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General Motion. Rest: Quasars Linear: Stars Keplerian: Binary Perturbed Keplerian: Asteroids, Satellites Complex: Planets, Space Vehicles Rotational: Earth, Moon, Satellites, …. Linear Motion. Radial Motion Proper Motion = Angular Motion. Quasar/Star Catalog. Epoch
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General Motion • Rest: Quasars • Linear: Stars • Keplerian: Binary • Perturbed Keplerian:Asteroids, Satellites • Complex: Planets, Space Vehicles • Rotational: Earth, Moon, Satellites, …
Linear Motion • Radial Motion • Proper Motion = Angular Motion
Quasar/Star Catalog • Epoch • Mean Place (at Epoch) • Parallax (at Epoch) • Proper Motion • Radial Velocity • Astrophys. Quantities:Magnitude, Color, … • ICRFnn, HIPPARCOS, FKn, PPM, AGKn
Keplerian • Two Body Motion under Newtonian Mech. • Gravitational Constant • Elements = 6 Constants of Motion • Shape • Orientation • Timing
Units of Mass • SI: kilogram kg • Astronomical: Solar Mass • Newtonian Gravitational Constant • Measurable Quantity = GM = Body-centric Gravitational Constant • Heliocentric Geocentric
Keplerian Elements • Semi-Major Axis: a • Eccentricity: e • Longitude of Ascending Node: W • Inclination: I • Argument of Pericenter: w • Epoch of Pericenter Passage: T
Ellipse • Semi-major axis: a • Semi-minor axis: b
Eccentricity • Eccentricity: e, Co-Eccentricity: e’ F ae
Orbital Orientation • Euler (3-1-3) Angles of Orbital Plane RF • 3 Important Directions • Departure Point: X-axis • Ascending Node: N • Pericenter: P
Orbital Plane Z w P I g W N
Keplerian Orbits • Elliptic: e < 1 • Planets, Satellites, Binary • Parabolic: e = 1 • Good Approximation for Comets • Nearly Parabolic: e ~ 1 • Comets, some peculiar Asteroids • Hyperbolic: e > 1 • Space Vehicles, Virtual (Change of Origin)
Elements to Position, Velocity • Solve Kepler’s Equation • Time Derivative of E • PV in Orbital RF
Elements to PV (contd.) • Backward Euler Rotation
Kepler’s Equation • First Nonlinear Equation in History • Elliptic • Parabolic • Hyperbolic
Elliptic Kepler’s Equation • Eccentric Anomaly: E • Mean Anomaly: M = n ( t – T ) • Kepler’s 3rd Law • True Anomaly: f
Solution of Kepler’s Equation • Reduction of Variable Domain • Newton Method
Initial Guess for Newton Method • Stability Theory • Initial Guess = Upper Bound • Efficient Choice
Perturbed Keplerian Orbits • Elements as Functions of Time • Perturbation Theory • Polynomial + Fourier Series
Complex Motion • Equation of Motion • Numerical/Analytical Solution • Parameter Fitting to Observational Data • Results = Ephemeris
Planetary/Lunar Ephemerides • Numerical: DE series (NASA/JPL), DE405 • Analytical: VSOP/ELP (BdL) • DE: available at NAO/CC • Fortran/C callable routines + Binary file(s) • DE405: 1600-2200, UNIX/Win/Mac • P/V of Sun+Moon+9planets • Base: PN Eq.Motion + Precision Data + Least Square Fitting (Mass, Init. Cond., etc.) • Other Solar System Bodies: HORIZONS • Details: http://ssd.jpl.nasa.gov/