[Isocops] TEST ONLY: IBEX Orbit# 199 ATS v001 - approve
Mark Tapley
mtapley at swri.edu
Mon Jan 14 18:16:42 EST 2013
All,
I have looked at the TEST ONLY Orbit 199 ATS v001
IBEX_2013_069_o0199a_TEST_v001.txt
and I approve.
No constraint violation per .ccvr file:
IBEX_2013_069_o0199a_TEST_v001.ccvr
The PL commands in the ATS v001 file match those in the STF
IBEX_2013_068_o0199a_test_v001.stf
according to Ken's script (thanks!).
PL ascending and descending operations make sense with
respect to each other and to 14 and 15 Re ascending, Apogee, and 15
Re descending times from
IBEX_2011_069_o199a_TEST_v001_.oef
Star tracker outage for 2 days and 21 hours of second arc
science operations; may require de-spinning but occurs after inertial
maneuver at apogee is complete.
Moon in -LO FOV two periods during descending arc; ATS
commands are 1.5 hours late start and 7 hours late end compared to
.oef start and end times for a 45 hour Moon in FOV period, and then 4
hours late start and on time end for an 11 hour Moon-in-FOV period.
These are about normal.
No Ground station contact commands nor Contacts file.
No Battery cell balancing this orbit; should have done either
this or last orbit, but not important for TEST files.
Inertial maneuver at the end of orbit 198 leaves us pointing
in a safe direction at Ascending and Descending macros on first arc.
[tapley at ena ~]$ ibex_rotate -o -u 0.973643,-0.205055,-0.099858 -w
ibex-sun -t 2013/03:10:08:10:18
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.973643,-0.205055,-0.099858
which is R.A. +348.107 Decl. -5.731
missing R.A. +350.599 Decl. -4.050 (ibex-sun)
error is R.A. +2.492 Decl. +1.681
for a total 2.998 deg
[tapley at ena ~]$ ibex_rotate -o -u 0.973643,-0.205055,-0.099858 -w
ibex-sun -t 2013/03:13:23:41:42
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.973643,-0.205055,-0.099858
which is R.A. +348.107 Decl. -5.731
missing R.A. +353.983 Decl. -2.638 (ibex-sun)
error is R.A. +5.876 Decl. +3.093
for a total 6.626 deg
Inertial maneuver at apogee leaves us pointing in a safe
direction at maneuver and at following Ascending and Descending
Macros.
[tapley at ena ~]$ ibex_rotate -o -u 0.989057,-0.131072,-0.067719 -w
ibex-sun -t 2013/03:14:01:24:50
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.989057,-0.131072,-0.067719
which is R.A. +352.451 Decl. -3.883
missing R.A. +354.048 Decl. -2.610 (ibex-sun)
error is R.A. +1.597 Decl. +1.273
for a total 2.040 deg
[tapley at ena ~]$ ibex_rotate -o -u 0.989057,-0.131072,-0.067719 -w
ibex-sun -t 2013/03:14:02:59:56
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.989057,-0.131072,-0.067719
which is R.A. +352.451 Decl. -3.883
missing R.A. +354.108 Decl. -2.585 (ibex-sun)
error is R.A. +1.657 Decl. +1.298
for a total 2.103 deg
[tapley at ena ~]$ ibex_rotate -o -u 0.989057,-0.131072,-0.067719 -w
ibex-sun -t 2013/03:18:15:14:01
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.989057,-0.131072,-0.067719
which is R.A. +352.451 Decl. -3.883
missing R.A. +358.136 Decl. -0.808 (ibex-sun)
error is R.A. +5.685 Decl. +3.075
for a total 6.459 deg
Inertial maneuver at perigee leaves us pointing in a safe
direction at maneuver and at following Apogee.
[tapley at ena ~]$ ibex_rotate -o -u 0.997648,-0.058205,-0.03619 -w
ibex-sun -t 2013/03:18:17:19:48
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.997648,-0.058205,-0.036190
which is R.A. +356.661 Decl. -2.074
missing R.A. +358.216 Decl. -0.771 (ibex-sun)
error is R.A. +1.555 Decl. +1.303
for a total 2.028 deg
[tapley at ena ~]$ ibex_rotate -o -u 0.997648,-0.058205,-0.03619 -w
ibex-sun -t 2013-03-23T20:29:02.023Z
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.997648,-0.058205,-0.036190
which is R.A. +356.661 Decl. -2.074
missing R.A. +2.997 Decl. +1.261 (ibex-sun)
error is R.A. +353.664 Decl. +3.335
for a total 7.160 deg
No -Lo O-mode Commands.
No overlap to any previous commands apparent by manual check;
http://ibex.unh.edu/cgi-bin/ats.cgi has not yet ingested the o198 or
o199 test loads.
Command Approval Checklist attached.
-Hi Neg collimator back to operating at nominal voltage.
Pointing for -Lo ISM mode operations during January complete,
so sun angles are back to normal.
At 22:57 -0500 1/12/13, Tim Perry wrote:
>All,
> Attached are the products for Orbit 199. And again these products were
>generated using the 14 - 14 re times.
> Enjoy
> Tim
--
- Mark 210-379-4635
-----------------------------------------------------------------------
Large Asteroids headed toward planets
inhabited by beings that don't have
technology adequate to stop them:
Think of it as Evolution in Fast-Forward.
-------------- next part --------------
A non-text attachment was scrubbed...
Name: IBEX-CAC_Rev11_TEST_0199_MT.doc
Type: application/msword
Size: 96256 bytes
Desc: not available
Url : http://lists.sr.unh.edu/mailman/private/isocops/attachments/20130114/eb9f1606/IBEX-CAC_Rev11_TEST_0199_MT-0001.doc
More information about the Isocops
mailing list