Astronomie si astrofizica_problema Kepler.ppt

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    Kepler laws

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    The two-body problem

    What defines the problem? A large planet and a smaller satellite

    Different views on the solar system Nicolaus Copernicus

    Tycho Brahe Johannes Kepler

    Keplers laws on orbit motions Elliptical orbits within an orbital plane

    Equal area law

    Scale vs orbital period law

    Equations of Motion

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    Keplerian Laws

    Law I

    Each planet revolves around the Sun in anelliptical path, with the Sun occupying one ofthe foci of the ellipse.

    Law II

    The straight line joining the Sun and aplanet sweeps out equal areas in equalintervals of time.

    Law III The squares of the planets' orbital periods

    are proportional to the cubes of the semi-major axes of their orbits.

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    Keplers first law

    )cos(1

    )1()(

    2

    e

    ear

    rThere are 4 cases:

    e=0, circle

    0

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    In-plane Kepler parameters

    )1(ear )1( ear

    ea

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    Keplers second law

    D

    B

    O

    C

    A

    ABO CDO

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    Keplers Third law

    nT 2)(32 mMGan

    The variable n represents the mean motion in radians persecond, a is the semi-major axis, G is the gravitational

    constant, Mis the mass of the Sun, m is the mass of the

    satellite (m

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    How to obtain r()

    A particle moves in a central force field The motion takes place within an orbital plane

    The solution of the equation of motion isrepresented in the orbital plane

    Substitution 1: polar coordinates in the orbitalplane

    Substitution 2: replace r by 1/u

    Analogy with a mathematical pendulum

    Solve this an substitute elliptical configuration Final step: transformation orbital plane to 3D

    (this gives us the set of 6 Keplerian elements)

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    Mathematics on r():

    Substitute:

    Characteristic:

    (h = length ang mom vector)

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    Velocity and Position

    (aka vis-viva equations)

    arGMv

    Eea

    e

    ear

    12

    )cos.1(

    cos1

    )1( 2

    radius r

    velocity v

    Note: in this case only , or E or M depend on time.

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    Total Energy

    The total energy inthe system is the

    sum of kinetic and

    potential energy

    For the Kepler

    problem one can

    show that the total

    energy is half thatof the potential

    energy

    ca

    a

    GMc

    mc

    r

    GMmmv

    EEE totpotkin

    2atEnergyPotential

    2

    .

    2

    1 2