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SUPPORT SITE |
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SUPPORT SITE |
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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.
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Form:
d = TelescopeUKF;
y = TelescopeUKF( x, d )
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Inputs
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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
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Outputs
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y (6,1) [azimuth;elevation] in NEU frame
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Common: Time/JD2000 Common: Time/JD2T Math: Linear/Unit OrbitMiniToolbox: Support/EarthRot
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