This Xcos block calculates access between ground station and satellite.
This Xcos block calculates access between ground station and satellite. It has two inputs. First should provide information about the ground station in a 4x1 column vector containing:
Second input is a 3x1 vector defining satellite position in meters in terrestial reference frame. Outputis a 1x1 real number equal to 1 if access is possible and 0 if it is not.
Input 1: 4x1 double (ground station parameters [latitude; longitude; altitude; mask])
Input 2: 3x1 double (satellite position in terrestial reference frame [x;y;z])
Output: 1x1 double (1/0 access information)
This block has no dialog box.
This block has no cofigurable properties.
macros/STATION_VISIBILITY.sci
macros/AB_station_visibility.sci
CelestLab - CelestLab aerospace library
CL_gm_stationPointing - CelestLab function used to calculate satellite eleveation above the ground station local horizon.
KEP_TO_CAR - Aerospace Blockset block allowing for conversion from classical keplerian orbital elements to position and velocity for an elliptic, hyperbolic or parabolic orbit
GROUND_STATION - Aerospace Blockset block allowing for easy input of ground station name, location and visibility mask.