FUNCTION	PURPOSE
slaAddet	add E-terms of aberration
slaAfin	sexagesimal character string to angle
slaAirmas	air mass
slaAltaz	velocities etc. for altazimuth mount
slaAmp	apparent to mean
slaAmpqk	quick apparent to mean
slaAop	apparent to observed
slaAoppa	apparent-to-observed parameters
slaAoppat	update apparent-to-observed parameters
slaAopqk	quick apparent to observed
slaAtmdsp	atmospheric dispersion
slaAv2m	rotation matrix from axial vector
slaBear	direction between points on a sphere
slaC2i	ICRS to CIRS
slaC2ipa	ICRS to CIRS parameters
slaC2ipad	make ICRS to CIRS parameters stop at GCRS
slaC2ipas	ICRS to CIRS parameters, space observer
slaC2iqk	quick ICRS to CIRS
slaC2iqkz	quick ICRS to CIRS, no P.M. etc.
slaCaf2r	deg,arcmin,arcsec to radians
slaCaldj	calendar date to MJD
slaCalyd	calendar date to year,day
slaCc2s	Cartesian to spherical
slaCc62s	Cartesian 6-vector to spherical
slaCd2tf	days to hour,min,sec
slaCldj	calendar date to MJD
slaClyd	calendar date to year,day
slaCombn	next combination
slaCr2af	radians to deg,arcmin,arcsec
slaCr2tf	radians to hour,min,sec
slaCs2c	spherical to Cartesian
slaCs2c6	spherical position and velocity to Cartesian
slaCtf2d	hour,min,sec to days
slaCtf2r	hour,min,sec to radians
slaDaf2r	deg,arcmin,arcsec to radians
slaDafin	sexagesimal character string to angle
slaDat	TAI-UTC
slaDav2m	rotation matrix from axial vector
slaDbear	direction between points on a sphere
slaDbjin	decode string to B/J epoch
slaDc62s	Cartesian 6-vector to spherical
slaDcc2s	Cartesian to spherical
slaDcmpf	interpret linear fit
slaDcs2c	spherical to Cartesian
slaDd2tf	days to hour,min,sec
slaDe2h	[HA,Dec] to [Az,El]
slaDeuler	Euler angles to rotation matrix
slaDfltin	decode a double precision number
slaDh2e	[Az,El] to [HA,Dec]
slaDimxv	apply 3D reverse rotation
slaDjcal	MJD to Gregorian for output
slaDjcl	MJD to year,month,day,frac
slaDm2av	rotation matrix to axial vector
slaDmat	solve simultaneous equations
slaDmoon	approximate Moon position and velocity
slaDmxm	product of two 3x3 matrices
slaDmxv	apply 3D rotation
slaDpav	position-angle between two directions
slaDr2af	radians to deg,min,sec,frac
slaDr2tf	radians to hour,min,sec,frac
slaDrange	put angle into range +/-pi
slaDranrm	put angle into range 0-2pi
slaDs2c6	spherical position and velocity to Cartesian
slaDs2tp	spherical to tangent plane
slaDsep	angle between two points on a sphere
slaDsepv	angle between two vectors
slaDt	approximate ET minus UT
slaDtf2d	hour,min,sec to days
slaDtf2r	hour,min,sec to radians
slaDtp2s	tangent plane to spherical
slaDtp2v	tangent plane to [x,y,z]
slaDtps2c	plate centre from [xi,eta] and [RA,Dec]
slaDtpv2c	plate centre from [xi,eta] and [x,y,z]
slaDtt	TT minus UTC
slaDv2tp	[x,y,z] to tangent plane
slaDvdv	scalar product
slaDvn	normalize vector
slaDvxv	vector product
slaE2h	[HA,Dec] to [Az,El]
slaEarth	approximate Earth position and velocity
slaEcleq	ecliptic to equatorial
slaEcmat	form [RA,Dec] -> [lambda,beta] matrix
slaEcor	radial velocity & light-time corrections to Sun
slaEg50	B1950 [RA,Dec] to [LII,BII]
slaEl2ue	conventional to universal elements
slaEo	equation of the origins.
slaEors	EO from NPB matrix and s
slaEpb	MJD to Besselian epoch
slaEpb2d	Besselian epoch to MJD
slaEpco	convert epoch to B or J
slaEpj	MJD to Julian epoch
slaEpj2d	Julian epoch to MJD
slaEpv	Earth position & velocity (high accuracy)
slaEqecl	J2000 [RA,Dec] to [lambda,beta]
slaEqeqx	equation of the equinoxes
slaEqgal	J2000 [RA,Dec] to [LII,BII]
slaEra	Earth rotation angle
slaEtrms	E-terms of aberration
slaEuler	rotation matrix from Euler angles
slaEvp	Earth position & velocity
slaFitxy	fit linear model to two [x,y] sets
slaFk425	FK4 to FK5
slaFk45z	FK4 to FK5, no proper motion or parallax
slaFk524	FK5 to FK4
slaFk52h	FK5 to Hipparcos
slaFk54z	FK5 to FK4, no proper motion or parallax
slaFk5hz	FK5 to Hipparcos, no proper motion
slaFlotin	decode a single-precision real number
slaFw2m	rotation matrix from F-W angles
slaFw2xy	CIP X,Y given F-W NPB angles.
slaG2ixys	GCRS to CIRS matrix given [X,Y,s]
slaGaleq	galactic to J2000 [RA,Dec]
slaGalsup	galactic to supergalactic
slaGe50	galactic to B1950 [RA,Dec]
slaGeoc	geodetic to geocentric
slaGmst	UT to GMST
slaGmsta	UT to GMST (extra precision)
slaGst	GST (from ERA and EO)
slaH2e	[Az,El] to [HA,Dec]
slaH2fk5	Hipparcos to FK5
slaHfk5z	Hipparcos to FK5, no proper motion
slaI2c	CIRS to ICRS
slaI2cqk	quick CIRS to ICRS
slaI2o	CIRS to observed place
slaI2opa	CIRS-to-observed parameters
slaI2opad	in CIRS-to-observed, disable diurnal aberration
slaI2opat	update CIRS-to-observed parameters
slaI2oqk	quick CIRS to observed place
slaImxv	apply 3D reverse rotation
slaInt2in	decode an integer number
slaIntin	decode a long integer number
slaInvf	invert linear model
slaKbj	select epoch prefix
slaM2av	rotation matrix to axial vector
slaMap	mean to apparent
slaMappa	mean to apparent parameters
slaMapqk	quick mean to apparent
slaMapqkz	quick mean to apparent, no P.M. etc.
slaMoon	approximate Moon position and velocity
slaMxm	product of two 3x3 matrices
slaMxv	apply 3D rotation
slaNu	nutation components, IAU 2006
slaNu00a	nutation, IAU 2000A
slaNut	nutation matrix
slaNutc	nutation components
slaNutc80	nutation components, IAU 1980
slaO2i	observed place to CIRS
slaO2iqk	quick observed place to CIRS
slaOap	observed to apparent
slaOapqk	quick observed to apparent
slaObs	observatory parameters
slaPa	[HA,Dec] to parallactic angle
slaPav	position-angle between two directions
slaPcd	apply radial distortion
slaPda2h	hour angle for a given azimuth
slaPdq2h	hour angle for a given parallactic angle
slaPermut	next permutation
slaPertel	perturbed orbital elements
slaPertue	perturbed universal elements
slaPfw	IAU 2006 precession angles
slaPlanel	planet position from elements
slaPlanet	planetary ephemerides, approximate
slaPlante	[RA,Dec] of planet from elements
slaPlantu	[RA,Dec] from universal elements
slaPm	proper motion
slaPncio	CIO based NPB matrix
slaPneqx	equinox based NPB matrix
slaPolmo	polar motion
slaPomom	polar motion matrix
slaPrebn	precession matrix (FK4)
slaPrec	precession matrix (IAU 1976)
slaPreces	precession
slaPrecl	precession matrix (more accurate)
slaPrenut	precession-nutation matrix
slaPv2el	orbital elements from position & velocity
slaPv2ue	position and velocity to universal elements
slaPvobs	observatory position & velocity
slaPxy	apply linear model
slaRange	put angle into range +/-pi
slaRanorm	put angle into range 0-2pi
slaRcc	barycentric coordinate time
slaRdplan	apparent [RA,Dec] of planet
slaRefco	refraction constants
slaRefcoq	refraction constants (fast)
slaRefro	refraction
slaRefv	apply refraction to vector
slaRefz	apply refraction to ZD
slaRverot	radial velocity correction to Earth centre
slaRvgalc	radial velocity correction to galactic centre
slaRvlg	radial velocity correction to local group
slaRvlsrd	radial velocity correction to dynamical LSR
slaRvlsrk	radial velocity correction to kinematical LSR
slaS	the CIO locator s
slaS2tp	spherical to tangent plane
slaSep	angle between two points on sphere
slaSepv	angle between two vectors
slaSmat	solve simultaneous equations
slaSp	the CIO locator s'
slaSubet	remove E-terms
slaSupgal	supergalactic to galactic
slaSvd	singular value decomposition
slaSvdcov	covariance matrix from SVD
slaSvdsol	solution vector from SVD
slaTp2s	tangent plane to spherical
slaTp2v	tangent plane to [x,y,z]
slaTps2c	plate centre from [xi,eta] and [RA,Dec]
slaTpv2c	plate centre from [xi,eta] and [x,y,z]
slaUe2el	universal to conventional elements
slaUe2pv	position & velocity from universal elements
slaUnpcd	remove radial distortion
slaV2tp	[x,y,z] to tangent plane
slaVdv	scalar product
slaVn	normalize vector
slaVxv	vector product
slaXy2xy	apply linear model to an [x,y]
slaZd	[HA,Dec] to zenith distance

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