Space Systems Dynamics

Orbital and attitude dynamics and control

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This zip file contains the coefficients of the Lindstedt-Poincaré series expansion up to the 9th order for L1/L2 halo orbits in the Earth-Moon,
Sun-Earth, and Sun-Venus three-body systems. See README inside the archive for more details.

This zip file contains the coefficients of the Lindstedt-Poincaré series expansion up to the 15th order for L1/L2 Lissajous orbits in the Earth-Moon, Sun-Earth, and Sun-Venus three-body systems. See README inside the archive for more details.

The zip file contains the phase state vectors for L1/L2 lunar halo orbits. They can be used to obtain any intermediate lunar halo orbit by means of interpolation and differential correction. See the README file inside the archive for more details.

This zip file contains the coefficients of the formal Fourier-like series to accurately approximate a vast range of planar distant retrograde orbits in the Earth-Moon and Sun-Earth three-body systems. The details are given in the README file inside the archive.

This zip file contains the phase state vectors for a set of planar distant retrograde orbits (DROs) in the Earth-Moon and Sun-Earth three-body
systems. They can be used to obtain any intermediate DRO by means of interpolation and differential correction. 
See the README file inside the archive for more details.