laws of planetary motionastrolab/files/lecture9_lab3... · 2016-11-23 · we need to describe a...
TRANSCRIPT
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LawsofPlanetaryMotion
Check out Planetarium Software: http://stellarium.org
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Kepler’sLawsofPlanetaryMotion
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Sun
Planet
Kepler’sLawsofPlanetaryMotion
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“ReminderoftheGravity”
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F1 =m1v12 / r1 =4p2m1r1/P2(ß v1 =2pr1/P)
F2 =m2v22 / r2 =4p2m2r2/P2
r1 / r2 =m2 /m1 &a = r1 + r2
® r1 =m2a /(m1 +m2)orr2 =m1a /(m1 +m2)
Fgrav = F1 = F2 = Gm1m2 / a2
GravityGeneral
Newton’sformofKepler’s3rd law
YoucandriveKepler’s3rd lawdirectlyfromthegravity.
Foraboundsystem:
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Describablebyrμ &vμ
L&Econservation
Equationofaconicsection.
Threesolutionsforrfordifferente.
Ellipse!
Eccentricity
Parabola!
Hyperbola!
“Reduced-massSolution”
Let’schangethe2-bodyproblemto1-bodyproblemaroundthecenterofmass!
GravityGeneral
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● Threedifferentorbitsarepossible:elliptical,parabolic,&hyperbolic;● Ellipticalforboundsystems(E<0;e.g.,solarsystemplanets);parabolicforE=0;hyperbolicforopen(E>0;unbound)systems;● “Kepler’slawsrepresentthecaseforboundsystems(motionsaroundCM)”
Whycouldn’tKeplerknowtheexistenceoftheparabolicand/orhyperbolicorbits?
WhereistheCMoftheSolarsystem?
Ellipse!
Parabola!
Hyperbola!
Newton’sformofKepler’s3rd law(seenextslides)
Generalsolutionofbound2-bodyorbit
“Reduced-massSolution”
Let’schangethe2-bodyproblemto1-bodyproblemaroundthecenterofmass!
GravityGeneral
2-BodyProblem
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ConicSections
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Parabola: Thesetofallpointsintheplanewhosedistancesfromafixedpoint,calledthefocus,andafixedline,calledthedirectrix,arealwaysequal.
Hyperbola: Thesetofallpointsintheplane,thedifferenceofwhosedistancesfromtwofixedpoints,calledthefoci,remainsconstant.
Ellipse:Acurveonaplanesurroundingtwofocalpointssuchthatastraightlinedrawnfromoneofthefocalpointstoanypointonthecurveandthenbacktotheotherfocalpointhasthesamelengthforeverypointonthecurve.
ConicSections
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“ConicSections”2-bodygravitysystempredictsorbitsofconicsections
GravityGeneral
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Hyperbola!
Orbitsof2-bodygravityproblemCircularVelocity EscapeVelocity
• Circularorbitisthespecialcaseoftheellipticorbits.
• v<vE →Ellipse
• v=vE →Parabola
• v>vE →Hyperbola
GravityGeneral
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Example:2-bodyorbit“Cometshaveellipticalorparabolic/hyperbolicorbits”
Orbits of Comet Kohoutek (red) and Earth (blue), illustrating the high eccentricity of the orbit and more rapid motion when closer to the Sun.
CometsofhyperbolicorbitswillleavetheSolarsystemattheend(cf:non-periodiccomets)
GravityGeneral
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SolarSystemPlanets(inellipticalorbits)
Planetaryorbitsareinclined.
X
X
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OrbitalElementsSohowmanyparameters(=orbitalelements)doweneedtodescribeaplanetaryorbit?
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OrbitalElementsSohowmanyparameters(=orbitalelements)doweneedtodescribeaplanetaryorbit?
Referenceplane(e.g.,ecliptic,equatorial)
Planetaryorbitalplane
PlanetaryorbitalplaneReferenceplane(e.g.,ecliptic,equatorial)
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OrbitalElementsSohowmanyparameters(=orbitalelements)doweneedtodescribeaplanetaryorbit?
Referenceplane(e.g.,ecliptic,equatorial)
Planetaryorbitalplane
PlanetaryorbitalplaneReferenceplane(e.g.,ecliptic,equatorial)
1.Weneedtoknowthesizeandshapeoftheellipticalorbititself.
2.Weneedtoknowtheorientationsoftheorbit.
3.Weneedareferencetime.
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OrbitalElements
Vernalpoint Ascendingnode
1.Semi-majoraxis(a)andeccentricity(e).
2.Inclination(i),longitudeofascendingnode(W),argumentofperihelion(w):ß 3angles;W andw aremeasuredinthecounter-clockwisedirectionandshowthelocationofthenodeandrotationoftheplane,respectively.
3.Epochofperihelion(t).
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From Wikipedia
Motion of an asteroid w.r.t. background stars
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TheSolarSystemTodayandThePossibleDiscoveryofaNinthPlanet