Path: Link/Coverage
% Determine ground station visibility for spacecraft position(s). Has a built-in demo. -------------------------------------------------------------------------- Form: visible = GroundStationVisibility( rGroundStation, jD, rSC, horizonAngle ) -------------------------------------------------------------------------- ------ Inputs ------ rGroundStation (3,m) Earth fixed location of station(s) jD (1,n) Julian date rSC (3,n) Position(s) of spacecraft, ECI frame horizonAngle (1,1) Minimum elevation to ground station (rad) ------- Outputs ------- visible (n,m) Matrix of visible flags -------------------------------------------------------------------------- See also SatelliteVisibility, ECIToEF, LatLonAltToEF --------------------------------------------------------------------------