Path: SpacecraftEstimation/DemoFuns
% Telescope model for satelite tracking.
This function does not account for field-of-view so it produces
measurements even when the spacecrat is behind the planet.
--------------------------------------------------------------------------
Form:
d = TelescopeUKF;
y = TelescopeUKF( x, d )
--------------------------------------------------------------------------
------
Inputs
------
x (3,1) State vector r
d (1,1) Data structure
.noise (2,1) Noise vector 1 sigma
.jD (1,1) Julian day number
.rGS (3,1) Ground station position vector
.eFToNEU (3,3) Transformation from EF to NEU
-------
Outputs
-------
y (6,1) [azimuth;elevation] in NEU frame
--------------------------------------------------------------------------
SC: Ephem/EOfE SC: Ephem/EarthRot SC: Ephem/GMSTime SC: Ephem/MSidDay SC: Ephem/NutDelta SC: Ephem/ObOfE Common: Time/DTSToDTA Common: Time/Date2JD Common: Time/JD2000 Common: Time/JD2T Common: Time/JDToMidnight Math: Linear/Unit Math: MathUtils/R2P5 Math: Trigonometry/CosD Math: Trigonometry/SinD
Back to the SpacecraftEstimation Module page