Download PPT - LSU Physics & Astronomy

Survey
yes no Was this document useful for you?
   Thank you for your participation!

* Your assessment is very important for improving the workof artificial intelligence, which forms the content of this project

Document related concepts

Classical central-force problem wikipedia , lookup

Newton's theorem of revolving orbits wikipedia , lookup

Newton's laws of motion wikipedia , lookup

Transcript
Physics 2113
Jonathan Dowling
Isaac Newton
(1642–1727)
Physics 2113
Lecture 03: FRI 29 AUG
CH13: Gravitation III
Version: 5/24/2017
Michael Faraday
(1791–1867)
13.7: Planets and Satellites: Kepler’s 1st Law
1. THE LAW OF ORBITS: All planets move in elliptical
orbits, with the Sun at one focus.
Laws were
based on
data fits!
Tycho Brahe
1546–1601
Johannes Kepler
1571–1630
13.7: Planets and Satellites: Kepler’s 2nd Law
2. THE LAW OF AREAS:
A line that connects a planet to
the Sun sweeps out equal areas
in the plane of the planet’s
orbit in equal time intervals;
that is, the rate dA/dt at which it
sweeps out area A is constant.
Angular momentum, L:
Þ A µt
13.7: Planets and Satellites: Kepler’s 3rd Law
3. THE LAW OF PERIODS: The square of the period of any planet is
proportional to the cube of the semi-major axis of its orbit.
Consider a circular orbit with radius r
(the radius of a circle is equivalent to
the semimajor axis of an ellipse).
Applying Newton’s second law to the
orbiting planet yields
T=
Using the relation of the angular
velocity, ω, and the period, T, one
gets:
2p
w
13.7: Planets and Satellites: Kepler’s 3rd Law
1
ICPP:
(a) The larger the orbit the
longer the period: SAT-2.
T=
(b) The smaller the orbit the
greater the speed: SAT-1.
v = w r = 2Tp =
rLEO = REarth + aLEO = 10 7 m
TLEO =
vLEO =
µr
3/2
GM
r
µ
1
r
rGEO = REarth + aGEO = 4.22 ´ 10 7 m
kg×s2
(10 7 m)3
4π 2
1
-11
3
24
1 6.67´10 m 5.97´10 kg
1
24
6.67´10 -11 m 3 5.97´10 kg 1
1
kg×s 2
10 7 m
4 p 2r 3
GM
2
= 6307s TGEO =
= 7.4km/s
vGEO =
kg×s2
(4.22´10 7 m)3
4π 2
1
-11
3
24
1 6.67´10 m 5.97´10 kg
1
24
6.67´10 -11 m 3 5.97´10 kg
1
2
1
kg×s
4.22´10 7 m
= 8.62 ´ 10 4 s = 24hrs
= 3km/s
13.7: Newton Derived Kepler’s Laws from Inverse Square Law!
http://galileo.phys.virginia.edu/classes/152.mf1i.spring02/KeplersLaws.htm
Kepler’s Second Law First:
Equal Areas Proportional to Equal
Time!
Angular Momentum
Rate of sweeping out of area,
dA / dt = c
is proportional to the angular momentum L, and
equal to L/2m = Constant = C.
Þ A µt
13.7: Newton Derived Kepler’s Laws from Inverse Square Law!
http://galileo.phys.virginia.edu/classes/152.mf1i.spring02/KeplersLaws.htm
Kepler’s First Law:
Ellipse with Sun at Focus
This is equivalent to the
standard (r, q ) equation of an
ellipse of semi-major axis a and
eccentricity e, with the origin —
the Sun — at one focus. Note
1/L2 is from inverse
Square Law.
13.7: Newton Derived Kepler’s Laws from Inverse Square Law!
http://galileo.phys.virginia.edu/classes/152.mf1i.spring02/KeplersLaws.htm
Kepler’s 3rd Law:
For Ellipse
T µa
2
3
Example, Halley’s Comet
ICPP: Estimate comet’s speed at farthest distance?
v = v^ = w r
w = 2p / T
2p r
6 ´ 9 ´ 1010 m
1012 m
v=
@
@
@ 1,000m/s
7
9
T
76y ´ 3 ´ 10 s/y 10 s
13.8: Satellites: Orbits and Energy
As a satellite orbits Earth in an elliptical
path, the mechanical energy E of the
satellite remains constant. Assume that the
satellite’s mass is so much smaller than
Earth’s mass.
The potential energy of the system is given
by
For a satellite in a circular orbit,
Thus, one gets:
For an elliptical orbit (semimajor axis a),
ICPP
GMm
1
E=µ2r
r
1
dE µ + 2 dr
r
T=
4p 2
GM
r µ +r
3
dT µ +r dr
(a) path 1: As E decreases (dE < 0); r decreases (dr < 0)
(b) Less: As r decreases (dr < 0); T decreases (dT < 0)
2
3
NASA Gravity Recovery and Climate Experiment
What Do the Two Satellites Measure? Changing g field!
http://www.jpl.nasa.gov/missions/gravity-recovery-and-climate-experiment-grace/
Earth is NOT a Uniform Sphere —> Gravitational Field Changes in Orbit.
Rocky Mtn. High
ΔM
mid-Atl. Low
GM
1
1
GM
µ
+
v=
µ +r 2
r2
r2
r
1
3
dg µ - 3 dr
2
dv µ -r dr
r
As g increases (dg > 0); r decreases (dr < 0). As r decreases (dr < 0); v increases (dv > 0).
g=
•
•
•
•
Changing field Δg give rise to changing velocity Δv.
Changing Δv gives changing satellite-to-sattellite distance.
Microwave link measures changing distance between satellites.
Measuring Δg allows computation of ΔM — Earth’s Mass Distribution.
Example, Mechanical Energy of a Bowling Ball
13.9: Einstein and Gravitation: Curvature of Space
13.9: Einstein and Gravitation: Gravity Waves
LIVINGSTON LASER INTERFEROMETER GRAVITATIONAL-WAVE OBSERVATORY
Disturbances in the Gravitational Field Move Outward As Waves
Two Orbiting Black Holes
HW01 DUE TONIGHT: 11:59PM FRI 29 AUG!
WEB ASSIGN CLASS KEY FOR SECTION 2: lsu 8181 3713
Tutoring in Middleton & Nicholson (Starts NEXT Week): http://cas.lsu.edu/tutorial-centers
Free online tutoring available NOW: http://cas.lsu.edu/line-tutoring
Minority Student Tutoring via LAMP Program! Apply here: http://www.lsu.edu/lamp/index.html
Student Athlete Tutoring: http://www.acsa.lsu.edu/sports/2013/11/7/tutorialcenter.aspx
Private Tutors: http://cas.lsu.edu/private-tutors