[astrom, pmt, eb, eh, em, v, bm1, bpn, along, xpl, ypl, sphi, cphi, diurab, eral, refa, refb, eo] = ERFA.apci13(date1, date2)
For a terrestrial observer, prepare star-independent astrometry parameters for transformations between ICRS and geocentric CIRS coordinates. The caller supplies the date, and ERFA models are used to predict the Earth ephemeris and CIP/CIO.
The parameters produced by this function are required in the parallax, light deflection, aberration, and bias-precession-nutation parts of the astrometric transformation chain.
date1 double TDB as a 2-part...
date2 double ...Julian Date (Note 1)
astrom ASTROM* star-independent astrometry parameters:
pmt double PM time interval (SSB, Julian years)
eb double[3] SSB to observer (vector, au)
eh double[3] Sun to observer (unit vector)
em double distance from Sun to observer (au)
v double[3] barycentric observer velocity (vector, c)
bm1 double sqrt(1-|v|^2): reciprocal of Lorenz factor
bpn double[3][3] bias-precession-nutation matrix
along double unchanged
xpl double unchanged
ypl double unchanged
sphi double unchanged
cphi double unchanged
diurab double unchanged
eral double unchanged
refa double unchanged
refb double unchanged
eo double* equation of the origins (ERA-GST)
- The TDB date date1+date2 is a Julian Date, apportioned in any convenient way between the two arguments. For example, JD(TDB)=2450123.7 could be expressed in any of these ways, among others:
date1 date2
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 method is best matched to the way the argument is handled internally and will deliver the optimum resolution. The MJD method and the date & time methods are both good compromises between resolution and convenience. For most applications of this function the choice will not be at all critical.
TT can be used instead of TDB without any significant impact on accuracy.
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All the vectors are with respect to BCRS axes.
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In cases where the caller wishes to supply his own Earth ephemeris and CIP/CIO, the function eraApci can be used instead of the present function.
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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.
eraEpv00 Earth position and velocity
eraPnm06a classical NPB matrix, IAU 2006/2000A
eraBpn2xy extract CIP X,Y coordinates from NPB matrix
eraS06 the CIO locator s, given X,Y, IAU 2006
eraApci astrometry parameters, ICRS-CIRS
eraEors equation of the origins, given NPB matrix and s
This revision: 2013 October 9
Copyright (C) 2013-2021, NumFOCUS Foundation. Derived, with permission, from the SOFA library.