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on
1
Introductory comments
2
Outline
3
Equations of motion
4
3-body energy - constant of motion
5
Tisserand relation, Tisserand curve meaning
6
Realms of possible motion
7
Zero velocity curves
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Zero velocity surfaces
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Lagrange points
10
L4, L5 - triangular points
11
L4, L5 - tadpole and horseshoe orbits
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L1, L2 - collinear points
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L1, L2 - 4 types of trajectories
14
Lissajous orbits
15
Halo orbits 3D
16
Lyapunov orbits planar
17
Stability of periodic orbits
18
Stability of halo orbits
19
Approaching and departing directions
20
Quasi-halo orbits
21
Stable and unstable manifolds
22
Transition tubes
23
MATLAB exercise intro
24
Differential correction
25
MATLAB demo
26
Cislunar-heliocentric space connection
27
Lunar L1 to Sun-Earth L2
28
Apollo 12 upper stage
29
Orbital resonance
30
Resonances with moon
31
Poincare section
32
Mixed phase space, chaotic and resonance regions
33
Semi-analytical model of multiple lunar flybys
34
Connection with ballistic capture
35
Persistence in realistic models
36
References
Description:
Explore the complexities of orbital dynamics in cislunar space through this comprehensive lecture on the restricted 3-body model. Delve into the fundamentals of astrodynamics beyond the geosynchronous belt, covering topics such as lunar mean motion resonances, libration-point orbits, and invariant manifolds. Learn about the Lagrange points, various types of orbits including Lissajous and halo orbits, and the stability of periodic orbits. Gain insights into the application of MATLAB for differential correction and modeling. Discover the connections between cislunar and heliocentric space, orbital resonances, and the implications for space mission design. Enhance your understanding of advanced concepts in celestial mechanics and their practical applications in space exploration.

Cislunar Space - 3-Body Model of Orbital Dynamics Beyond the Geosynchronous Belt

Ross Dynamics Lab
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