Path: SCPro/ProSensors
% Computes optical navigation observables.
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Form:
NavObservables;
[c, a, f, m] = NavObservables( r, rP, radiusP, jD, nameP, nameM, alb )
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Inputs
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r (3,:) Trajectory (au)
rP (3,:,m) Planet trajectories (au)
radiusP (1,m) Radius of the planets
jD (1,:) Julian dates of trajectory points
nameP {1,m} Planet names
nameM (1,:) Mission name for plot titles
alb (1,m) Albedo fractions for planets
albF (1,m) Albedo fraction
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Outputs
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c (m,:) Chordwidths of planets and sun (rad)
a (1,:) Minimum planet angular separation (rad)
f (m,:) Power flux (W/m^2)
m (1,:) Range to nearest target (au)
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AC: ACData/ACTConstants Orbit: OrbitData/Messenger Orbit: OrbitData/ReadHorizons SC: BasicOrbit/E2Nu SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy SC: BasicOrbit/M2Nu SC: BasicOrbit/M2NuPb SC: BasicOrbit/RVFromKepler SC: Ephem/Planets SC: Ephem/SolarSys SC: SCData/sCTConstants 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/Plot3D Common: Graphics/PltStyle Common: Graphics/TextS Common: Graphics/TimeLabl Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Common: Time/DTSToDTA Common: Time/Date2JD Common: Time/JD2T Math: Linear/DupVect Math: Linear/Mag Math: Linear/Unit
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