Kepler's Laws of Planetary Motion and Orbital Mechanics, Slides of Physics

An overview of kepler's laws of planetary motion, including the elliptical shape of planetary orbits around the sun, the equal area swept out in equal times, and the relationship between the orbital period and the semi-major axis. The document also discusses the mechanical energy and orbit families of two-body systems, and the conservation of angular momentum in planetary orbits.

Typology: Slides

2012/2013

Uploaded on 07/26/2013

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1) !Planets move in ellipses of semi-major axis a with the sun
at a focus.!
An ellipse has eccentricity e, where ea is the distance from
the center to a focus. !
perihelion - !
Rp = a(1–e) !
closest point !
in sun-planet !
orbit!
aphelion - !
Ra = a(1+e) !
farthest point!
in sun-planet!
orbit!
Keplers laws of planetary motion!
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  1. Planets move in ellipses of semi-major axis a with the sun at a focus. An ellipse has eccentricity e, where ea is the distance from the center to a focus. perihelion - Rp = a (1– e ) closest point in sun-planet orbit aphelion - Ra = a (1+ e ) farthest point in sun-planet orbit

Kepler’s laws of planetary motion

  1. Planetary orbits sweep out equal areas in equal times. This law reflects the fact that gravity is a central force. Since gravity acts along the radial direction connecting two bodies, it produces no torque on either. For a planet of mass m , the angular momentum of the orbit is conserved and determines the rate of area A swept out by its orbit
  2. The square of the orbital period is proportional to the cube of the semi-major axis (and inversely to the Sun’s mass M ) € dA dt = L 2 m T 2 = 4 π 2 GM a 3 Java applet: http://www.walter-fendt.de/ph11e/keplerlaw2.htm

Consider an asteroid of mass m in (an arbitrary) orbit around a much larger planet of mass M. The mechanical energy of the two- body system is a conserved quantity that determines the nature of the orbit. Different families of orbits result from different signs of E mec

E

mec

= K + U =

1 2

mv

2

− G

Mm

r

family E mec eccentricity e orbit bound < 0 < 1 (0) ellipse (circle) just unbound = 0 = 1 parabola really unbound > 0 > 1 hyperbola

mechanical energy and orbit families

If two bodies of masses m and M are in a gravitationally bound orbit, the mechanical energy determines the size of the orbit , defined as the semi-major axis a , of the two-body system while the angular momentum L determines the shape of the orbit, defined by the eccentricity e

GMm

2 a

E

mec

GMm

2 a

E

mec

L

2

= GMm

2

a (1– e

2

For a set of bodies in circular orbits around a large mass M , the square of the orbital speed decreases inversely with distance r

v

2

= GM / r

Bound (negative energy) orbits

http://cfa-www.harvard.edu/~bmcleod/castle.html Images of Lensing removed