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SUPPORT SITE |
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SUPPORT SITE |
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Path: SpacecraftEstimation/OpticalNavigation
% Computes the noise matrix for navigation with stars and planets.
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Form:
OpticalNavPlanetStarNoiseMatrix
[dY, rM] = OpticalNavPlanetStarNoiseMatrix( g, r, noise )
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Inputs
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g
.uS (3,:) Star vectors
.kP (1,1) Planet id
.rP (3,1) Two planets
.mode (1,:) 'polar star' or 'two planet'
r (3,1) Position vector
noise (1,1) Noise data structure
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Outputs
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dY (1,1) Number of measurements
rM (n,n) Measurement noise matrix
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Common: Database/Constant Common: Time/Date2JD Common: Time/JD2T Common: Transform/RaDec2U Math: Linear/Mag Math: Linear/Unit SC: Ephem/Planets SC: Ephem/SolarSys SpacecraftEstimation: OpticalNavigation/NavTargetTrackingPlanetary SpacecraftEstimation: StellarCatalog/LoadCatalog
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