Roadmap¶
This page documents the current feature development roadmap for RAstro.
- Constants
- Mathematics
- Time
- Planetary Constants
- Earth Orientation Parameters
- Data Model Structure
- Fetching updated parameters
- Data retrieval
- Management / Versioning with packaging
- Customized of handling of out-of-range EOP requests
- Time Management (Epoch)
- Epoch Class
- Initialization
- String
- Caldate
- MJD
- GPS Elapsed Seconds
- GPS Week / Seconds
- Fundamental Operations
- Initialization
- Epoch Range Iterator
- Epoch Class
- Reference Frames
- Precession/Nutation Model
- Earth Rotation Model
- Polar Motion
- Orbits
- Orbital Period
- Mean Motion
- Periapsis/Apoapsis Velocity
- Perigee/Apogee Velocity
- Periapsis/Apoapsis Distance
- Anomaly True <-> Eccentric
- Anomaly Eccentric <-> Mean
- Anomaly True <-> Mean
- Sun-synchronous Inclination
- Osculating <-> Mean Transformation
- Transformations
- State ECI <-> ECEF (IAU 2010)
- Rotation ECI <-> ECEF (IAU 2010)
- State OSC <-> CART
- State OSC <-> ECEF
- Coordinate Transform
- Cart <-> Geocentric
- Cart <-> Geodetic
- Geocentric <-> Topocentric (ENU)
- Geocentric <-> Topocentric (SEZ)
- Geodetic <-> Topocentric (ENU)
- Geodetic <-> Topocentric (SEZ)
- ENU <-> AzEl
- SEZ <-> AzEl
- Relative Transformations
- ECI <-> RTN
- RTN <-> ROE
- ECI <-> ROE
- TLE
- TLE Object
- SGP4 Propagation
- Force Modeling
- Gravity
- Point Gravity
- Spherical Harmonic
- Third-Body Gravity
- SRP
- Direct Sun
- Earth Albedo
- Eclipse
- Drag Model
- Harris Priester
- NRLMSISE00
- Relativistic Corrections
- Tides
- Solid Earth
- Ocean
- Gravity
- Numerical Integrators
- Arbitrary RK integrator
- RK4
- RK8
- Variable Step
- Arbitrary RK integrator
- Orbit Propagators
- Keplerian
- Full Force
- Event Detection
- State propagation (multithreaded Jacobian evaluation)
- Arbitrary Python Force/Function Inclusion
- Arbitrary State Inclusion / Addition
- Access
- Location Data Model
- Access Computation - Constraint Definition
- Tessellation (Area Access)
- Estimation
- EKF
- UKF