Astrodynamics 101 - DerAstrodynamics.com
Astrodynamics 101 - DerAstrodynamics.com
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.