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SUPPORT SITE |
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Path: Orbit/OrbitMechanics
% Compute ground coverage for an orbit.
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Form:
[lat, lon] = GroundCoverage( xECI, jD, d )
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Inputs
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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
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Outputs
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lat (1,4) Latitude of the coverage points
lon (1,4) Longitude of the coverage points
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AerospaceUtils: Coord/Gc2GdLat AerospaceUtils: Coord/QLVLH AerospaceUtils: Coord/R2LatLon Common: Quaternion/QTForm Common: Time/JD2T Math: Geometry/IntersectLineAndEllipsoid SC: Ephem/TruEarth
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