-
Notifications
You must be signed in to change notification settings - Fork 2
Commit
This commit does not belong to any branch on this repository, and may belong to a fork outside of the repository.
- Loading branch information
1 parent
c38eb9b
commit d78c4bd
Showing
11 changed files
with
5,557 additions
and
0 deletions.
There are no files selected for viewing
Large diffs are not rendered by default.
Oops, something went wrong.
Binary file not shown.
This file contains bidirectional Unicode text that may be interpreted or compiled differently than what appears below. To review, open the file in an editor that reveals hidden Unicode characters.
Learn more about bidirectional Unicode characters
Original file line number | Diff line number | Diff line change |
---|---|---|
@@ -0,0 +1,179 @@ | ||
|
||
Low accuracy, long term predict earth PCK | ||
========================================= | ||
|
||
Created by: Nat Bachman (NAIF/JPL) | ||
Creation date: 2023-06-03T03:59:00 | ||
Program version: WRTPEM Version 7.0.0, 02-JUN-2023 | ||
Original file name: earth_200101_990825_predict.bpc | ||
|
||
Data Sources | ||
|
||
Input file: extended EOP created from | ||
|
||
JPL EOP file latest.long | ||
(Copied from WWW URL | ||
http://epic.jpl.nasa.gov/nav/eop/latest.long) | ||
|
||
Source EOP metadata: | ||
|
||
$ JPL Earth Orientation Parameter File | ||
$ Last Data Point 1-JUN-2023 | ||
$ Predicts to 25-AUG-2023 | ||
$ | ||
EOPLBL='EOP. LAST DATUM 1-JUN-2023. PREDICTS->25-AUG-2023, UT1TYP=UT1. ' | ||
EOPFNG='Enter MAKE_EOP 2-Jun-2023 11:03:48 linked 05-Aug-2020 19:40:42 ' | ||
EOPUT1='UT1' | ||
EOPTYP='EOP' | ||
EOPTIM=' 2-Jun-2023 11:03:48 ' | ||
EOPTRF='ITRF93' | ||
EOPCRF='ICRF93' | ||
|
||
Input file: leapseconds kernel naif0012.tls | ||
|
||
|
||
Coverage | ||
|
||
Start time: 2020 JAN 01 00:01:09.183 TDB | ||
Stop time: 2099 AUG 25 00:01:09.182 TDB | ||
|
||
UTC Epoch of last datum: 1-JUN-2023 | ||
|
||
Particulars | ||
|
||
This is low-accuracy predict PCK file giving the orientation of the Earth as | ||
a function of time for the interval shown above. This PCK file is made from | ||
an extended EOP file which consists of the JPL EOP file named above, with | ||
four extra records appended. These records are designed to add 76 years to | ||
the coverage of the EOP file without affecting interpolated data values for | ||
times within the coverage interval of the original EOP file. Data values | ||
of records in the extended interval are constant, with the exception of | ||
the TAI-UT1 offsets. Those are adjusted so that the corresponding values | ||
of TAI-UT1R are constant. | ||
|
||
The terrestrial frame whose orientation is given by this file is ITRF93; the | ||
inertial base frame is Ecliptic of J2000. Rotational effects included are: | ||
|
||
-Precession (1976 IAU model) | ||
-Nutation (1980 IAU model) | ||
-Nutation corrections | ||
-Rotation through true sidereal time | ||
-Polar motion | ||
|
||
Euler angles have been extracted from the Ecliptic-to-ITRF93 rotation matrix, | ||
and Chebyshev polynomials were fit to the Euler angles. The Chebyshev | ||
expansion degree was 49; the degree of the retained polynomials is 20. | ||
The coverage interval for each set of polynomials is 1 day or less. | ||
|
||
This file represents the same earth orientation as does the cited EOP file | ||
for the time range: | ||
|
||
01-JAN-2020 UTC | ||
25-AUG-2023 UTC | ||
|
||
That EOP file was extended as described below. The extended EOP file | ||
was used to create this binary PCK file. | ||
|
||
For epochs after the end of EOP coverage, polar motion and nutation | ||
corrections from the EOP file are held constant at values obtained by | ||
extrapolating 1 day from the last source EOP record. TAI-UT1 values are | ||
set so that the corresponding TAI-UT1R values at each epoch of the | ||
extrapolated records are equal. Details of the EOP extrapolation process | ||
are given below. | ||
|
||
Let n be the number of data records in the original EOP file. Let | ||
MJD(i) be the epoch of the ith record expressed as a modified | ||
Julian date. The added records have the following | ||
characteristics: | ||
|
||
Record n+1: Epoch is MJD(n) + 1. Nutation correction and polar | ||
motion values are obtained by extrapolating to the | ||
epoch a cubic Lagrange interpolating polynomial | ||
fitted to the corresponding data in records n-3 : n. | ||
TAI-UT1 is obtained by converting to TAI-UT1R the | ||
TAI-UT1 data in records n-3 : n, extrapolating an | ||
interpolating polynomial as for the other data, then | ||
converting the extrapolated TAI-UTR1 value to TAI-UT1. | ||
UTC string is consistent with the MJD epoch. | ||
|
||
Record n+2: Epoch is MJD(n) + 2. Nutation correction and polar | ||
motion values match those of record n+1. TAI-UT1 is | ||
set so that the corresponding value of TAI-UT1R at | ||
this epoch is that corresponding to TAI-UT1 at the | ||
epoch of record n+1. UTC string is consistent with the | ||
MJD epoch. | ||
|
||
Record n+3: Epoch is MJD(n) + 3. Data values are as described for | ||
record n+2, adjusted for this epoch. | ||
|
||
Record n+4: Epoch is MJD(n) + 28854. Data values are as described | ||
for record n+2, adjusted for this epoch. | ||
|
||
In all of the four records described above, the values of TAI-UT1 | ||
have been selected so the corresponding values of TAI-UT1R are | ||
constant and equal to the value resulting from extrapolating the cubic | ||
interpolating polynomial for TAI-UT1R, fitted to the final four values | ||
of TAI-UT1R derived from the original EOP file, to the epoch of | ||
record n+1. | ||
|
||
The expected behavior of the interpolation algorithm is as follows: | ||
|
||
Time range Interpolation characteristics | ||
============ ============================= | ||
|
||
Epoch of record 1 to | ||
epoch of record n-1: Interpolation is identical to standard EOP | ||
file, up to round-off error. | ||
|
||
Orientation error relative to that provided | ||
by a binary PCK derived from the source EOP | ||
file is non-zero due to differences in the | ||
Chebyshev fitting process. Error is at the | ||
0.031 nanoradian level. | ||
|
||
Epoch of record n-1 to | ||
epoch of record n: Nearly identical to standard EOP file; | ||
small round-off error will occur. | ||
|
||
Orientation error relative to that provided | ||
by a binary PCK derived from the source EOP | ||
file at the at the 0.017 nanoradian level | ||
[sic]. | ||
|
||
Epoch of record n to | ||
epoch of record n+1: Some ringing of interpolated data | ||
will occur. This interval has duration 1 day. | ||
|
||
Orientation difference relative to the | ||
IAU_EARTH reference frame's rotation model | ||
is at the 1.38 milliradian level. | ||
|
||
Epoch of record n+1 to | ||
epoch of record n+2: Some ringing of interpolated data will occur. | ||
This interval has duration 1 day. | ||
|
||
Orientation difference relative to the | ||
IAU_EARTH reference frame's rotation model | ||
is at the 1.38 milliradian level. | ||
|
||
Epoch of record n+2 to | ||
epoch of record n+3: Ideally nutation corrections and polar | ||
motion will be constant, as will TAI-UT1R | ||
derived from TAI-UT1 values in the file. | ||
Some round-off error should be expected. | ||
This interval has duration 1 day. | ||
|
||
Orientation difference relative to the | ||
IAU_EARTH reference frame's rotation model | ||
is at the 1.39 milliradian level. | ||
|
||
Epoch of record n+3 to | ||
epoch of record n+4: Data are as described for records n+2 to | ||
n+3. This interval has duration ~76 years. | ||
|
||
Orientation difference relative to the | ||
IAU_EARTH reference frame's rotation model | ||
ranges from the 1.39 milliradian level at | ||
the interval start to the 4.45 milliradian | ||
level at the end. | ||
|
Binary file not shown.
This file contains bidirectional Unicode text that may be interpreted or compiled differently than what appears below. To review, open the file in an editor that reveals hidden Unicode characters.
Learn more about bidirectional Unicode characters
Original file line number | Diff line number | Diff line change |
---|---|---|
@@ -0,0 +1,55 @@ | ||
|
||
Binary "High Accuracy" Earth PCK File | ||
===================================== | ||
|
||
Created by: NAIF/JPL | ||
Creation date: 2023-06-03T04:33:29 | ||
Program version: WRTPEM Version 7.0.0, 02-JUN-2023 | ||
Original file name: earth_720101_230601.bpc | ||
|
||
Data Sources | ||
|
||
Input EOP file: latest.long | ||
Input LSK: naif0012.tls | ||
|
||
Coverage | ||
|
||
ET Start time: 1972 JAN 01 00:00:42.183 TDB | ||
ET Stop time: 2023 JUN 01 00:01:09.184 TDB | ||
|
||
UTC Epoch of last datum: 2023 JUN 01 00:00:00.000 UTC | ||
|
||
Particulars | ||
|
||
The body ID code used in this file for the Earth is 3000; this | ||
number indicates that the terrestrial frame used is ITRF93. | ||
|
||
This file is a "high-precision" PCK file giving the orientation of | ||
the Earth as a function of time for the interval shown above. The | ||
terrestrial frame is ITRF93; the inertial base frame is Ecliptic of | ||
J2000. Rotational effects included are: | ||
|
||
-Precession (1976 IAU model) | ||
-Nutation (1980 IAU model) | ||
-Rotation through true sidereal time | ||
-Polar motion | ||
-Nutation corrections | ||
|
||
Euler angles have been extracted from the Ecliptic-to-ITRF93 | ||
rotation matrix, and Chebyshev polynomials were fit to the | ||
Euler angles. The Chebyshev expansion degree was 49; the | ||
degree of the retained polynomials is 20. The coverage | ||
interval for each set of polynomials is 1 day or less. | ||
|
||
Usage | ||
|
||
This file may be used for applications requiring earth orientation | ||
accuracy of several microradians. | ||
|
||
Note that high accuracy transformation of station locations | ||
from terrestrial to inertial reference frames requires | ||
accounting for motion of the station relative to the terrestrial | ||
reference frame; such motion is not reflected by the rotation | ||
data in this file. | ||
|
||
******************************************************************************** |
Binary file not shown.
This file contains bidirectional Unicode text that may be interpreted or compiled differently than what appears below. To review, open the file in an editor that reveals hidden Unicode characters.
Learn more about bidirectional Unicode characters
Original file line number | Diff line number | Diff line change |
---|---|---|
@@ -0,0 +1,55 @@ | ||
|
||
Binary "High Accuracy" Earth PCK File | ||
===================================== | ||
|
||
Created by: NAIF/JPL | ||
Creation date: 2023-09-14T17:07:02 | ||
Program version: WRTPEM Version 7.0.0, 02-JUN-2023 | ||
Original file name: /home/nbachman/make_earth_pck/earth_000101_231207_230914.bpc | ||
|
||
Data Sources | ||
|
||
Input EOP file: /home/nbachman/make_earth_pck/latest.long | ||
Input LSK: /group/naif/kernels/gen/lsk/leapseconds.ker | ||
|
||
Coverage | ||
|
||
ET Start time: 2000 JAN 01 00:01:04.183 TDB | ||
ET Stop time: 2023 DEC 07 00:01:09.183 TDB | ||
|
||
UTC Epoch of last datum: 2023 SEP 14 00:00:00.000 UTC | ||
|
||
Particulars | ||
|
||
The body ID code used in this file for the Earth is 3000; this | ||
number indicates that the terrestrial frame used is ITRF93. | ||
|
||
This file is a "high-precision" PCK file giving the orientation of | ||
the Earth as a function of time for the interval shown above. The | ||
terrestrial frame is ITRF93; the inertial base frame is Ecliptic of | ||
J2000. Rotational effects included are: | ||
|
||
-Precession (1976 IAU model) | ||
-Nutation (1980 IAU model) | ||
-Rotation through true sidereal time | ||
-Polar motion | ||
-Nutation corrections | ||
|
||
Euler angles have been extracted from the Ecliptic-to-ITRF93 | ||
rotation matrix, and Chebyshev polynomials were fit to the | ||
Euler angles. The Chebyshev expansion degree was 49; the | ||
degree of the retained polynomials is 20. The coverage | ||
interval for each set of polynomials is 1 day or less. | ||
|
||
Usage | ||
|
||
This file may be used for applications requiring earth orientation | ||
accuracy of several microradians. | ||
|
||
Note that high accuracy transformation of station locations | ||
from terrestrial to inertial reference frames requires | ||
accounting for motion of the station relative to the terrestrial | ||
reference frame; such motion is not reflected by the rotation | ||
data in this file. | ||
|
||
******************************************************************************** |
Oops, something went wrong.