[Isocops] IBEX Orbit# 168 ATS v001 - approve

[Mark Tapley]

All,
	I have looked at the Orbit 168 ATS v001

IBEX_2012_152_o0168a_v001.txt

and I approve.

	No constraint violations per .ccvr file:

IBEX_2012_152_o0168a_v001.ccvr

	The PL commands in the ATS v001 match the STF v001

IBEX_2012_152_o0168a_v001.stf

per Ken's script (thanks!).

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

IBEX_2012_152_o0168a_v001.oef

	Star tracker outages on June 6-7 during second arc and 8-9 
during perigee descend do not affect maneuver windows.

	Ground station contact times and rates per

IBEX_Orbit168Contacts_v001.txt

match S/C commands for all 3 contacts.

	Battery cell balancing this orbit for 1.5 hours, ends with 
Flag FALSE (as appropriate), and is more than an hour from anything. 
Did this last orbit, should skip next orbit.

	Inertial maneuver at the end of orbit 167 left us pointing in 
a safe direction for ascending and descending macros during first 
half of orbit:

[tapley at ena ~]$ ibex_rotate -o -u 0.376763,0.854882,0.356689 -w 
ibex-sun -t 2012/05:31:19:12:13
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  +0.376763,+0.854882,+0.356689
  which is     R.A.  +66.216 Decl. +20.897
  missing      R.A.  +68.943 Decl. +22.033 (ibex-sun)
  error is     R.A.   +2.727 Decl.  +1.136
  for a total  2.781 deg
[tapley at ena ~]$ ibex_rotate -o -u 0.376763,0.854882,0.356689 -w 
ibex-sun -t 2012/06:04:07:44:28
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  +0.376763,+0.854882,+0.356689
  which is     R.A.  +66.216 Decl. +20.897
  missing      R.A.  +72.678 Decl. +22.453 (ibex-sun)
  error is     R.A.   +6.462 Decl.  +1.556
  for a total  6.203 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 0.306388,0.878245,0.367167 -w 
ibex-sun -t 2012/06:04:09:32:18
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  +0.306388,+0.878245,+0.367167
  which is     R.A.  +70.768 Decl. +21.541
  missing      R.A.  +72.756 Decl. +22.461 (ibex-sun)
  error is     R.A.   +1.988 Decl.  +0.920
  for a total  2.060 deg
[tapley at ena ~]$ ibex_rotate -o -u 0.306388,0.878245,0.367167 -w 
ibex-sun -t 2012/06:04:11:03:22
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  +0.306388,+0.878245,+0.367167
  which is     R.A.  +70.768 Decl. +21.541
  missing      R.A.  +72.821 Decl. +22.468 (ibex-sun)
  error is     R.A.   +2.053 Decl.  +0.927
  for a total  2.117 deg
[tapley at ena ~]$ ibex_rotate -o -u 0.306388,0.878245,0.367167 -w 
ibex-sun -t 2012/06:08:19:18:18
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  +0.306388,+0.878245,+0.367167
  which is     R.A.  +70.768 Decl. +21.541
  missing      R.A.  +77.197 Decl. +22.909 (ibex-sun)
  error is     R.A.   +6.429 Decl.  +1.368
  for a total  6.106 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 0.233612,0.897109,0.374995 -w 
ibex-sun -t 2012/06:09:03:21:30
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  +0.233612,+0.897109,+0.374995
  which is     R.A.  +75.404 Decl. +22.024
  missing      R.A.  +77.517 Decl. +22.944 (ibex-sun)
  error is     R.A.   +2.113 Decl.  +0.920
  for a total  2.158 deg
[tapley at ena ~]$ ibex_rotate -o -u 0.233612,0.897109,0.374995 -w 
ibex-sun -t 2012-06-13T20:16:10.318Z
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  +0.233612,+0.897109,+0.374995
  which is     R.A.  +75.404 Decl. +22.024
  missing      R.A.  +82.520 Decl. +23.228 (ibex-sun)
  error is     R.A.   +7.116 Decl.  +1.204
  for a total  6.677 deg

	No -Lo O-mode Commands.

	No overlap to orbit 167 commands apparent by manual check or 
by reference to http://ibex.unh.edu/cgi-bin/ats.cgi .

	Command Approval Checklist attached.

	-Hi Neg collimator voltage back to operating at nominal voltage.


At 13:53 -0400 5/17/12, Ibex Mission Operations wrote:
>Guys,
>     Here are the planning files and ATS for Orbit# 168.
>Please respond to this email thread with approvals/comments.
>All approvals/comments are due before 21 May 12 @ 0200 UTC
>
>NOTE the following:
>1. Battery Balancing commands
>2. 10 minute thruster enable time  

-- 
						- Mark     210-379-4635
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