Path: SC/MannedVehicle
% Computes the coordinates in the ISS frame
The ISS frame is defined as:
+X Along the velocity vector (Forward)
-X Opposite the velocity vector (Aft)
+Y -Orbit Normal (Starboard)
-Y +Orbit Normal (Port)
+Z Zenith (Deck)
-Z Nadir (Overhead)
This is the same as LVLH. Julian date propagates the initial ISS coordinate
set. If there are no outputs the function draws a 3D view of the scene using
the CAD model in ISS.mat.
Type ISSCoord for a demo for a position offset from the ISS by a few tens of
meters.
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Form:
rISS = ISSCoord(r,jD)
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Inputs
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r (3,:) ECI coordinates
jD (1,1) Julian date
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Outputs
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rL (3,:) Position in ISS Coordinates
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References: https://www.nasa.gov/mission_pages/station/multimedia/
iss_labs_guide.html
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AerospaceUtils: Coord/QLVLH SC: BasicOrbit/El2RV SC: Ephem/ISSOrbit SC: SCModels/ISS Common: ComponentModels/AggregateComponents Common: Graphics/Arrow3D Common: Graphics/DrawVertices Common: Quaternion/QForm
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