Check in Moon planetary files, for CI
This should avoid something like 6 downloads per CI run.
This commit is contained in:
parent
f822f23e31
commit
4f964e556d
|
@ -0,0 +1,607 @@
|
|||
KPL/FK
|
||||
|
||||
|
||||
SPICE Lunar Reference Frame Specification Kernel
|
||||
=====================================================================
|
||||
|
||||
Original file name: moon_080317.tf
|
||||
Creation date: 2008 March 17 20:10
|
||||
Created by: Nat Bachman (NAIF/JPL)
|
||||
Date of last revision: 2008 March 21 16:07
|
||||
Purpose of revision:
|
||||
|
||||
Changed names of PA system and frame from "principal axis" to
|
||||
"principal axes."
|
||||
|
||||
|
||||
Version description:
|
||||
|
||||
This frame kernel contains lunar frame specifications compatible
|
||||
with the current lunar binary PCK file
|
||||
|
||||
moon_pa_de421_1900-2050.bpc
|
||||
|
||||
The above PCK contains lunar orientation data from the DE-421 JPL
|
||||
Planetary Ephemeris.
|
||||
|
||||
The previous NAIF lunar frame specification kernel was
|
||||
|
||||
moon_071218.tf
|
||||
|
||||
That kernel is compatible with the DE-418-based lunar binary PCK
|
||||
file
|
||||
|
||||
moon_pa_de418_1950-2050.bpc
|
||||
|
||||
The comment section below titled "Lunar body-fixed frame
|
||||
associations" discusses lunar frame association kernels. These
|
||||
kernels direct portions of the SPICE system that rely on default
|
||||
body-fixed reference frames to associate with the Moon either the
|
||||
MOON_ME or MOON_PA reference frames.
|
||||
|
||||
|
||||
This file was modified on 26-FEB-2009 by Nat Bachman. The initial
|
||||
blank line was removed and this change description was added.
|
||||
Nothing else has been changed.
|
||||
|
||||
|
||||
Frames Specified by this Kernel
|
||||
=====================================================================
|
||||
|
||||
Frame Name Relative to Type Frame ID
|
||||
-------------- ----------------- ----- --------
|
||||
MOON_PA MOON_PA_DE421 FIXED 31000
|
||||
MOON_ME MOON_ME_DE421 FIXED 31001
|
||||
MOON_PA_DE421 ICRF/J2000 PCK 31006
|
||||
MOON_ME_DE421 MOON_PA_DE421 FIXED 31007
|
||||
|
||||
|
||||
Introduction
|
||||
=====================================================================
|
||||
|
||||
This kernel specifies lunar body-fixed reference frames for use by
|
||||
SPICE-based application software. These reference frames are
|
||||
associated with high-accuracy lunar orientation data provided by the
|
||||
JPL Solar System Dynamics Group's planetary ephemerides (both
|
||||
trajectory and lunar orientation data are stored in these ephemeris
|
||||
files). These ephemerides have names of the form DE-nnn (DE stands
|
||||
for "developmental ephemeris").
|
||||
|
||||
The frames specified by this kernel are realizations of two different
|
||||
lunar reference systems:
|
||||
|
||||
Principal Axes (PA) system
|
||||
--------------------------
|
||||
The axes of this system are defined by the principal axes of the
|
||||
Moon. Due to the nature of the Moon's orbit and
|
||||
rotation, the Z axis of this system does not coincide with the
|
||||
Moon's mean spin axis, nor does the X axis coincide with the mean
|
||||
direction to the center of the Earth (in contrast with the ME
|
||||
system defined below).
|
||||
|
||||
Lunar principal axes frames realizing the lunar PA system and
|
||||
specified by this kernel are associated with JPL planetary
|
||||
ephemerides. Each new JPL planetary ephemeris can (but does not
|
||||
necessarily) define a new realization of the lunar principal axes
|
||||
system. Coordinates of lunar surface features expressed in lunar
|
||||
PA frames can change slightly from one lunar ephemeris version to
|
||||
the next.
|
||||
|
||||
|
||||
Mean Earth/Polar Axis (ME) system
|
||||
---------------------------------
|
||||
The Lunar mean Earth/polar axis system is a lunar body-fixed
|
||||
reference system used in the IAU/IAG Working Group Report [2] to
|
||||
describe the orientation of the Moon relative to the ICRF frame.
|
||||
The +Z axis of this system is aligned with the north mean lunar
|
||||
rotation axis, while the prime meridian contains the the mean
|
||||
Earth direction.
|
||||
|
||||
This system is also sometimes called the "mean Earth/mean
|
||||
rotation axis" system or "mean Earth" system.
|
||||
|
||||
The mean directions used to define the axes of a mean Earth/polar
|
||||
axis reference frame realizing the lunar ME system and specified
|
||||
by this kernel are associated with a given JPL planetary
|
||||
ephemeris version. The rotation between the mean Earth frame for
|
||||
a given ephemeris version and the associated principal axes frame
|
||||
is given by a constant matrix (see [1]).
|
||||
|
||||
|
||||
For the current JPL planetary ephemeris (DE), this kernel includes
|
||||
specifications of the corresponding principal axes and mean Earth/
|
||||
polar axis frames. The names of these frames have the form
|
||||
|
||||
MOON_PA_DEnnn
|
||||
|
||||
and
|
||||
|
||||
MOON_ME_DEnnn
|
||||
|
||||
respectively, where nnn is the version number of the DE. The set of
|
||||
DE-dependent frame specifications will grow over time; frame
|
||||
specifications pertaining to older DEs can be obtained from earlier
|
||||
versions of this frame kernel.
|
||||
|
||||
For each of the two reference systems, there is a corresponding
|
||||
"generic" frame specification: these generic frames are simply
|
||||
aliases for the PA and ME frames associated with the latest DE. The
|
||||
generic frame names are
|
||||
|
||||
MOON_PA
|
||||
MOON_ME
|
||||
|
||||
These generic frame names are provided to enable SPICE-based
|
||||
applications to refer to the latest DE-based (or other) lunar
|
||||
rotation data without requiring code modifications as new kernels
|
||||
become available. SPICE users may, if they wish, modify this kernel
|
||||
to assign these frame aliases to other frames than those selected
|
||||
here, for example, older DE-based frames. NAIF recommends that, if
|
||||
this frame kernel is modified, the name of this file also be changed
|
||||
to avoid confusion.
|
||||
|
||||
|
||||
Comparison of PA and ME frames
|
||||
------------------------------
|
||||
|
||||
The rotation between the mean Earth frame for a given DE and the
|
||||
associated principal axes frame for the same DE is given by a
|
||||
constant matrix (see [1]). For DE-421, the rotation angle of this
|
||||
matrix is approximately 0.0288473 degrees; this is equivalent to
|
||||
approximately 875 m when expressed as a displacement along a great
|
||||
circle on the Moon's surface.
|
||||
|
||||
|
||||
Comparison of DE-based and IAU/IAG report-based ME frames
|
||||
---------------------------------------------------------
|
||||
|
||||
Within the SPICE system, a lunar ME frame specified by the
|
||||
rotational elements from the IAU/IAG Working Group report [2] is
|
||||
given the name IAU_MOON; the data defining this frame are provided
|
||||
in a generic text PCK.
|
||||
|
||||
The orientation of the lunar ME frame obtained by applying the
|
||||
DE-based PA-to-ME rotation described above to the DE-based lunar
|
||||
libration data does not agree closely with the lunar ME frame
|
||||
orientation given by the rotational elements from the IAU/IAG
|
||||
Working Group report (that is, the IAU_MOON frame). The difference
|
||||
is due to truncation of the libration series used in the report's
|
||||
formula for lunar orientation (see [1]).
|
||||
|
||||
In the case of DE-421, for the time period ~2000-2020, the
|
||||
time-dependent difference of these ME frame implementations has an
|
||||
amplitude of approximately 0.0051 degrees, which is equivalent to
|
||||
approximately 155 m, measured along a great circle on the Moon's
|
||||
surface, while the average value is approximately 0.00249 degrees,
|
||||
or 76 m.
|
||||
|
||||
|
||||
Comparison of DE-421 and DE-418 Lunar Reference Frames
|
||||
======================================================
|
||||
|
||||
The magnitudes of the rotational offsets between the
|
||||
DE-418 and DE-421 realizations of the MOON_PA and MOON_ME
|
||||
frames are discussed below.
|
||||
|
||||
Note that the angle ranges shown below are ordered as signed values,
|
||||
*not* by absolute value.
|
||||
|
||||
MOON_PA frame orientation differences
|
||||
-------------------------------------
|
||||
|
||||
Tests performed by NAIF indicate an approximately 0.45 microradian
|
||||
maximum rotation between the MOON_PA_DE418 and MOON_PA_DE421 frames,
|
||||
based on a sampling of orientation data over the time period
|
||||
2000-2020. This offset corresponds to a displacement of about 0.79 m
|
||||
along a great circle on the Moon's surface.
|
||||
|
||||
When the transformation from the MOON_PA_DE418 frame to the
|
||||
MOON_PA_DE421 frame is decomposed as a 1-2-3 Euler angle sequence,
|
||||
the offset angle ranges for each axis are:
|
||||
|
||||
X axis: -3.8063e-07 to -2.9746e-07 radians
|
||||
Y axis: -2.5322e-07 to -1.8399e-07 radians
|
||||
Z axis: -9.9373e-08 to 6.0046e-08 radians
|
||||
|
||||
|
||||
MOON_ME frame orientation differences
|
||||
-------------------------------------
|
||||
|
||||
Tests performed by NAIF indicate an approximately 0.27 microradian
|
||||
maximum rotation between the MOON_ME_DE418 and MOON_ME_DE421 frames,
|
||||
based on a sampling of orientation data over the time period
|
||||
2000-2020. This offset corresponds to a displacement of about 0.46 m
|
||||
along a great circle on the Moon's surface.
|
||||
|
||||
When the transformation from the MOON_ME_DE418 frame to the
|
||||
MOON_ME_DE421 frame is decomposed as a 1-2-3 Euler angle sequence,
|
||||
the offset angle ranges for each axis are:
|
||||
|
||||
X axis: 7.2260e-09 to 9.0391e-08 radians
|
||||
Y axis: 3.7643e-08 to 1.0691e-07 radians
|
||||
Z axis: -2.4471e-07 to -8.5296e-08 radians
|
||||
|
||||
|
||||
Regarding Use of the ICRF in SPICE
|
||||
==================================
|
||||
|
||||
The IERS Celestial Reference Frame (ICRF) is offset from the J2000
|
||||
reference frame (equivalent to EME 2000) by a small rotation: the
|
||||
J2000 pole offset magnitude is about 18 milliarcseconds (mas) and
|
||||
the equinox offset magnitude is approximately 78 milliarcseconds
|
||||
(see [3]).
|
||||
|
||||
Certain SPICE data products use the frame label "J2000" for data
|
||||
that actually are referenced to the ICRF. This is the case for SPK
|
||||
files containing JPL version DE-4nn planetary ephemerides, for
|
||||
orientation data from generic text PCKs, and for binary PCKs,
|
||||
including binary lunar PCKs used in conjunction with this lunar
|
||||
frame kernel.
|
||||
|
||||
Consequently, when SPICE computes the rotation between the "J2000"
|
||||
frame and either of the lunar PA or ME frames, what's computed is
|
||||
actually the rotation between the ICRF and the respective lunar
|
||||
frame.
|
||||
|
||||
Similarly, when SPICE is used to compute the state given by a JPL DE
|
||||
planetary ephemeris SPK file of one ephemeris object relative to
|
||||
another (for example, the state of the Moon with respect to the
|
||||
Earth), expressed relative to the frame "J2000," the state is
|
||||
actually expressed relative to the ICRF.
|
||||
|
||||
Because SPICE is already using the ICRF, users normally need not
|
||||
use the J2000-to-ICRF transformation to adjust results computed
|
||||
with SPICE.
|
||||
|
||||
Lunar body-fixed frame associations
|
||||
=====================================================================
|
||||
|
||||
By default, the SPICE system considers the body-fixed reference
|
||||
frame associated with the Moon to be the one named IAU_MOON. This
|
||||
body-frame association affects the outputs of the SPICE frame system
|
||||
routines
|
||||
|
||||
CIDFRM
|
||||
CNMFRM
|
||||
|
||||
and of the SPICE time conversion and geometry routines
|
||||
|
||||
ET2LST
|
||||
ILLUM
|
||||
SRFXPT
|
||||
SUBPT
|
||||
SUBSOL
|
||||
|
||||
Also, any code that calls these routines to obtain results involving
|
||||
lunar body-fixed frames are affected. Within SPICE, the only
|
||||
higher-level system that is affected is the dynamic frame system.
|
||||
|
||||
NAIF provides "frame association" kernels that simplify changing the
|
||||
body-fixed frame associated with the Moon. Using FURNSH to load
|
||||
either of the kernels named below changes the Moon's body-fixed
|
||||
frame from its current value, which initially is IAU_MOON, to that
|
||||
shown in the right-hand column:
|
||||
|
||||
Kernel name Lunar body-fixed frame
|
||||
----------- ----------------------
|
||||
moon_assoc_me.tf MOON_ME
|
||||
moon_assoc_pa.tf MOON_PA
|
||||
|
||||
For further information see the in-line comments in the association
|
||||
kernels themselves. Also see the Frames Required Reading section
|
||||
titled "Connecting an Object to its Body-fixed Frame."
|
||||
|
||||
In the N0062 SPICE Toolkit, the routines
|
||||
|
||||
ILLUM
|
||||
SRFXPT
|
||||
SUBPT
|
||||
SUBSOL
|
||||
|
||||
are superseded, respectively, by the routines
|
||||
|
||||
ILUMIN
|
||||
SINCPT
|
||||
SUBPNT
|
||||
SUBSLR
|
||||
|
||||
The newer routines don't require frame association kernels: the name
|
||||
of the target body's body-fixed reference frame is an input argument
|
||||
to these routines.
|
||||
|
||||
|
||||
Using this Kernel
|
||||
=====================================================================
|
||||
|
||||
In order for a SPICE-based application to use reference frames
|
||||
specified by this kernel, the application must load both this kernel
|
||||
and a binary lunar PCK containing lunar orientation data for the
|
||||
time of interest. Normally the kernels need be loaded only once
|
||||
during program initialization.
|
||||
|
||||
SPICE users may find it convenient to use a meta-kernel (also called
|
||||
a "FURNSH kernel") to name the kernels to be loaded. Below, we show
|
||||
an example of such a meta-kernel, as well as the source code of a
|
||||
small Fortran program that uses lunar body fixed frames. The
|
||||
program's output is included as well.
|
||||
|
||||
The kernel names shown here are simply used as examples; users must
|
||||
select the kernels appropriate for their applications.
|
||||
|
||||
Numeric results shown below may differ very slightly from those
|
||||
obtained on users' computer systems.
|
||||
|
||||
|
||||
Meta-kernel
|
||||
-----------
|
||||
|
||||
|
||||
KPL/MK
|
||||
|
||||
|
||||
Example meta-kernel showing use of
|
||||
|
||||
- binary lunar PCK
|
||||
- generic lunar frame kernel (FK)
|
||||
- leapseconds kernel (LSK)
|
||||
- planetary SPK
|
||||
|
||||
17-MAR-2008 (NJB)
|
||||
|
||||
Note: to actually use this kernel, replace the @ characters
|
||||
below with backslashes (\). The backslash character cannot be
|
||||
used here, within the comments of this frame kernel, because the
|
||||
begindata and begintext strings would be interpreted as
|
||||
directives bracketing actual load commands.
|
||||
|
||||
This meta-kernel assumes that the referenced kernels exist
|
||||
in the user's current working directory.
|
||||
|
||||
@begindata
|
||||
|
||||
KERNELS_TO_LOAD = ( 'moon_pa_de421_1900-2050.bpc'
|
||||
'moon_080317.tf'
|
||||
'leapseconds.ker'
|
||||
'de421.bsp' )
|
||||
|
||||
@begintext
|
||||
|
||||
|
||||
Example program
|
||||
---------------
|
||||
|
||||
PROGRAM EX1
|
||||
IMPLICIT NONE
|
||||
|
||||
INTEGER FILSIZ
|
||||
PARAMETER ( FILSIZ = 255 )
|
||||
|
||||
CHARACTER*(FILSIZ) META
|
||||
|
||||
DOUBLE PRECISION ET
|
||||
DOUBLE PRECISION LT
|
||||
DOUBLE PRECISION STME ( 6 )
|
||||
DOUBLE PRECISION STPA ( 6 )
|
||||
|
||||
C
|
||||
C Prompt user for meta-kernel name.
|
||||
C
|
||||
CALL PROMPT ( 'Enter name of meta-kernel > ', META )
|
||||
|
||||
C
|
||||
C Load lunar PCK, generic lunar frame kernel,
|
||||
C leapseconds kernel, and planetary ephemeris
|
||||
C via metakernel.
|
||||
C
|
||||
CALL FURNSH ( META )
|
||||
|
||||
C
|
||||
C Convert a time of interest from UTC to ET.
|
||||
C
|
||||
CALL STR2ET ( '2008 MAR 17 20:10:00', ET )
|
||||
|
||||
WRITE (*,*) 'ET (sec past J2000 TDB): ', ET
|
||||
WRITE (*,*) ' State of Earth relative to Moon'
|
||||
|
||||
C
|
||||
C Find the geometric state of the Earth relative to the
|
||||
C Moon at ET, expressed relative to the ME frame.
|
||||
C
|
||||
CALL SPKEZR ( 'Earth', ET, 'MOON_ME',
|
||||
. 'NONE', 'Moon', STME, LT )
|
||||
|
||||
WRITE (*,*) ' In MOON_ME frame:'
|
||||
WRITE (*,*) STME
|
||||
|
||||
C
|
||||
C Find the geometric state of the Earth relative to the
|
||||
C Moon at ET, expressed relative to the PA frame.
|
||||
C
|
||||
CALL SPKEZR ( 'Earth', ET, 'MOON_PA',
|
||||
. 'NONE', 'Moon', STPA, LT )
|
||||
|
||||
WRITE (*,*) ' In MOON_PA frame:'
|
||||
WRITE (*,*) STPA
|
||||
|
||||
END
|
||||
|
||||
|
||||
Program output
|
||||
--------------
|
||||
|
||||
Enter name of meta-kernel > meta
|
||||
ET (sec past J2000 TDB): 259056665.
|
||||
State of Earth relative to Moon
|
||||
In MOON_ME frame:
|
||||
379892.825 33510.118 -12661.5278 0.0400357582 0.0117963334 0.115130508
|
||||
In MOON_PA frame:
|
||||
379908.634 33385.003 -12516.8859 0.0399957879 0.0117833314 0.115145731
|
||||
|
||||
|
||||
|
||||
References
|
||||
=====================================================================
|
||||
|
||||
[1] J.G. Williams, D.H. Boggs and W.M. Folkner. "DE421 Lunar
|
||||
Orbit, Physical Librations, and Surface Coordinates,"
|
||||
preprint of JPL IOM 335-JW,DB,WF-20080314-001, dated
|
||||
March 14, 2008.
|
||||
|
||||
[2] Seidelmann, P.K., Abalakin, V.K., Bursa, M., Davies, M.E.,
|
||||
Bergh, C. de, Lieske, J.H., Oberst, J., Simon, J.L., Standish,
|
||||
E.M., Stooke, P., and Thomas, P.C. (2002). "Report of the
|
||||
IAU/IAG Working Group on Cartographic Coordinates and Rotational
|
||||
Elements of the Planets and Satellites: 2000," Celestial
|
||||
Mechanics and Dynamical Astronomy, v.82, Issue 1, pp. 83-111.
|
||||
|
||||
[3] Roncoli, R. (2005). "Lunar Constants and Models Document,"
|
||||
JPL D-32296.
|
||||
|
||||
|
||||
Frame Specifications
|
||||
=====================================================================
|
||||
|
||||
MOON_PA is the name of the generic lunar principal axes (PA) reference
|
||||
frame. This frame is an alias for the principal axes frame defined
|
||||
by the latest version of the JPL Solar System Dynamics Group's
|
||||
planetary ephemeris.
|
||||
|
||||
In this instance of the lunar reference frames kernel, MOON_PA is an
|
||||
alias for the lunar principal axes frame associated with the
|
||||
planetary ephemeris DE-421.
|
||||
|
||||
\begindata
|
||||
|
||||
FRAME_MOON_PA = 31000
|
||||
FRAME_31000_NAME = 'MOON_PA'
|
||||
FRAME_31000_CLASS = 4
|
||||
FRAME_31000_CLASS_ID = 31000
|
||||
FRAME_31000_CENTER = 301
|
||||
|
||||
TKFRAME_31000_SPEC = 'MATRIX'
|
||||
TKFRAME_31000_RELATIVE = 'MOON_PA_DE421'
|
||||
TKFRAME_31000_MATRIX = ( 1 0 0
|
||||
0 1 0
|
||||
0 0 1 )
|
||||
|
||||
\begintext
|
||||
|
||||
MOON_ME is the name of the generic lunar mean Earth/polar axis (ME)
|
||||
reference frame. This frame is an alias for the mean Earth/polar
|
||||
axis frame defined by the latest version of the JPL Solar System
|
||||
Dynamics Group's planetary ephemeris.
|
||||
|
||||
In this instance of the lunar reference frames kernel, MOON_ME is an
|
||||
alias for the lunar mean Earth/polar axis frame associated with the
|
||||
planetary ephemeris DE-421.
|
||||
|
||||
\begindata
|
||||
|
||||
FRAME_MOON_ME = 31001
|
||||
FRAME_31001_NAME = 'MOON_ME'
|
||||
FRAME_31001_CLASS = 4
|
||||
FRAME_31001_CLASS_ID = 31001
|
||||
FRAME_31001_CENTER = 301
|
||||
|
||||
TKFRAME_31001_SPEC = 'MATRIX'
|
||||
TKFRAME_31001_RELATIVE = 'MOON_ME_DE421'
|
||||
TKFRAME_31001_MATRIX = ( 1 0 0
|
||||
0 1 0
|
||||
0 0 1 )
|
||||
|
||||
|
||||
\begintext
|
||||
|
||||
|
||||
MOON_PA_DE421 is the name of the lunar principal axes
|
||||
reference frame defined by JPL's DE-421 planetary ephemeris.
|
||||
|
||||
\begindata
|
||||
|
||||
FRAME_MOON_PA_DE421 = 31006
|
||||
FRAME_31006_NAME = 'MOON_PA_DE421'
|
||||
FRAME_31006_CLASS = 2
|
||||
FRAME_31006_CLASS_ID = 31006
|
||||
FRAME_31006_CENTER = 301
|
||||
|
||||
FRAME_MOON_PA_DE403 = 31002
|
||||
FRAME_31002_NAME = 'MOON_PA_DE403'
|
||||
FRAME_31002_CLASS = 2
|
||||
FRAME_31002_CLASS_ID = 31002
|
||||
FRAME_31002_CENTER = 301
|
||||
|
||||
|
||||
|
||||
|
||||
\begintext
|
||||
|
||||
MOON_ME_DE421 is the name of the lunar mean Earth/polar
|
||||
axis reference frame defined by JPL's DE-421 planetary ephemeris.
|
||||
|
||||
Rotation angles are from reference [1].
|
||||
|
||||
\begindata
|
||||
|
||||
FRAME_MOON_ME_DE421 = 31007
|
||||
FRAME_31007_NAME = 'MOON_ME_DE421'
|
||||
FRAME_31007_CLASS = 4
|
||||
FRAME_31007_CLASS_ID = 31007
|
||||
FRAME_31007_CENTER = 301
|
||||
|
||||
TKFRAME_31007_SPEC = 'ANGLES'
|
||||
TKFRAME_31007_RELATIVE = 'MOON_PA_DE421'
|
||||
TKFRAME_31007_ANGLES = ( 67.92 78.56 0.30 )
|
||||
TKFRAME_31007_AXES = ( 3, 2, 1 )
|
||||
TKFRAME_31007_UNITS = 'ARCSECONDS'
|
||||
|
||||
\begintext
|
||||
|
||||
|
||||
Updating this Kernel
|
||||
--------------------
|
||||
|
||||
When a new JPL DE providing lunar rotation data becomes available,
|
||||
the new lunar PA frame associated with that data set will be named
|
||||
|
||||
MOON_PA_DEnnn
|
||||
|
||||
where nnn is the version number of the DE.
|
||||
|
||||
The PCK body ID code associated with that data set will be
|
||||
|
||||
31008
|
||||
|
||||
The frame ID and class ID for this frame will also be 31008.
|
||||
|
||||
The generic PA frame specification will be updated to point to the
|
||||
new DE-specific PA frame. The rest of this frame specification
|
||||
is unchanged.
|
||||
|
||||
The ME frame name associated with the new data set will be named
|
||||
|
||||
MOON_ME_DEnnn
|
||||
|
||||
The frame ID and class ID for this frame will be
|
||||
|
||||
31009
|
||||
|
||||
The rotational offset between this frame and the new DE-specific PA
|
||||
frame will need to be updated; this offset is DE-dependent.
|
||||
|
||||
The generic ME frame specification will be updated to point to the
|
||||
new DE-specific ME frame. The rest of this frame specification
|
||||
is unchanged.
|
||||
|
||||
|
||||
|
||||
=====================================================================
|
||||
End of kernel
|
||||
|
||||
|
||||
|
||||
|
||||
|
||||
|
||||
|
||||
|
||||
|
Binary file not shown.
File diff suppressed because it is too large
Load Diff
Loading…
Reference in New Issue