From d54fe7c1f704a63824c5bfa0ece65245572e9b27 Mon Sep 17 00:00:00 2001 From: Joseph Hunkeler Date: Wed, 4 Mar 2015 21:21:30 -0500 Subject: Initial commit --- src/slalib/sun67.htx/node152.html | 145 ++++++++++++++++++++++++++++++++++++++ 1 file changed, 145 insertions(+) create mode 100644 src/slalib/sun67.htx/node152.html (limited to 'src/slalib/sun67.htx/node152.html') diff --git a/src/slalib/sun67.htx/node152.html b/src/slalib/sun67.htx/node152.html new file mode 100644 index 0000000..9e5ea39 --- /dev/null +++ b/src/slalib/sun67.htx/node152.html @@ -0,0 +1,145 @@ + + + + +SLA_PREC - Precession Matrix (FK5) + + + + + + + + + + + + +

+ +next + +up + +previous +
+ Next: SLA_PRECES - Precession +
+Up: SUBPROGRAM SPECIFICATIONS +
+ Previous: SLA_PREBN - Precession Matrix (FK4) +

+

+

SLA_PREC - Precession Matrix (FK5) +   +

+
+
ACTION: +
Form the matrix of precession between two epochs (IAU 1976, FK5). +
CALL: +
CALL sla_PREC (EP0, EP1, RMATP) +

+

+
GIVEN: +
+
+ + + + + + + + + +
EP0Dbeginning epoch
EP1Dending epoch
+

+
RETURNED: +
+
+ + + + + +
RMATPD(3,3)precession matrix
+

+
NOTES: +
+
1. +
The epochs are TDB Julian epochs. +
2. +
The matrix is in the sense: +
v1 = M$\cdot$v0
+ where v1 is the star vector relative to the + mean equator and equinox of epoch EP1, M is the + $3\times3$ matrix RMATP and + v0 is the star vector relative to the + mean equator and equinox of epoch EP0. +
3. +
Though the matrix method itself is rigorous, the precession + angles are expressed through canonical polynomials which are + valid only for a limited time span. There are also known + errors in the IAU precession rate. The absolute accuracy + of the present formulation is better than + $0\hspace{-0.05em}^{'\hspace{-0.1em}'}\hspace{-0.4em}.1$ from + 1960AD to 2040AD, better than $1\hspace{-0.05em}^{'\hspace{-0.1em}'}$ from 1640AD to 2360AD, + and remains below $3\hspace{-0.05em}^{'\hspace{-0.1em}'}$ for the whole of the period + 500BC to 3000AD. The errors exceed $10\hspace{-0.05em}^{'\hspace{-0.1em}'}$ outside the + range 1200BC to 3900AD, exceed $100\hspace{-0.05em}^{'\hspace{-0.1em}'}$ outside 4200BC to + 5600AD and exceed $1000\hspace{-0.05em}^{'\hspace{-0.1em}'}$ outside 6800BC to 8200AD. + The SLALIB routine sla_PRECL implements a more elaborate + model which is suitable for problems spanning several + thousand years. +
+

+
REFERENCES: +
+
1. +
Lieske, J.H., 1979. Astr.Astrophys. 73, 282; +equations 6 & 7, p283. +
2. +
Kaplan, G.H., 1981. USNO circular no. 163, pA2. +
+

+ +next + +up + +previous +
+ Next: SLA_PRECES - Precession +
+Up: SUBPROGRAM SPECIFICATIONS +
+ Previous: SLA_PREBN - Precession Matrix (FK4) +

+

+

+SLALIB --- Positional Astronomy Library
Starlink User Note 67
P. T. Wallace
12 October 1999
E-mail:ptw@star.rl.ac.uk
+
+ + -- cgit