void sxform_c ( ConstSpiceChar * from,
ConstSpiceChar * to,
SpiceDouble et,
SpiceDouble xform[6][6] )
Return the state transformation matrix from one frame to
another at a specified epoch.
FRAMES
FRAMES
VARIABLE I/O DESCRIPTION
-------- --- --------------------------------------------------
from I Name of the frame to transform from.
to I Name of the frame to transform to.
et I Epoch of the state transformation matrix.
xform O A state transformation matrix.
from is the name of a reference frame in which a state is
known.
to is the name of a reference frame in which it is desired
to represent the state.
et is the epoch in ephemeris seconds past the epoch of
J2000 (TDB) at which the state transformation matrix
should be evaluated.
xform is the matrix that transforms states from the reference
frame `from' to the frame `to' at epoch `et'. If (x, y,
z, dx, dy, dz) is a state relative to the frame `from'
then the vector ( x', y', z', dx', dy', dz' ) is the
same state relative to the frame `to' at epoch `et'.
Here the vector ( x', y', z', dx', dy', dz' ) is defined
by the equation:
- - - - - -
| x' | | | | x |
| y' | | | | y |
| z' | = | xform | | z |
| dx' | | | | dx |
| dy' | | | | dy |
| dz' | | | | dz |
- - - - - -
None.
1) If sufficient information has not been supplied via loaded
SPICE kernels to compute the transformation between the
two frames, the error will be diagnosed by a routine
in the call tree of this routine.
2) If either frame `from' or `to' is not recognized the error
SPICE(UNKNOWNFRAME) will be signaled.
None.
This routine provides the user level interface for computing
state transformations from one reference frame to another.
Note that the reference frames may be inertial or non-inertial.
However, the user must take care that sufficient SPICE kernel
information is loaded to provide a complete state transformation
path from the `from' frame to the `to' frame.
Suppose that you have geodetic coordinates of a station on
the surface of the earth and that you need the inertial
(J2000) state of this station. The following code fragment
illustrates how to transform the position of the station to
a J2000 state.
#include "SpiceUsr.h"
.
.
.
bodvcd_c ( 399, radii, 3, &n, abc );
equatr = abc[0];
polar = abc[2];
f = (equatr - polar) / equatr;
georec_c ( long, lat, 0.0, equatr, f, estate );
estate[3] = 0.0;
estate[4] = 0.0;
estate[5] = 0.0;
sxform_c ( "IAU_EARTH", "J2000", et, xform );
mxvg_c ( xform, estate, 6, 6, jstate );
The state `jstate' is the desired J2000 state of the station.
None.
None.
C.H. Acton (JPL)
N.J. Bachman (JPL)
B.V. Semenov (JPL)
W.L. Taber (JPL)
-CSPICE Version 1.1.3, 27-FEB-2008 (BVS)
Added FRAMES to the Required_Reading section of the header.
-CSPICE Version 1.1.2, 24-OCT-2005 (NJB)
Header updates: example had invalid flattening factor
computation; this was corrected. Reference to bodvar_c was
replaced with reference to bodvcd_c.
-CSPICE Version 1.1.1, 03-JUL-2003 (NJB) (CHA)
Various header corrections were made.
-CSPICE Version 1.1.0, 08-FEB-1998 (NJB)
References to C2F_CreateStr_Sig were removed; code was
cleaned up accordingly. String checks are now done using
the macro CHKFSTR.
-CSPICE Version 1.0.0, 25-OCT-1997 (NJB)
Based on SPICELIB Version 1.0.0, 19-SEP-1995 (WLT)
Find a state transformation matrix
Link to routine sxform_c source file sxform_c.c
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