Man pages for asteRisk
Computation of Satellite Position
| calculateRazel | Calculates azimuth, elevation and range of a given object |
| dateTimeToMJD | Calculate Modified Julian Date for a given date and time |
| deg2rad | Converts an angle in degrees to radians |
| ECItoKOE | Calculate ECI coordinates from Keplerian orbital elements |
| GCRFtoITRF | Convert coordinates from GCRF to ITRF |
| GCRFtoLATLON | Convert coordinates from GCRF to geodetic latitude, longitude... |
| getLatestSpaceData | Retrieves the latest space data |
| hpop | High-precision numerical orbital propagator |
| ITRFtoGCRF | Convert coordinates from ITRF to GCRF |
| ITRFtoLATLON | Convert coordinates from ITRF to geodetic latitude, longitude... |
| JPLephemerides | Calculate JPL main celestial objects ephemerides for a given... |
| KOEtoECI | Calculate ECI coordinates from Keplerian orbital elements |
| LATLONtoGCRF | Convert coordinates from geodetic latitude, longitude and... |
| LATLONtoITRF | Convert coordinates from geodetic latitude, longitude and... |
| parseTLElines | Parse the lines of a TLE |
| rad2deg | Converts an angle in radians to degrees |
| readGLONASSNavigationRINEX | Read a RINEX navigation file for GLONASS satellites |
| readGPSNavigationRINEX | Read a RINEX navigation file for GPS satellites |
| readOEM | Read an Orbital Ephemeris Message file |
| readTLE | Read a TLE file |
| revDay2radMin | Converts revolutions per day to radians per minute |
| sdp4 | Propagate an orbital state vector with the SDP4 model |
| sgdp4 | Propagate an orbital state vector with the SGP4/SDP4 model |
| sgp4 | Propagate an orbital state vector with the SGP4 model |
| TEMEtoGCRF | Convert coordinates from TEME to GCRF |
| TEMEtoITRF | Convert coordinates from TEME to ITRF |
| TEMEtoLATLON | Convert coordinates from TEME to geodetic latitude, longitude... |
