Here's what the Red Hat test machine sees for the SRP-NPlates version.
It is talking 16+ minutes to run in that build.
Enter a script file, q to quit, or an option:
/home/buildbot/jazz/test/script/input/Resources/FRR-24_MeasurementSimulator/scripts/Simulator_AsteroidOccultation.script
Interpreting scripts from the file.
***** file:
/home/buildbot/jazz/test/script/input/Resources/FRR-24_MeasurementSimulator/scripts/Simulator_AsteroidOccultation.script
Successfully set Planetary Source to use: DE405
Successfully set Planetary Source to use: DE405
**** WARNING **** RungeKutta4 is an integrator with no error control.
The accuracy setting will be ignored.
*** WARNING *** "BatchEstimatorInv" resource is deprecated and will be
removed from a future build; please use "BatchEstimator" instead.
Setting value for bat.EstimationEpoch has no effect due to
bat.EstimationEpochFormat to be "FromParticipants"
Kernel ../data/planetary_ephem/spk/DE421AllPlanets.bsp has been loaded.
Kernel ../data/planetary_coeff/SPICEPlanetaryConstantsKernel.tpc has
been loaded.
Kernel ../data/time/SPICELeapSecondKernel.tls has been loaded.
Kernel ../data/planetary_ephem/spk/de421.bsp has been loaded.
Kernel ../data/planetary_ephem/spk/ceres_1900_2100.bsp has been loaded.
Successfully interpreted the script
.................... Print out the whole sequence
........................................
Command::NoOp
Command::BeginMissionSequence
Command::RunSimulator
Command::RunEstimator
.................... End sequence
........................................................
Running mission...
Successfully set Planetary Source to use: DE405
Successfully set Planetary Source to use: DE421
Kernel ../data/planetary_coeff/SPICEEarthPredictedKernel.bpc has been
loaded.
Kernel ../data/planetary_coeff/SPICEEarthCurrentKernel.bpc has been
loaded.
Kernel ../data/planetary_coeff/earth_latest_high_prec.bpc has been loaded.
Kernel ../data/planetary_coeff/SPICELunaCurrentKernel.bpc has been loaded.
Kernel ../data/planetary_coeff/SPICELunaFrameKernel.tf has been loaded.
Warning: SPICE does not handle GmatTime. Value of GmatTime was convert
to GmatEpoch.
Warning: The orbit state transition matrix does not currently contain
SRP contributions from shadow partial derivatives when using Spherical
SRP.
Warning: The orbit state transition matrix does not currently contain
SRP contributions from shadow partial derivatives when using Spherical
SRP.
Warning: The orbit state transition matrix does not currently contain
SRP contributions from shadow partial derivatives when using Spherical
SRP.
Warning: The orbit state transition matrix does not currently contain
SRP contributions from shadow partial derivatives when using Spherical
SRP.
*** WARNING *** The light time calculation for celestial body
occultation failed to converge in 10 iterations. The convergance
tolerance is 1e-06, while the difference on the last iteration was
6.59375e-06
Number of thrown records due to:
.Invalid measurement value : 0
.Record duplication or time order : 0
Data file 'Simulator_AsteroidOccultation.gmd' has 4042 of 4042 records
used for estimation.
Total number of load records : 4042
List of tracking configurations (present in participant ID) for load
records from data file 'Simulator_AsteroidOccultation.gmd':
Config 0: {{MAD,SimSat01,MAD},Range}
**** No tracking configuration was generated because the tracking
configuration is defined in the script.
********************************************************
*** Performing Estimation (using "bat")
***
********************************************************
a priori state:
Estimation Epoch:
23645.0628707683063112199307 A.1 modified Julian
23645.0628703703699686273382 TAI modified Julian
01 Oct 2005 13:30:00.000 UTCG
EstSat.CeresJ2000Eq.X = 492.183000028
EstSat.CeresJ2000Eq.Y = 193.063000023
EstSat.CeresJ2000Eq.Z = -0.000177413225174
EstSat.CeresJ2000Eq.VX = -0.0763443
EstSat.CeresJ2000Eq.VY = 0.194628
EstSat.CeresJ2000Eq.VZ = 0.279831
Warning: The orbit state transition matrix does not currently contain
SRP contributions from shadow partial derivatives when using Spherical
SRP.
Warning: The orbit state transition matrix does not currently contain
SRP contributions from shadow partial derivatives when using Spherical
SRP.
Number of Records Removed Due To:
. No Computed Value Configuration Available : 0
. Out of Ramp Table Range : 0
. Signal Blocked : 0
. Initial RMS Sigma Filter : 0
. Outer-Loop Sigma Editor : 0
Number of records used for estimation: 4042
WeightedRMS residuals for this iteration : 6.25469030993e-06
BestRMS residuals : 6.25469030993e-06
PredictedRMS residuals for next iteration: 6.22971959808e-06
This iteration is converged due to absolute tolerance convergence
criteria.
********************************************************
*** Estimation Completed in 1 iterations
********************************************************
Estimation converged!
WeightedRMS residual, 6.25469e-06 is within the AbsoluteTol, 0.0001
Final Estimated State:
Estimation Epoch:
23645.0628707683063112199307 A.1 modified Julian
23645.0628703703699686273382 TAI modified Julian
01 Oct 2005 13:30:00.000 UTCG
EstSat.CeresJ2000Eq.X = 492.182995439
EstSat.CeresJ2000Eq.Y = 193.0630337
EstSat.CeresJ2000Eq.Z = -0.00012269616127
EstSat.CeresJ2000Eq.VX = -0.0763443393244
EstSat.CeresJ2000Eq.VY = 0.194627985815
EstSat.CeresJ2000Eq.VZ = 0.279830994061
Final Covariance Matrix:
4.466268910905e+00 -2.773335462989e+01
-3.661585786628e+01 2.745915872115e-02
1.207084525386e-02 2.906386708043e-03
-2.773332378691e+01 1.730073877868e+02
2.299141211050e+02 -1.721770478761e-01
-7.522474733979e-02 -1.849402311030e-02
-3.661575991467e+01 2.299137657609e+02
3.083863509294e+02 -2.304809909941e-01
-9.982858884573e-02 -2.526050187224e-02
2.745909443750e-02 -1.721768383456e-01
-2.304810661806e-01 1.723311111240e-04
7.478129210580e-05 1.880693697187e-05
1.207083480840e-02 -7.522476583831e-02
-9.982876793656e-02 7.478140162165e-05
3.271559917776e-05 8.007028496097e-06
2.906369473022e-03 -1.849393616241e-02
-2.526042430766e-02 1.880687283841e-05
8.006988712865e-06 2.142204617678e-06
Final Correlation Matrix:
1.000000000000 -0.997694657416
-0.986618388436 0.989766953197 0.998591371146
0.939616185263
-0.997693547854 1.000000000000
0.995372751264 -0.997151366353 -0.999887119762
-0.960657540489
-0.986615749118 0.995371212864
1.000000000000 -0.999782877064 -0.993870771377
-0.982797233271
0.989764636089 -0.997150152872
-0.999783203209 1.000000000000 0.995941160529
0.978826569526
0.998590507019 -0.999887365644
-0.993872554365 0.995942619066 1.000000000000
0.956452615692
0.939610613291 -0.960653024049
-0.982794215506 0.978823231633 0.956447863520
1.000000000000
********************************************************
Mission run completed.
===> Total Run Time: 979.699 seconds
========================================
*** GMAT Integration test (Console version) successful! ***
- DJC
On 12/16/19 11:30 AM, Darrel Conway wrote:
I have it running now. I suspect it's just timing out; that script
takes a long time to run (at least on Linux). It is not (so far)
crashing, and ran to completion on Ubuntu (just finished):
Interpreting scripts from the file.
***** file:
/home/djc/jazz/test/script/input/Resources/FRR-24_MeasurementSimulator/scripts/Simulator_AsteroidOccultation.script
**** WARNING **** RungeKutta4 is an integrator with no error
control. The accuracy setting will be ignored.
*** WARNING *** "BatchEstimatorInv" resource is deprecated and
will be removed from a future build; please use "BatchEstimator"
instead.
Setting value for bat.EstimationEpoch has no effect due to
bat.EstimationEpochFormat to be "FromParticipants"
Successfully interpreted the script
Running mission...
Warning: SPICE does not handle GmatTime. Value of GmatTime was
convert to GmatEpoch.
Warning: The orbit state transition matrix does not currently
contain SRP contributions from shadow partial derivatives when
using Spherical SRP.
Warning: The orbit state transition matrix does not currently
contain SRP contributions from shadow partial derivatives when
using Spherical SRP.
Warning: The orbit state transition matrix does not currently
contain SRP contributions from shadow partial derivatives when
using Spherical SRP.
Warning: The orbit state transition matrix does not currently
contain SRP contributions from shadow partial derivatives when
using Spherical SRP.
*** WARNING *** The light time calculation for celestial body
occultation failed to converge in 10 iterations. The convergance
tolerance is 1e-06, while the difference on the last iteration was
6.58322e-06
Number of thrown records due to:
.Invalid measurement value : 0
.Record duplication or time order : 0
Data file 'Simulator_AsteroidOccultation.gmd' has 4042 of 4042
records used for estimation.
Total number of load records : 4042
List of tracking configurations (present in participant ID) for
load records from data file 'Simulator_AsteroidOccultation.gmd':
Config 0: {{MAD,SimSat01,MAD},Range}
**** No tracking configuration was generated because the
tracking configuration is defined in the script.
********************************************************
*** Performing Estimation (using "bat")
***
********************************************************
a priori state:
Estimation Epoch:
23645.0628707683063112199307 A.1 modified Julian
23645.0628703703699686273382 TAI modified Julian
01 Oct 2005 13:30:00.000 UTCG
EstSat.CeresJ2000Eq.X = 492.183000028
EstSat.CeresJ2000Eq.Y = 193.063000023
EstSat.CeresJ2000Eq.Z = -0.000177413225174
EstSat.CeresJ2000Eq.VX = -0.0763443
EstSat.CeresJ2000Eq.VY = 0.194628
EstSat.CeresJ2000Eq.VZ = 0.279831
Warning: The orbit state transition matrix does not currently
contain SRP contributions from shadow partial derivatives when
using Spherical SRP.
Warning: The orbit state transition matrix does not currently
contain SRP contributions from shadow partial derivatives when
using Spherical SRP.
Number of Records Removed Due To:
. No Computed Value Configuration Available : 0
. Out of Ramp Table Range : 0
. Signal Blocked : 0
. Initial RMS Sigma Filter : 0
. Outer-Loop Sigma Editor : 0
Number of records used for estimation: 4042
WeightedRMS residuals for this iteration : 6.40187963176e-06
BestRMS residuals : 6.40187963176e-06
PredictedRMS residuals for next iteration: 6.39003216836e-06
This iteration is converged due to absolute tolerance convergence
criteria.
********************************************************
*** Estimation Completed in 1 iterations
********************************************************
Estimation converged!
WeightedRMS residual, 6.40188e-06 is within the AbsoluteTol,
0.0001
Final Estimated State:
Estimation Epoch:
23645.0628707683063112199307 A.1 modified Julian
23645.0628703703699686273382 TAI modified Julian
01 Oct 2005 13:30:00.000 UTCG
EstSat.CeresJ2000Eq.X = 492.183015615
EstSat.CeresJ2000Eq.Y = 193.062908709
EstSat.CeresJ2000Eq.Z = -0.000287115573883
EstSat.CeresJ2000Eq.VX = -0.0763442159135
EstSat.CeresJ2000Eq.VY = 0.194628040216
EstSat.CeresJ2000Eq.VZ = 0.279831007047
Final Covariance Matrix:
4.304681617005e+00 -2.672503914278e+01
-3.527528514518e+01 2.645533677847e-02
1.163244859849e-02 2.798463149644e-03
-2.672502504820e+01 1.667157471723e+02
2.215496732115e+02 -1.659136787531e-01
-7.248924014957e-02 -1.782070247444e-02
-3.527523995008e+01 2.215495081208e+02
2.972671983211e+02 -2.221547559176e-01
-9.619190270153e-02 -2.436555342717e-02
2.645530719001e-02 -1.659135816769e-01
-2.221547912087e-01 1.660962557593e-04
7.205810382333e-05 1.813675983057e-05
1.163244380277e-02 -7.248924846328e-02
-9.619198553260e-02 7.205815430662e-05
3.152624077562e-05 7.714269049678e-06
2.798455235946e-03 -1.782066250591e-02
-2.436551795937e-02 1.813673043091e-05
7.714250782348e-06 2.070195591927e-06
Final Correlation Matrix:
1.000000000000 -0.997607075171
-0.986112627634 0.989379381388 0.998537846869
0.937439793226
-0.997606549040 1.000000000000
0.995197570634 -0.997043163814 -0.999882901484
-0.959247813999
-0.986111364215 0.995196829048
1.000000000000 -0.999774829955 -0.993639679870
-0.982193589795
0.989378274835 -0.997042580443
-0.999774988778 1.000000000000 0.995787830382
0.978079352821
0.998537435201 -0.999883016159
-0.993640535495 0.995788528022 1.000000000000
0.954889236143
0.937437142266 -0.959245662584
-0.982192160061 0.978077767356 0.954886974972
1.000000000000
********************************************************
Mission run completed.
===> Total Run Time: 420.274 seconds
========================================
BTW, Can we please fix the spelling in the warning message?
*** WARNING *** The light time calculation for celestial body
occultation failed to converge in 10 iterations. The *convergance*
tolerance is 1e-06, while the difference on the last iteration was
6.59375e-06
- DJC
On 12/16/19 9:32 AM, Cooley, D S. (GSFC-5950) wrote:
Thanks for doing the Linux run Darrel. Do you have any insight into
the Linux crash SES mentions below?
*From:* Slojkowski, Steven E. (GSFC-595.0)[OMITRON]
<[email protected]>
*Sent:* Monday, December 16, 2019 10:16 AM
*To:* [email protected]; Cooley, D S. (GSFC-5950)
<[email protected]>; Nguyen, Tuan D. (GSFC-5830)
<[email protected]>; [email protected]
*Subject:* RE: [EXTERNAL] [Gmat-buildtest] Results: Linux Regression
Test requested
Simulator_AsteroidOccultation is appearing as a crash/hang on Linux
and passing on Win.
*From:* Darrel Conway <[email protected]
<mailto:[email protected]>>
*Sent:* Monday, December 16, 2019 10:01 AM
*To:* Cooley, D S. (GSFC-5950) <[email protected]
<mailto:[email protected]>>; Nguyen, Tuan D. (GSFC-5830)
<[email protected] <mailto:[email protected]>>;
[email protected]
<mailto:[email protected]>
*Subject:* [EXTERNAL] [Gmat-buildtest] Results: Linux Regression Test
requested
Attached for Red Hat and Ubuntu. *These are runs on the SRP_NPlates
branch*, commit a2aeba141f. (GSFC folks might see the code as commit
133ff0a29; there was a cmake fix required to build on Linux that I
might not have pushed yet.)
- DJC
On 12/13/19 1:34 PM, Cooley, D S. (GSFC-5950) wrote:
Darrel,
Would it be possible for you to kick off a full Linux regression
test run for Tuan’s SRP_Nplates git Branch. Probably best to
compile yourself as opposed to using Tuan’s build. (Tuan
doesn’t build everything)
steve
*From:* gmat-nav <[email protected]>
<mailto:[email protected]> *On Behalf Of *Nguyen,
Tuan D. (GSFC-5830) via gmat-nav
*Sent:* Friday, December 13, 2019 3:22 PM
*To:* GMAT Navigation Team <[email protected]>
<mailto:[email protected]>
*Subject:* [gmat-nav] A new SRP_NPlates branch GMAT build was
upload to mesa repo today.
A new SRP_NPlates branch GMAT build was upload to mesa repo today
in GMAT\Tuan\SRP_NPlates_12132019 folder.
The build contains:
1.The current merged code from master branch to SRP_NPlates branch
2.Fixed bug related to AreaCoefficient noise sigma
3.Fixed bug related to TSF_Epsilon noise sigma
Tuan
--
Darrel J. Conway, Ph.D. Thinking Systems, Inc.
Senior Scientist and CEO 437 W Thurber Road, Suite 6
Phone: (623) 298-4530 Tucson, AZ 85705
FAX: (520) 232-2533www.thinksysinc.com
<https://urldefense.proofpoint.com/v2/url?u=http-3A__www.thinksysinc.com&d=DwMD-g&c=ApwzowJNAKKw3xye91w7BE1XMRKi2LN9kiMk5Csz9Zk&r=HkPRNsvBaUz0R48WFhbgYAtIy_j-oGtHWpdZNpH75TFG7vNTC5O9xUvdr7kESTU-&m=ST5Aac_0GHWa9NtycgEnuodmBLgX_F_CTGMlWti_Ns0&s=3lXV6vNCKMC_aKlFeQS5tpsmG9eWjdY5hwWkamiwh1k&e=>
Cell: (520) [email protected]
<mailto:[email protected]>
--
Darrel J. Conway, Ph.D. Thinking Systems, Inc.
Senior Scientist and CEO 437 W Thurber Road, Suite 6
Phone: (623) 298-4530 Tucson, AZ 85705
FAX: (520) 232-2533www.thinksysinc.com
Cell: (520) [email protected]
--
Darrel J. Conway, Ph.D. Thinking Systems, Inc.
Senior Scientist and CEO 437 W Thurber Road, Suite 6
Phone: (623) 298-4530 Tucson, AZ 85705
FAX: (520) 232-2533 www.thinksysinc.com
Cell: (520) 425-3626 [email protected]
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