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• Homework 1 due Tuesday Jan 15 Celestial Mechanics Fun with Kepler and Newton •Elliptical Orbits •Newtonian Mechanics •Kepler’s Laws Derived •Virial Theorem Elliptical Orbits I Tyco Brahe’s (1546-1601) Observations • Uraniborg Observatory - Island of Hveen, King Frederick II of Denmark • Large Measuring Instruments (Quadrant) High Accuracy (better than 4’) • Demonstrated that comets farther than the moon • Supernova of 1572 Universe Changes • No clear evidence of the motion of Earth through heavens concluded that Copernican model was false Elliptical Orbits 2 Kepler’s (1571-1630) Analysis • Painstaking analysis of Brahe’s Data • Heliocentrist but still liked spheres/circles…until he could not get agreement with observations. Two points off by 8’ considered the possibility that orbits were elliptical in shape. • Minor mathematical but major philosophical change • Assuming elliptical orbits enabled Kepler to fit all of Tycho Brahe’s data Elliptical Orbits 3 Kepler’s Laws of Planetary Motion Kepler’s First Law: A planet orbits the Sun in an ellipse, with the Sun at one focus of the ellipse. Kepler’s Second Law: A line connecting a planet to the Sun sweeps out equal areas in equal time intervals Kepler’s Third Law: The Harmonic Law P2=a3 Where P is the orbital period of the planet measured in years, and a is the average distance of the planet from the Sun, in astronomical units (1AU = average distance from Earth to Sun) Kepler’s First Law Kepler’s First Law: A planet orbits the Sun in an ellipse, with the Sun at one focus of the ellipse. • a=semi-major axis • e=eccentricity • r+r’=2a - points on ellipse satisfy this relation between sum of distance from foci and semimajor axis Kepler’s Second Law Kepler’s Second Law: A line connecting a planet to the Sun sweeps out equal areas in equal time intervals Kepler’s Third Law Kepler’s Third Law: The Harmonic Law P2=a3 • Semimajor axis vs Orbital Period on a loglog plot shows harmonic law relationship The Geometry of Elliptical Motion Can determine distance from focal point to any point along elliptical path by using Pythagoras’s help…. b 2 = a 2 (1- e 2 ) r¢2 = r 2 sin 2 q + (2ae + r cos q ) 2 r¢2 = r 2 = 4ae(ae + r cos q ) r + r¢ = 2a a(1- e 2 ) r= 1+ ecosq Conic Sections • By passing a plane though a cone with different orientations one obtains the conic sections – – – – Circle (e=0.0) Ellipse (0<e<1.0) Parabola (e=1.0) Hyperbola (e>1.0) Galileo Galilei (1564-1642) • Experimental Physicist • Studied Motion of Objects – formulated concept of inertia – understood acceleration (realized that objects of different weights experienced same acceleration when falling toward earth) • Father of Modern Astronomy – – – – Resolved stars in Milky Way Moons of Jupiter Craters on Moon Sunspots • Censored/Arrested by Church…Apology 1992 Sir Isaac Newtonian (12/25/1642- 1727) • Significant Discoveries and theoretical advances in understanding – – – – motion Astronomy Optics Mathematics • …published in Principia and Optiks Newton’s Laws of Motion • Newton’s First Law: The Law of Inertia. An object at rest will remain at rest and an object in motion will remain in motion in a straight line at a constant speed unless acted upon by an external force. • Newton’s First Law: The net force (thesum of all forces) acting on an object is proportional to the object’s mass and its resultant acceleration. n Fnet = å Fi = ma i=1 • Newton’s Third Law: For every action there is an equal and opposite reaction Newton’s Law of Universal Gravitation • Using his three laws of motion along with Kepler’s third law, Newton obtained an expression describing the force that holds planets in their orbits… Mm F =G 2 r Gravitational Acceleration • Does the Moon’s acceleration due to the earth “match” the acceleration of objects such as apples? Work and Energy • • • • • • Energetics of systems Potential Energy Kinetic Energy K = 1 mv 2 2 Total Mechanical Energy Conservation of Energy Gravitational Potential Mm energy U = -G r • Escape velocity v esc = 2GM /r Derivations on pp37-39 Kepler’s Laws Derived Center of Mass Reference Frame and Total Orbital Angular Momentum • Displacement vector • Center of mass position • Reduced Mass • Total Orbital Angular Momentum • Definitions on pp 39-43. Derivation of Kepler’s First Law • Consider Effect of Gravitation on the Orbital Angular Momentum L = mr ´ v = r ´ p • Central Force Angular Momentum Conserved • Consideration of quantity a ´ L leads to equation of ellipse describing orbit!!! • Derivation on pp43-45 Derivation of Kepler’s Second Law • Consider area element swept out by line from principal focus to planet. • Express in terms of angular momentum dA 1 L = dt 2 m • Since Angular Momentum is conserved we obtain the second law • Derived on pp 45-48 Derivation of Kepler’s Third Law • Integration of the expression of the 2nd law over one full period dA 1 L = dt 2 m • • Results in A= 1L P 2m 2 4 p P2 = a3 G(m1 + m2 ) • Derived on pp 48-49 Virial Theorem • Virial Theorem: For gravitationally bound systems in equilibrium the Total energy is always one half the time averaged potential energy U E= 2 • The Virial Theorem can be proven by considering the quantity Q º å pi · ri and its time derivative along with Newton’s laws i and vector identities • Many applications in Astrophysics…stellar equilibrium, galaxy clusters,…. • Derivation on pp 50-53