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Astrodynamics 101 - DerAstrodynamics.com

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Newton / Classical Formulation<br />

Equations of motion<br />

2<br />

d r <br />

= r a<br />

2 3 d t r<br />

Given : r(t 0), v(t<br />

0), t 0 , t<br />

Find : r(t ) , v(t<br />

)<br />

Kepler method:<br />

Assume zero perturbation:<br />

,<br />

a 0<br />

d =<br />

resulting in spherical<br />

gravity effect.<br />

Kepler analytic solution:<br />

r fI =<br />

v <br />

fI gI<br />

gI<br />

<br />

<br />

r0<br />

v<br />

where f , g, f , and g are<br />

analytic and functions of<br />

r r(t ) and v v(t<br />

)<br />

<br />

<br />

<br />

d<br />

0 <br />

0 0 0 0<br />

UNCLASSIFIED<br />

Comparison of Analytic Solutions<br />

Vinti / Hamilton-Jacobi Formulation<br />

Equations of motion<br />

dpk H(q, p, t ) dqk<br />

H(q,<br />

p, t )<br />

, <br />

d t qk d t pk<br />

where q's and p's are respectively<br />

coordinates and momenta, and k 1,<br />

2, 3<br />

Given : r(t 0), v(t<br />

0), t 0 , t<br />

Find : r(t ) , v(t<br />

)<br />

Vinti method:<br />

Assume non-zero perturbation:<br />

,<br />

a 0<br />

d <br />

resulting in spheroidal gravity effect so that<br />

zonal geopotentials J , J , J are included.<br />

2 3 4<br />

Vinti analytic solution:<br />

See Vinti AIAA book, V177, 1998,<br />

"Orbital and Celestial Mechanics",<br />

Chapter 8.<br />

Also see GTDS, Chapter 5.12 on<br />

attributes of "Vinti Theory", singularity free<br />

and applicability to satellites and missiles.

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