[Isocops] IBEX Orbit# 183 ATS v001 (Hi/CEU) and v001 (Lo) - approve

Mark Tapley mtapley at swri.edu
Thu Oct 4 13:41:37 EDT 2012


All,
	I have looked at the Orbit 183 ATS v001 (No -Lo commands)

IBEX_2012_289_o0183a_v001.txt

	and the corresponding -Lo command ATS v001

IBEX_2012_289_o0183a_Lo_Commands_v001.txt

and I approve.

	No constraint violations per .ccvr file:

IBEX_2012_289_o0183a_v001.ccvr

	-Lo-only load .ccvr

IBEX_2012_289_o0183a_Lo_Commands_v001.ccvr

	has the expected violations due to lack of -Hi and CEU 
commands in the -Lo alone load.

	The PL commands in the ATS v001 match the STF v002

IBEX_2012_289_o0183a_v002.stf

	and the -Lo commands in the -Lo ATS v001 match the -Lo STF v001

IBEX_2012_289_o0183a_LoCommanding_v001.stf

per Ken's script (thanks!).

	PL ascending and descending operations (-Hi/CEU and -Lo) make 
sense with respect each other and to 15 Re ascending, Apogee, and 15 
Re descending times from

IBEX_2012_289_o0183a_v001.oef

	Star tracker outage late in perigee starts 7 hours after 
perigee maneuver. No consequence from outage.

	Moon in -LO FOV for 14 hours during descending arc. -Lo 
commands this load include PMT set-back similar to times in .oef, 
late by 1 hour at start and 1.5 hours at end.

	No ground station contact commands in either load, to save 
command space. Contacts file shows contacts at reasonable times, not 
during battery cell balancing or maneuver.

	Battery cell balancing this orbit. Did last orbit, should 
skip next orbit.

	Inertial maneuver at the end of orbit 182 left us pointing in 
a safe direction for ascending and descending macros during first 
half of orbit:

[tapley at ena ~]$ ibex_rotate -o -u -0.936985,-0.315276,-0.150536 -w 
ibex-sun -t 2012/10:16:11:53:10
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  -0.936985,-0.315276,-0.150536
  which is     R.A. +198.597 Decl.  -8.658
  missing      R.A. +201.582 Decl.  -9.057 (ibex-sun)
  error is     R.A.   +2.985 Decl.  +0.400
  for a total  2.976 deg
[tapley at ena ~]$ ibex_rotate -o -u -0.936985,-0.315276,-0.150536 -w 
ibex-sun -t 2012/10:19:23:25:49
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  -0.936985,-0.315276,-0.150536
  which is     R.A. +198.597 Decl.  -8.658
  missing      R.A. +204.765 Decl. -10.327 (ibex-sun)
  error is     R.A.   +6.168 Decl.  +1.669
  for a total  6.308 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 -0.907621,-0.380001,-0.17839 -w 
ibex-sun -t 2012/10:20:01:09:37
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  -0.907621,-0.380001,-0.178390
  which is     R.A. +202.718 Decl. -10.276
  missing      R.A. +204.834 Decl. -10.353 (ibex-sun)
  error is     R.A.   +2.116 Decl.  +0.077
  for a total  2.083 deg
[tapley at ena ~]$ ibex_rotate -o -u -0.907621,-0.380001,-0.17839 -w 
ibex-sun -t 2012/10:20:02:44:43
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  -0.907621,-0.380001,-0.178390
  which is     R.A. +202.718 Decl. -10.276
  missing      R.A. +204.896 Decl. -10.377 (ibex-sun)
  error is     R.A.   +2.178 Decl.  +0.101
  for a total  2.145 deg
[tapley at ena ~]$ ibex_rotate -o -u -0.907621,-0.380001,-0.17839 -w 
ibex-sun -t 2012/10:24:10:05:32
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  -0.907621,-0.380001,-0.178390
  which is     R.A. +202.718 Decl. -10.276
  missing      R.A. +209.101 Decl. -11.910 (ibex-sun)
  error is     R.A.   +6.383 Decl.  +1.634
  for a total  6.473 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 -0.872179,-0.443611,-0.206187 -w 
ibex-sun -t 2012/10:24:17:26:05
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  -0.872179,-0.443611,-0.206187
  which is     R.A. +206.959 Decl. -11.899
  missing      R.A. +209.402 Decl. -12.011 (ibex-sun)
  error is     R.A.   +2.443 Decl.  +0.113
  for a total  2.393 deg
[tapley at ena ~]$ ibex_rotate -o -u -0.872179,-0.443611,-0.206187 -w 
ibex-sun -t 2012-10-29T08:25:37.426Z
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  -0.872179,-0.443611,-0.206187
  which is     R.A. +206.959 Decl. -11.899
  missing      R.A. +213.718 Decl. -13.566 (ibex-sun)
  error is     R.A.   +6.759 Decl.  +1.667
  for a total  6.800 deg

	No -Lo O-mode Commands.

	No overlap to orbit 182 commands apparent by manual check; 
http://ibex.unh.edu/cgi-bin/ats.cgi has a lot of commands interleaved 
among various loads and is not usable for confirming no-overlap right 
now.

	Command Approval Checklists attached.

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


At 11:54 -0400 10/3/12, Ibex Mission Operations wrote:
>Guys,
>    Here are the planning files and ATS  for Orbit# 183.
>Please respond to this email thread with comments/approvals.
>All approvals and comments are required before 5 Oct 12 @1800 UTC
>
>1. No contact commands within the ATS.  All contacts are blind_acqs
>2. Battery Balancing during PERIGEE
>3. Command Violations

At 12:17 -0400 10/3/12, Ibex Mission Operations wrote:
>Guys,
>Here are the planning files and ATS for Orbit# 183 IBEX_Lo Commands
>All approvals/commands are required before 19 Oct 12 @1800 UTC
>
>Please note the following:
>1. All Soft Constraint Violations are generated because only IBEX_Lo 
>commands were used to generate the ATS
>2. Orbit# 183 ATS contains BUS, IBEX_Hi and Inertial Maneuver Commands
>3. Command Load Violations

-- 
						- 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.
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