Path: Orbit/OrbitMechanics
% Compute ground coverage for an orbit.
--------------------------------------------------------------------------
Form:
[lat, lon] = GroundCoverage( xECI, jD, d )
--------------------------------------------------------------------------
------
Inputs
------
xECI (6,1) [r;v]
jD (1,1) Julian sdate
d (:)
.m (3,3) Transformation from LVLH to Sensor
.fOV .x (1,1) angle along x
.y (1,1) angle along y
.e (3,1) [a;b;c] Dimensions of planet
-------
Outputs
-------
lat (1,4) Latitude of the coverage points
lon (1,4) Longitude of the coverage points
--------------------------------------------------------------------------
AerospaceUtils: Coord/Gc2GdLat AerospaceUtils: Coord/QLVLH AerospaceUtils: Coord/R2LatLon SC: Ephem/EOfE SC: Ephem/EarthNut SC: Ephem/EarthPre SC: Ephem/EarthRot SC: Ephem/GMSTime SC: Ephem/MSidDay SC: Ephem/NutDelta SC: Ephem/ObOfE SC: Ephem/TruEarth Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Quaternion/Mat2Q Common: Quaternion/QTForm Common: Time/DTSToDTA Common: Time/Date2JD Common: Time/JD2000 Common: Time/JD2T Common: Time/JDToMidnight Math: Geometry/IntersectLineAndEllipsoid Math: Linear/Cross Math: Linear/DupVect Math: Linear/Mag Math: Linear/Unit Math: MathUtils/R2P5 Math: Trigonometry/CosD Math: Trigonometry/SinD
Back to the Orbit Module page