Module nyx_space::celestia [−][src]
Expand description
Provides the solar system planets, and state and (later) ephemeride management.
Modules
| eclipse | The eclipse module allows finding eclipses and (conversely) visibility between a state and another one (e.g. a planet or the Sun). |
| orientations | Known orientation IDs defined for ease of access. All Cosm objects may be accessed via Cosm directly. |
Structs
| BPlane | Stores a B-Plane |
| BPlaneTarget | |
| Cosm | |
| Euler3Axis | A fixed three-axis Euler rotation |
| Euler3AxisDt | A time varying three-axis Euler rotation |
| FrameTree | |
| IoError | The error type for I/O operations of the |
| NoRotation | |
| Orbit | Orbit defines an orbital state |
| OrbitDual | Orbit defines an orbital state |
| OrbitPartial | A type which stores the partial of an element |
| Spacecraft | A spacecraft state |
| Xb |
Enums
| AngleUnit | |
| Bodies | Defines the default celestial bodies in the provided de438 XB. |
| EulerRotation | Defines an Euler rotation, angle must be in radians |
| Frame | |
| GuidanceMode | |
| IoErrorKind | A list specifying general categories of I/O error. |
| LTCorr | Enable or not light time correction for the computation of the celestial states |
| NyxError | |
| StmKind | Defines the kind of state transition matrix stored in the orbit. |
Constants
| AU | Astronomical unit, in kilometers, according to the IAU. |
| SPEED_OF_LIGHT | Speed of light in meters per second |
| SPEED_OF_LIGHT_KMS | Speed of light in kilometers per second |
| SS_MASS | Mass of the solar system from https://en.wikipedia.org/w/index.php?title=Special:CiteThisPage&page=Solar_System&id=905437334 |
| SUN_GM | GM of the Sun in km^3/s^2 |
Traits
| ParentRotation |
Functions
| assert_orbit_eq_or_abs | |
| assert_orbit_eq_or_rel | |
| try_achieve_b_plane | Returns the Delta V (in km/s) needed to achieve the B Plane specified by B dot R and B dot T. If no LTOF target is set, this method will fix VX, VY and VZ successively and use the minimum of those as a seed for the LTOF variation finding. If the 3x3 search is worse than any of the 2x2s, then a 2x2 will be returned. This uses the hyperdual formulation of the Jacobian and will also vary the linearize time of flight (LTOF). |