Space Mission Design allows one to perform an initial space mission design, around a given celestial body or between celestial bodies.
This package was written to support my thesis and my astrodynamics courses (ASEN 6008 Space Mission Design / Interplanetary Mission Design) at the University of Colorado Boulder.
Note: this list may not be up to date with the latest developments.
- Propagation of an orbit around a celestial body
- Direct closed-loop optimization of continuous thrust via Naasz and Ruggiero control laws.
- VSOP87 support via the amazing https://github.com/soniakeys/meeus
- Patched conics for interplanetary missions
- Stream orbital elements as CSV for live visualization of how they change
- Export as a set of NASA Cosmographia files (cf. http://cosmoguide.org/) for really cool visualization of the overall mission
- Export mission state as CSV (cf. the
examples/statOD/main.go)
If running smd and planning on changing reference frames (e.g. when doing patched conics) to attempting to include third body dynamics, you will need to define the SMD_CONFIG environment variable. This must define whether using VSOP87 or SPICE for frame transformations. An example of such a file is found in conf.toml.
Important: this configuration file must be called conf.toml (but it can be placed in any directory).
Note: the availability of this file will only occur in the function which gets the heliocentric orbit of a given planet. So definitely make sure this is configured before running a long simulation or it will crash when you're looking away.