What is the equation/algorithm for transforming Earth-Centered Inertial (ECI) frame to Topocentric-Horizon system (SEZ) in c#? Can anyone help me?
X=4, Y=6, Z=10, phi=40, theta= 49
What is the equation/algorithm for transforming Earth-Centered Inertial (ECI) frame to Topocentric-Horizon system (SEZ) in c#? Can anyone help me?
X=4, Y=6, Z=10, phi=40, theta= 49