[Isocops] IBEX Orbit# 189 ATS v002 and -Hi threshold test - approve

Mon Nov 26 13:38:58 EST 2012

All,
	I have looked at the Orbit 189 ATS v002

IBEX_2012_343_o0189a_v002.txt

	and I approve.

	One constraint violation per .ccvr file:

IBEX_2012_343_o0189a_v001.ccvr

	low battery state caused by eclipse, as expected.

	The PL commands in the ATS v002 file match those in the STF

IBEX_2012_343_o0189a_v001.stf

	and those in the -Hi threshold test match the -Hi threshold STF

IBEX_2012_343_o0189a_v001_htd.stf

	according to Ken's script (thanks!).

	PL ascending and descending operations make sense with 
respect to each other and to 15 Re ascending, Apogee, eclipse, and 15 
Re descending times from

IBEX_2012_343_o0189a_v001.oef

	Star tracker outage for first 19 hours of first arc ascending 
science operations and SSR dump pass; should not affect ramp-up but 
may require de-spinning.

	Eclipse operations near perigee, after descending for second arc.

	No Moon in -LO FOV.

	Ground station contact commands match contact times in Contacts file

IBEX_2012_Orbit189_v002.caf

	for all 3 contacts. No contacts during eclipse. Post Eclipse 
pass  begins 2 hours after eclipse ends.

	Battery cell balancing unavoidable due to eclipse operations. 
FALSE command is the second command, as appropriate.

	Inertial maneuver at the end of orbit 188 left us pointing in 
a safe direction for ascending and descending macros during first 
half of orbit:

[tapley at ena ~]$ ibex_rotate -o -u -0.273567,-0.87735,-0.394231 -w 
ibex-sun -t 2012/12:09:00:41:10
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  -0.273567,-0.877350,-0.394231
  which is     R.A. +252.682 Decl. -23.218
  missing      R.A. +256.066 Decl. -22.817 (ibex-sun)
  error is     R.A.   +3.384 Decl.  +0.401
  for a total  3.140 deg
[tapley at ena ~]$ ibex_rotate -o -u -0.273567,-0.87735,-0.394231 -w 
ibex-sun -t 2012/12:12:11:31:21
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  -0.273567,-0.877350,-0.394231
  which is     R.A. +252.682 Decl. -23.218
  missing      R.A. +259.743 Decl. -23.135 (ibex-sun)
  error is     R.A.   +7.061 Decl.  +0.083
  for a total  6.491 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 -0.196438,-0.894566,-0.401452 -w 
ibex-sun -t 2012/12:12:13:14:29
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  -0.196438,-0.894566,-0.401452
  which is     R.A. +257.615 Decl. -23.669
  missing      R.A. +259.821 Decl. -23.140 (ibex-sun)
  error is     R.A.   +2.206 Decl.  +0.529
  for a total  2.093 deg
[tapley at ena ~]$ ibex_rotate -o -u -0.196438,-0.894566,-0.401452 -w 
ibex-sun -t 2012/12:12:14:49:35
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  -0.196438,-0.894566,-0.401452
  which is     R.A. +257.615 Decl. -23.669
  missing      R.A. +259.893 Decl. -23.145 (ibex-sun)
  error is     R.A.   +2.278 Decl.  +0.524
  for a total  2.155 deg
[tapley at ena ~]$ ibex_rotate -o -u -0.196438,-0.894566,-0.401452 -w 
ibex-sun -t 2012/12:16:21:04:31
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  -0.196438,-0.894566,-0.401452
  which is     R.A. +257.615 Decl. -23.669
  missing      R.A. +264.693 Decl. -23.352 (ibex-sun)
  error is     R.A.   +7.078 Decl.  +0.317
  for a total  6.497 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 -0.119854,-0.905742,-0.406529 -w 
ibex-sun -t 2012/12:17:08:01:00
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  -0.119854,-0.905742,-0.406529
  which is     R.A. +262.462 Decl. -23.987
  missing      R.A. +265.238 Decl. -23.359 (ibex-sun)
  error is     R.A.   +2.776 Decl.  +0.628
  for a total  2.619 deg
[tapley at ena ~]$ ibex_rotate -o -u -0.119854,-0.905742,-0.406529 -w 
ibex-sun -t 2012-12-21T20:11:25.903Z
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  -0.119854,-0.905742,-0.406529
  which is     R.A. +262.462 Decl. -23.987
  missing      R.A. +270.118 Decl. -23.471 (ibex-sun)
  error is     R.A.   +7.656 Decl.  +0.516
  for a total  7.026 deg

	No -Lo O-mode Commands.

	No overlap to orbit 188 commands apparent by manual check or 
by reference to http://ibex.unh.edu/cgi-bin/ats.cgi .

	Command Approval Checklist attached.

	-Hi Neg collimator back to operating at nominal voltage.

	-Hi threshold test during perigee Standby mode operation, as required.


At 18:23 -0500 11/25/12, Ibex Mission Operations wrote:
>All,
>    Attached is the Orbit 189 Hi threshold Test.
>      Enjoy
>          Tim

At 11:55 -0500 11/24/12, Tim Perry wrote:
>All,
>        I hope everyone had a wonderful Thanksgiving...
>Attached are the products for Orbit 189. And, Yes!!!  It's version 2 
>due to the edits in the command load.  I've incorporated a battery 
>balancing cycle in the command load post eclipse.
>Below are the details.
>Approvals/comments will be required before COB Nov 27
>Thanks
>         Tim :-)

-- 
						- Mark     210-379-4635
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