Earth-Moon-Spacecraft 3-Body Orbital Motion in Cislunar Space

Earth-Moon-Spacecraft 3-Body Orbital Motion in Cislunar Space

Ross Dynamics Lab via YouTube Direct link

Stability of halo orbit

19 of 28

19 of 28

Stability of halo orbit

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Classroom Contents

Earth-Moon-Spacecraft 3-Body Orbital Motion in Cislunar Space

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  1. 1 Cislunar Space Introduction
  2. 2 Example low-energy Cislunar spacecraft trajectories
  3. 3 Table of contents
  4. 4 Circular restricted three-body problem
  5. 5 Lunar rotating frame
  6. 6 Equations of motion
  7. 7 Tisserand relation, Jacobi constant
  8. 8 Dynamics along Tisserand curves
  9. 9 Realms of energetically possible motion
  10. 10 Five energy cases and zero velocity surfaces
  11. 11 Necks at Lagrange points L1, L2, and L3
  12. 12 Motion near the stable Lagrange points L4 and L5
  13. 13 Tadpole and horseshoe orbits
  14. 14 Oterma comet goes between interior, secondary and exterior realms
  15. 15 Motion near lunar L1 and L2
  16. 16 Periodic and quasiperiodic orbits about L1 or L2
  17. 17 Periodic orbit family metro map
  18. 18 Stability of trajectories, especially periodic orbits
  19. 19 Stability of halo orbit
  20. 20 Quasi-halo orbits around a halo orbit
  21. 21 MATLAB code description
  22. 22 MATLAB Demonstration, compute a halo orbit and manifolds
  23. 23 Connections between cislunar and heliocentric space
  24. 24 Mean motion resonances, Lunar gravity assists
  25. 25 Effect of distant lunar flybys, analytical model
  26. 26 Global phase space dynamics, chaotic sea, stable sea shores, stable resonant islands
  27. 27 Resonance zone within the chaotic sea
  28. 28 More realistic models

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