[astrom, pmt, eb, eh, em, v, bm1, bpn, along, xpl, ypl, sphi, cphi, diurab, eral, refa, refb] = ERFA.aper13(ut11, ut12)In the star-independent astrometry parameters, update only the Earth rotation angle. The caller provides UT1, (n.b. not UTC).
ut11 double UT1 as a 2-part...
ut12 double ...Julian Date (Note 1)
astrom ASTROM* star-independent astrometry parameters:
pmt double not used
eb double[3] not used
eh double[3] not used
em double not used
v double[3] not used
bm1 double not used
bpn double[3][3] not used
along double longitude + s' (radians)
xpl double not used
ypl double not used
sphi double not used
cphi double not used
diurab double not used
eral double not used
refa double not used
refb double not used
astrom ASTROM* star-independent astrometry parameters:
pmt double unchanged
eb double[3] unchanged
eh double[3] unchanged
em double unchanged
v double[3] unchanged
bm1 double unchanged
bpn double[3][3] unchanged
along double unchanged
xpl double unchanged
ypl double unchanged
sphi double unchanged
cphi double unchanged
diurab double unchanged
eral double "local" Earth rotation angle (radians)
refa double unchanged
refb double unchanged
- The UT1 date (n.b. not UTC) ut11+ut12 is a Julian Date, apportioned in any convenient way between the arguments ut11 and ut12. For example, JD(UT1)=2450123.7 could be expressed in any of these ways, among others:
ut11 ut12
2450123.7 0.0 (JD method)
2451545.0 -1421.3 (J2000 method)
2400000.5 50123.2 (MJD method)
2450123.5 0.2 (date & time method)
The JD method is the most natural and convenient to use in cases where the loss of several decimal digits of resolution is acceptable. The J2000 and MJD methods are good compromises between resolution and convenience. The date & time method is best matched to the algorithm used: maximum precision is delivered when the ut11 argument is for 0hrs UT1 on the day in question and the ut12 argument lies in the range 0 to 1, or vice versa.
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If the caller wishes to provide the Earth rotation angle itself, the function eraAper can be used instead. One use of this technique is to substitute Greenwich apparent sidereal time and thereby to support equinox based transformations directly.
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This is one of several functions that inserts into the astrom structure star-independent parameters needed for the chain of astrometric transformations ICRS <-> GCRS <-> CIRS <-> observed.
The various functions support different classes of observer and portions of the transformation chain:
functions observer transformation
eraApcg eraApcg13 geocentric ICRS <-> GCRS
eraApci eraApci13 terrestrial ICRS <-> CIRS
eraApco eraApco13 terrestrial ICRS <-> observed
eraApcs eraApcs13 space ICRS <-> GCRS
eraAper eraAper13 terrestrial update Earth rotation
eraApio eraApio13 terrestrial CIRS <-> observed
Those with names ending in "13" use contemporary ERFA models to compute the various ephemerides. The others accept ephemerides supplied by the caller.
The transformation from ICRS to GCRS covers space motion, parallax, light deflection, and aberration. From GCRS to CIRS comprises frame bias and precession-nutation. From CIRS to observed takes account of Earth rotation, polar motion, diurnal aberration and parallax (unless subsumed into the ICRS <-> GCRS transformation), and atmospheric refraction.
eraAper astrometry parameters: update ERA
eraEra00 Earth rotation angle, IAU 2000
This revision: 2013 September 25
Copyright (C) 2013-2021, NumFOCUS Foundation. Derived, with permission, from the SOFA library.