Expand description
Numerical astrodynamics engine for orbit propagation, force models, and future flight-dynamics primitives.
Current scope:
- inertial Cartesian state representation
- two-body gravity and J2 perturbation
- fixed-step RK4
- adaptive Dormand-Prince 5(4) (
DP54) - propagation results with step statistics
Planned future work includes dense output, event handling, richer propagation contexts, additional force models, covariance propagation, estimation, and maneuver support.
Re-exports§
pub use error::PropagationError;pub use state::CartesianState;pub use time::Time;
Modules§
- constants
- error
- events
- forces
- integrators
- math
- propagator
- sgp4
- SGP4 satellite propagation with 0 ULP parity to the Vallado C++ reference implementation (v2020-07-13).
- state
- time