannes Kepler

    1571- 1630

    PCD_STiCM

    http://en.wikipedia.org/wiki/Image:Galileo.arp.300pix.jpg

  • 14

    Two-body problem

    1R

    2R

    2 1 r R Rˆ

    ru

    r

    _1_ _ 2

    1 22 2 2

    2 1

    ˆ

    by onF

    m mm R G u

    R R

    1m

    2m

    _ 2_ _1

    1 21 1 2

    2 1

    ˆ

    by onF

    m mm R G u

    R R

    PCD_STiCM

  • CMR

    15

    Two-body problem: Centre of Mass

    1R

    2R

    1m

    2m

    1 1 2 2

    1 2

    CM

    m R m RR

    m m1 1 CMr R R

    2 2 CMr R R

    1 1 2 2 1 1 2 2

    1 1 2 2 1 2

    ( ) ( )

    0.

    CM CM

    CM

    m r m r m R R m R R

    m R m R m m R

    2 1 2 1 r R R r r

    1 2m m

    PCD_STiCM

  • 16

    2 1 1 2 3

    3 1 1 22 1...where ....for

    rr R R G m m

    G m m Gmr

    m

    r

    rm

    _1_ _ 2

    1 22 2 2

    2 1

    ˆ

    by onF

    m mm R G u

    R R

    _ 2_ _1

    1 21 1 2

    2 1

    ˆ

    by onF

    m mm R G u

    R R

    30.

    rr

    r

    This equation of motion describes the

    ‘relative motion’ of the smaller mass

    relative to the larger mass, assuming that

    the difference in the masses is huge.

    2 1 2 1 r R R r r

    ˆ r

    ur

    3 2LT PCD_STiCM

  • 17

    30.

    rr

    r

    30r r r r

    r

    ˆ ˆˆru rur r rrru v vv vrr

    3vv 0rr

    r

    0

    20

    limv

    v limt

    t

    r

    t

    t r

    We now take the dot product of the

    velocity with the ‘Eq. of motion’:

    ˆ ˆ ˆd d

    r r ru ru rudt dt

    PCD_STiCM

  • 18

    30.

    rr

    r

    0

    20

    limv

    v limt

    t

    r

    t

    t r

    2

    2

    v

    2

    v

    2

    Er

    Er

    Total ‘SPECIFIC’

    (i.e. per unit mass)

    MECHANICAL

    ENERGY: Constant

    of integral /

    Constant of Motion.

    INVARIANCE,

    SYMMETRY.

    We took the dot product of the ‘Eq. of

    motion’ with velocity:

    Integration

    w.r.t. time

    Differentiation

    w.r.t. time

    2 2

    3 2

    DIMENSIONS

    E L T

    L T

    PCD_STiCM

  • 19

    30.

    rr

    r

    30r r r r

    r

    Equation of Motion

    We took the dot product of the ‘Eq. of motion’ with velocity:

    2v

    2E

    r

    …….. and discovered a CONSERVED QUANTITY!

    E: constant

    symmetry with respect to translations in time.

    (E,t): canonically conjugate pair of variables PCD_STiCM

  • 20

    We now take the cross product of the position vector with the

    ‘Eq. of motion’:

    30.

    rr r r

    r

    : 0 Therefore r r

    , ( ) 0d

    Now r r r r r r r rdt

    = v is also a constant of motion.

    SPECIFIC ANGULAR MOMENTUM

    Therefore H r r r

    INVARIANCE, SYMMETRY

    Force: RADIAL

    central force symmetry

    PCD_STiCM

  • Homogeneity of time

    Homogeneity of space

    Translational Symmetry

    Conservation of energy

    Conservation of linear

    momentum

    Isotropy of space

    Rotational Symmetry Conservation of angular

    momentum

    Emmy Noether

    1882 to 1935

    SYMMETRY CONSERVATION

    LAWS

    Her entry to the Senate of the University of Gottingen,

    Germany, was resisted.

    David Hilbert argued in favor of admitting her to the University

    Senate. 21 PCD_STiCM

  • 22

    Time is homogeneous:

    Lagrangian of a closed system

    does not depend explicitly on time.

    Hamiltonian / Hamilton’s Principal Function

    q - is a CONSTANT.

    LL

    q

    HamiltonianConservation of Energy is

    thus connected with the

    symmetry principle

    regarding invariance with

    respect to temporal

    translations.

    “ENERGY”

    0

    L

    t

    PCD_STiCM

  • 23

    since 0, this means . . is conserved.

    . ., is independent of time, is a constant of motion

    L d L Li e p

    q dt q q

    i e

    Space is homogenous and isotropic

    Law of conservation of momentum,

    arises from the homogeneity of space.

    the condition for homogeneity of space : ( , , ) 0

    . ., 0

    which implies 0 where , ,

    L x y z

    L L Li e L x y z

    x y z

    Lq x y z

    q

    Symmetry Conservation Laws

    PCD_STiCM

  • ( )

    1

    ( )

    1

    Displacement is arbitrary, hence, 0;

    . . 0 =

    Thus P is conserved in the absence of external forces.

    Ni

    kk

    Ni

    kk

    F

    d di e p P

    dt dt

    The conservation of momentum was secured in ‘Unit 1’ on

    the basis of ‘translational invariance in homegenous

    space’, and not on the basis of Newton’s III law.

    ( )

    1

    0 N

    i

    kk

    F S

    24 PCD_STiCM

  • 25

    Given the symmetry related to

    translation in homogenous

    space, could you have

    discovered Newton’s 3rd law?

    2 1

    12 21

    0

    d P

    dt

    d p d p

    dt dt

    F F

    PCD_STiCM

  • 26

    Are the conservation principles consequences of the laws of

    nature? Or, are the laws of nature the consequences of the

    symmetry principles that govern them?

    Until Einstein's special theory of relativity,

    it was believed that

    conservation principles are the result of the laws of nature.

    Since Einstein's work, however, physicists began to analyze

    the conservation principles as consequences of certain

    underlying symmetry considerations,

    enabling the laws of nature to be revealed from this analysis.

    PCD_STiCM

  • 27

    Instead of introducing Newton’s III law as a

    fundamental principle,

    we deduced it (in Unit 1) from symmetry / invariance.

    This approach places SYMMETRY ahead of LAWS OF NATURE.

    It is this approach that is of greatest value to contemporary

    physics. This approach has its origins in the works of

    Albert Einstein, Emmily Noether and Eugene Wigner.

    (1882 – 1935) (1902 – 1995) (1879 – 1955) PCD_STiCM

  • 28

    30.

    rr

    r Equation of Motion for

    Kepler’s two-body problem

    We shall get yet another constant of motion, a

    conserved quantity, by taking the cross product of

    the ‘SPECIFIC ANGULAR MOMENTUM with

    the equation of motion:

    30.

    rH r H

    r

    H

    = v,

    the SPECIFIC ANGULAR MOMENTUM

    H r r r

    PCD_STiCM

  • 29

    3

    3

    v 0

    v - v 0

    H r r rr

    H r r r r rr

    30.

    rH r H

    r

    ˆ ˆ: vd dr

    Use r r re r e rrdt dt

    23 v - 0H r r rrrr

    PCD_STiCM

  • 30

    since, v .. 0d d

    Now H H r H r Hdt dt

    2 2

    3

    2

    ˆv v - 0

    vv 0

    dH r r re

    dt r

    d rH r

    dt r r

    v 0

    v 0

    d d rH

    dt dt r

    d rH

    dt r

    23 v - 0H r r rrrr

    PCD_STiCM

  • 31

    v 0

    ˆv ,

    constant

    d rH

    dt r

    H e A

    LAPLACE – RUNGE – LENZ

    VECTOR

    Observe how a

    constant of

    motion has

    emerged –

    - yet again

    -– by playing with

    the equation of

    motion!

    ˆv , constantA H e

    3 2

    1 2 1 3 2v

    L T

    H LT L T L T

    Physical

    Dimensions PCD_STiCM

  • 32

    We will take a Break… …… Any questions ?

    [email protected]

    Next Lecture: Dynamical Symmetry

    of the Kepler Problem

    References:

    [1] Oliver Montenbruck and Eberhard Gill

    ‘Satellite orbits – Models, Methods, Applications’.

    (Springer, Berlin, 2000)

    [2] Francis J. Hale

    ‘Introduction to Space Flight’

    (Prentice Hall, Englewood Cliffs, 1994)

    PCD_STiCM

  • STiCM

    Select / Special Topics in Classical Mechanics

    P. C. Deshmukh

    Department of Physics

    Indian Institute of Technology Madras

    Chennai 600036

    [email protected]

    STiCM Lecture 14: Unit 4

    Symmetry and Conservation Laws

    Dynamical Symmetry in the Kepler Problem

    33 PCD_STiCM

  • 34

    Take dot product with :

    Equation to the orbit / trajectory

    Without solving the differential equation of motion!

    r

    LAPLACE – RUNGE – LENZ VECTOR

    ˆv , constantH e A

    PCD_STiCM

  • 35

    Take dot product with : r

    2

    ,

    cosH r A r Ar

    A r

    ˆv H e A where vH r

    : vsign reversal H r r A r

    vH r r A r

    v H r r A r

    Interchange ‘dot’ and ‘cross’:

    PCD_STiCM

  • 36

    2 cos

    ,

    H r Ar

    A r

    ,A r

    X

    2

    2

    2

    cos

    cos 1 cos1 cos

    r A H

    HH p

    rAA

    What is ?A PCD_STiCM

  • ,A r

    X

    F

    37 PCD_STiCM

  • 38

    vr

    H Ar

    2 2 22

    v vH H r Ar

    0 0v , 90 & , v 90

    ˆv v

    H r H r H

    H H u

    2v v v v v - vH r r r

    22 2 2

    2 2 2

    v v v - v v cos v

    v sin

    H r r r r r r r

    r

    2 2 2 2 2 2 22v v sinH r Ar

    , vr

    PCD_STiCM

  • 39

    2 2 2 2 2 2 22v v sinH r Ar

    2 2 2 2 2 2 2

    2

    2v v sinH r A

    rH

    2 2 2 22vH Ar

    2 2 22H E A

    2 22 2

    21

    H E A

    2

    2

    21

    A EH

    v H r

    PCD_STiCM

  • 40

    2 2

    2

    1 cos

    2 & 1

    pr

    with

    H A EHp

    PCD_STiCM

  • 41

    1 cos

    1:

    1:

    0 1:

    0 :

    pr

    Hyperbola (open trajectory)

    Parabola (open trajectory)

    Ellipse (closed trajectory)

    Circle degenerate ellipse

    For satellite

    and ballistic

    missile

    trajectories,

    ellipses

    (inclusive of

    the circle) are

    of primary

    interest. PCD_STiCM

  • 42

    1 cos

    1:

    1:

    0 1:

    0 :

    pr

    Hyperbola (open trajectory)

    Parabola (open trajectory)

    Ellipse (closed trajectory)

    Circle degenerate ellipse

    1 1

    Deep space probes

    leave earth’s gravity

    on hyperbolic orbits

    Earth-orbiting

    satellites are in

    elliptic motion.

    0 1

    PCD_STiCM

  • 43

    b

    a

    Increasing eccentricity

    e=0 e=0.5 e=0.75 e=0.95

    2

    2

    semi-major axis

    semi-minor axis

    1

    a

    b

    be

    a:e eccentricity

    Focus

    b a

    PCD_STiCM

  • minr

    44

    X

    min min when 0 : 1

    pr r r

    maxr perigee

    apogee

    ; 1 cos

    pr

    2 2

    2

    2 & 1

    H A EHp

    perigee

    apogee max max when : 1

    pr r r

    0 1

    PCD_STiCM

  • 45

    2 2

    21 co

    2;

    s ; 1

    Hpr

    EHp

    rrperigee

    2a

    2b At apogee/perigee: 2 , constantr r a

    2

    2

    22

    1 1 1

    1

    perigee apogee

    p p pa r r

    p a

    211 cos

    ar

    2 2 2 for circular orbit2

    1 1

    2 2 2E

    H p a

    apogee

    PCD_STiCM

  • 46

    24 GPS satellites ---- Wikimedia Commons

    http://en.wikipedia.org/wiki/File:ConstellationGPS.gif PCD_STiCM

  • 47

    1̂e1

    ˆe

    X

    Y

    O

    “Unit Circle”

    1

    ˆ ˆv e e

    2

    v

    ˆ ˆ ˆ

    ˆz

    H r

    e e e

    e

    Plane/Cylindrical Polar Coordinate System

    ˆ ˆ ˆ, , ze e e ˆvA H e

    PCD_STiCM

  • 48

    The

    (specific)

    angular

    momentum

    vector is

    out of the

    plane of

    this figure,

    toward us.

    Laplace Runge Lenz Vector

    is constant for a strict

    potential.

    v

    H

    A

    v H

    S

    1r

    ˆvA H e PCD_STiCM

  • v

    l

    H

    êv H

    S

    ˆ - - : ,

    ˆv

    p lThe Laplace Runge Lenz vector A e

    or alternatively defined in terms

    of the specific angular momentum H as

    A H e

    49 PCD_STiCM

  • 50

    ˆvA H e

    ˆvv

    dedA d dHH

    dt dt dt dt

    ˆv dedA dH

    dt dt dt

    ˆ ˆˆ

    de eBut e

    dt

    dA dH e

    dt dt

    Central Field Symmetry

    Angular Momentum

    is Conserved

    PCD_STiCM

  • 51

    ˆvA H e

    dA dH e

    dt dt

    We must know the form of the interaction

    vWhat is the form of the force : ?

    per unit ma

    !

    s

    sd

    dt

    vdF ma m

    dt

    PCD_STiCM

  • 52

    2v

    2E

    r

    2per unit m :

    vˆThe for ace ss -

    de

    dt

    vˆH

    dA de

    dt dt

    22- ˆˆ ˆzdA

    dte e e

    0dA

    dt

    ˆ ˆ ˆ, , : ˆ ˆ ˆ

    z

    z

    e e e right handed basis set

    e e e

    PCD_STiCM

  • 53

    For this potential and for the

    associated field:

    no precession of orbit.

    The constancy of the orbit

    suggests a conserved quantity

    and one must look for an

    associated symmetry.

    Angular momentum is

    conserved,

    but major-axis not fixed.

    Rosette motion

    Two-body central field Kepler-Bohr

    problem,

    Attractive force:

    inverse-square-law.

    PCD_STiCM

  • 54

    Conclusion: 0d A

    dt

    ˆvA H e

    0A H LRL vector is in the plane of the orbit

    perigee

    A

    Direction of the LRL vector is: focus to perigee.

    : Must remain constant

    – no matter where the planet is! A

    This is precisely what FIXES the orbit!

    Find the direction of at the perigee. A

    H

    PCD_STiCM

  • 55

    Given the constancy related to the conservation of

    the LRL vector, could you have discovered the law of

    gravity?

    If you did that, wouldn’t you

    have discovered a law of nature?

    2

    vˆForce (per unit mass):

    Newton told us (but first, to Halley)!

    de

    dt

    Newton

    Halley PCD_STiCM

  • 56

    “It is now natural for us to try to derive the laws of nature

    and to test their validity by means of the laws of invariance,

    rather than to derive the laws of invariance from what we

    believe to be the laws of nature.” - Eugene Wigner

    Symmetry & Conservation Principles!

    Emmily

    Noether

    (1882 – 1935)

    Eugene

    Paul

    Wigner

    (1902-1995)

    PCD_STiCM

  • 57

    Pierre-Simon Laplace

    1749 - 1827

    Carl David Tolmé

    Runge

    1856 - 1927

    Wilhelm

    Lenz

    1888 -1957

    Symmetry of the H atom: ‘old’

    quantum theory. En ~ n-2

    ˆv

    Laplace Runge Lenz Vector :

    1constant for a strict potential.

    A H e

    r

    Conservation law associated

    with ‘dynamical / accidental ’

    symmetry.

    PCD_STiCM

    http://en.wikipedia.org/wiki/Image:CarleRunge.jpg

  • 58

    Further reading: • Symmetry & Conservation laws play an

    important role in understanding the very frontiers

    of Physics.

    • The implications go as far as testing the

    ‘standard’ model of physics, and exploring if

    there is any physics beyond the standards

    model. Do visit:

    Feynman's Messenger Lectures Online

    AKA Project Tuva

    http://www.fotuva.org/news/project_tuva.html PCD_STiCM

  • PCD_STiCM 59

    P. C. Deshmukh and Shyamala Venkataraman

    Obtaining Conservation Principles from Laws of Nature -- and the

    other way around!

    Bulletin of the Indian Association of Physics Teachers, Vol. 3, 143-

    148 (2011)

    P. C. Deshmukh and J. Libby

    (a) Symmetry Principles and Conservation Laws in Atomic

    and Subatomic Physics -1

    Resonance, 15, 832 (2010)

    b) Symmetry Principles and Conservation Laws in Atomic and

    Subatomic Physics -2

    Resonance, 15, 926 (2010)

    Useful references on ‘Symmetry & Conservation Laws’

  • 60

    Continuous Symmetries - Translation, Rotation

    Dynamical Symmetries - LRL, Fock Symmetry

    SO(4)

    Discrete Symmetries

    - P : Parity

    - C : Charge Conjugation

    - T : Time Reversal

    PCD_STiCM

  • 61

    Lorentz symmetry: associated with the PCT symmetry.

    PCT theorem (Wolfgang Pauli)

    No experiment has revealed any violation of PCT symmetry.

    This is predicted by the Standard Model of particle physics.

    PCD_STiCM

  • 62

    The ‘standard model’ unifies all the

    fundamental building blocks of matter,

    and three of the four fundamental forces.

    The Standard Model today

    To complete the Model a new particle is needed – the Higgs

    Boson – that the physics community hopes to find in the new

    built accelerator LHC at CERN in Geneva. PCD_STiCM

  • 63

    Yoichiro Nambu

    ½ prize

    Enrico Fermi Institute,

    Chicago, USA

    Makoto Kobayashi

    ¼ prize

    High Energy

    Accelerator

    Research Organization,

    Tsukuba, Japan

    Toshihide Maskawa

    ¼ prize

    Kyoto Sangyo Univ,

    KyotoJapan

    "for the discovery of the

    mechanism of spontaneous

    broken symmetry in

    subatomic physics"

    "for the discovery of the origin of

    the broken symmetry which

    predicts the existence of at least

    three families of quarks in nature"

    2008 Nobel Prize in Physics

    PCD_STiCM

  • 64

    ‘every symmetry in nature yields

    a conservation law

    and conversely,

    every conservation law reveals

    an underlying symmetry’.

    Noether’s theorem

    PCD_STiCM

  • 65

    “In the judgment of the most competent living

    mathematicians, Fräulein Noether was the most significant

    creative mathematical genius thus far produced since the

    higher education of women began.”

    “In the realm of algebra, … , she discovered methods which

    have proved of enormous importance …. ”

    “………. Her unselfish, significant work over a period of many

    years was rewarded by the new rulers of Germany with a

    dismissal, which cost her the means of maintaining her

    simple life and the opportunity to carry on her mathematical

    studies……”

    ALBERT EINSTEIN. Princeton University, May 1, 1935.

    New York Times May 5, 1935, Excerpts http://www-history.mcs.st-and.ac.uk/history/Obits2/Noether_Emmy_Einstein.html

    PCD_STiCM

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    We will take a Break… …… Any questions ?

    [email protected]

    Next: Unit 5: Inertial and non-inertial reference frames.

    Moving coordinate systems. Pseudo forces.

    Inertial and non-inertial reference frames.

    ‘Deterministic’ cause-effect relations in inertial frame,

    and their modifications in a non-inertial frame. PCD_STiCM