Astrodynamics 102 - DerAstrodynamics.com

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Space Debris and Satellite Growth 2007 2009, . . , 2013
1. What, Why, How What? Satellite rendezvous and docking, weather forecast, tracking of satellites, missiles and debris, mission planning, . . . . . , SSA are many challenging problems Why? Need accurate, fast and robust utility algorithms for multiple applications How? Understand the Physics and Mathematics of <strong>Astrodynamics</strong> for analytic orbit determination using radar and laser data Solving These Challenging Problems Requires Analytic Lambert+ Algorithm
Page 1 and 2: Launch / Impact Point Prediction S
Page 3 and 4: Astrodynamics 102: Lambert+ Algorit
Page 5 and 6: Radar/Laser Weather/Satellite Track
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Page 11 and 12: Physics and Mathematics 2. Physics
Page 13 and 14: direct transfer orbit o (inclinatio
Page 15 and 16: Choice of bounded x, gives a “ver
Page 17 and 18: Classical Kepler (2-Body) Perturbat
Page 19 and 20: Equations of Motion (2-Body) d2 r =
Page 21 and 22: v 2 vv2 vt2 v 2 Initial Step 1 B Ke
Page 23 and 24: Transfer orbit 1: inc_to = 1, i < 9
Page 25 and 26: Lambert Problem Given: r (t ) , r (
Page 27 and 28: Osculating Orbital Elements at t o
Page 29 and 30: Applications of Analytic Algorithms
Page 31 and 32: UNCLASSIFIED Applications of Analyt
Page 33 and 34: Astrodynamics 102 Part 2: Verificat
Page 35 and 36: ICBM transfer orbit , Single revolu
Page 37 and 38: Numerical Example 4 High Earth Orbi
Page 39 and 40: Numerical Example 6 ICBM transfer o
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Astrodynamics 102 - DerAstrodynamics.com

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