Path: SpacecraftEstimation/OpticalNavigation
% Computes the noise matrix for navigation with stars and planets.
--------------------------------------------------------------------------
Form:
OpticalNavPlanetStarNoiseMatrix
[dY, rM] = OpticalNavPlanetStarNoiseMatrix( g, r, noise )
--------------------------------------------------------------------------
------
Inputs
------
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
-------
Outputs
-------
dY (1,1) Number of measurements
rM (n,n) Measurement noise matrix
--------------------------------------------------------------------------
AC: ACData/ACTConstants SC: BasicOrbit/E2Nu SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy SC: BasicOrbit/M2Nu SC: BasicOrbit/M2NuPb SC: Ephem/LoadFK5 SC: Ephem/Planets SC: Ephem/SolarSys SC: SCData/sCTConstants SpacecraftEstimation: OpticalNavigation/NavTargetTrackingPlanetary SpacecraftEstimation: StellarCatalog/LoadCatalog SpacecraftEstimation: StellarData/FK5Polar SpacecraftEstimation: StellarData/Hipparcos Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Database/Constant Common: General/CellToMat Common: General/DeBlankLT Common: General/DeleteCell Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/TextS Common: Graphics/TitleS Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Time/DTSToDTA Common: Time/Date2JD Common: Time/JD2T Common: Transform/RaDec2U Math: Linear/Dot Math: Linear/DupVect Math: Linear/Mag Math: Linear/Unit
Back to the SpacecraftEstimation Module page