[Isocops] IBEX Orbit# 198 ATS v001 - approve

[Mark Tapley]

All,
	I have looked at the Orbit 198 ATS v001

IBEX_2013_059_o0198a_v001.txt

	and I approve.

	No constraint violation per .ccvr file:

IBEX_2013_059_o0198a_v001.ccvr

	The PL commands in the ATS v001 file match those in the STF v001

IBEX_2013_059_o0198a_v001.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, and 15 Re 
descending times from

IBEX_2013_059_o0198a_v001.oef

	Star tracker outage for 3 days and 7 hours starts after 
inertial maneuver.

	Moon in -LO FOV periods during second arc; ATS commands 45 
minutes early start and 4 hours early end for a 17 hour period, about 
normal.

	Ground station contact commands match contact times and bit 
rates in Contacts file

IBEX_Orbit198Contacts.txt

	for all 3 contacts.

	Battery cell balancing this orbit, as is appropriate. Should 
skip next orbit. Commands are more than 1 hour from anything, 1.5 
hours apart, and second command is false, all appropriate.

	Inertial maneuver at the end of orbit 197 left us pointing in 
extra safe directions for ascending and descending macros during 
first half of orbit:

[tapley at ena ~]$ ibex_rotate -o -u 0.943307,-0.300594,-0.140763 -w 
ibex-sun -t 2013/03:01:02:20:53
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  +0.943307,-0.300594,-0.140763
  which is     R.A. +342.325 Decl.  -8.092
  missing      R.A. +342.016 Decl.  -7.623 (ibex-sun)
  error is     R.A.   +0.309 Decl.  +0.469
  for a total  0.560 deg
[tapley at ena ~]$ ibex_rotate -o -u 0.943307,-0.300594,-0.140763 -w 
ibex-sun -t 2013/03:04:09:40:04
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  +0.943307,-0.300594,-0.140763
  which is     R.A. +342.325 Decl.  -8.092
  missing      R.A. +345.123 Decl.  -6.386 (ibex-sun)
  error is     R.A.   +2.798 Decl.  +1.706
  for a total  3.258 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 0.960031,-0.252594,-0.12057 -w 
ibex-sun -t 2013/03:04:11:23:12
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  +0.960031,-0.252594,-0.120570
  which is     R.A. +345.259 Decl.  -6.925
  missing      R.A. +345.189 Decl.  -6.359 (ibex-sun)
  error is     R.A.   +0.070 Decl.  +0.566
  for a total  0.570 deg
[tapley at ena ~]$ ibex_rotate -o -u 0.960031,-0.252594,-0.12057 -w 
ibex-sun -t 2013/03:04:12:58:18
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  +0.960031,-0.252594,-0.120570
  which is     R.A. +345.259 Decl.  -6.925
  missing      R.A. +345.249 Decl.  -6.334 (ibex-sun)
  error is     R.A.   +0.010 Decl.  +0.591
  for a total  0.591 deg
[tapley at ena ~]$ ibex_rotate -o -u 0.960031,-0.252594,-0.12057 -w 
ibex-sun -t 2013/03:09:08:24:15
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  +0.960031,-0.252594,-0.120570
  which is     R.A. +345.259 Decl.  -6.925
  missing      R.A. +349.618 Decl.  -4.468 (ibex-sun)
  error is     R.A.   +4.359 Decl.  +2.457
  for a total  4.985 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 0.973645,-0.205037,-0.099875 -w 
ibex-sun -t 2013/03:09:10:26:28
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  +0.973645,-0.205037,-0.099875
  which is     R.A. +348.108 Decl.  -5.732
  missing      R.A. +349.698 Decl.  -4.432 (ibex-sun)
  error is     R.A.   +1.590 Decl.  +1.300
  for a total  2.048 deg
[tapley at ena ~]$ ibex_rotate -o -u 0.973645,-0.205037,-0.099875 -w 
ibex-sun -t 2013-03-14T11:15:37.939Z
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  +0.973645,-0.205037,-0.099875
  which is     R.A. +348.108 Decl.  -5.732
  missing      R.A. +354.418 Decl.  -2.451 (ibex-sun)
  error is     R.A.   +6.310 Decl.  +3.281
  for a total  7.097 deg

	No -Lo O-mode Commands.

	No overlap to orbit 197 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.

	Pointing was in -Lo ISM mode operations during January and 
returning to nominal.


At 11:31 -0500 2/15/13, Ibex Mission Operations wrote:
>Guys,
>     Here are the planning files and ATS for Orbit# 198.
>Please respond to this email thread with all approvals and comments
>Approvals/comments are required before 18 Feb 13 @1800 UTC

-- 
						- 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_Rev10a_o198_MT.doc
Type: application/msword
Size: 87040 bytes
Desc: not available
Url : http://lists.sr.unh.edu/mailman/private/isocops/attachments/20130215/ec764680/IBEX-CAC_Rev10a_o198_MT-0001.doc