Open-space-toolkit-astrodynamics

**feat:**
- [make the propagator maintain the frame and size of the input State](https://github.com/open-space-collective/open-space-toolkit-astrodynamics/commit/7c1420a156ec157d8a8a4a3d6d642acc6d4713e8)

**feat**
- add boost logging + logs for sequence and segments (and solutions) (251)
- add custom logging option for conditional solver (252)
- add metadata for segment and sequence solutions (250)

**fix**
- fix missing binding for Segment::Solution (253)

**refactor**
- rename files with ':' for windows compatibility (247)

**feat**
- Python class meta-programming for State construction (244)
- add Brouwer-Lyddane Mean Long and Mean Short elements (240)
- add State constructor with Array of Subsets (238)
- add StateBuilder (237)
- enrich StateBuilder capabilities (239)


**refactor**
- Use the built-in State method to extract coordinates (235)

**feat**
- add bindings for ConstantThrust static constructors (232)
- add functions to extract multiple subsets at once. (234)
- return conditional solution for segment and sequences (233)
- update State printing to support extended state (231)

- clean: move dynamics to root.
- build: update physics and deps for stack-trace fixes.

**feat**
- add static constructors for constant thrust