[Isocops] IBEX Orbit# 185 ATS v001 (Hi/CEU) and v001 (Lo) - approve

Mark Tapley mtapley at swri.edu
Tue Oct 23 10:42:59 EDT 2012


All,
	I have looked at the Orbit 185 ATS v001

IBEX_2012_307_o0185a_v001.txt

	and at the provisional (in case the LUT table load is not 
carried out) No-Lo ATS v001

IBEX_2012_307_o0185a_NoLo_v001.txt

	and the corresponding -Lo command ATS v001

IBEX_2012_307_o0185a_Lo_Commands_v001.txt

and I approve.

	No constraint violations per .ccvr files:

IBEX_2012_307_o0185a_NoLo_v001.ccvr
IBEX_2012_307_o0185a_v001.ccvr

	-Lo-only load .ccvr

IBEX_2012_307_o0185a_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 all three ATS files match those in the STFs

IBEX_2012_307_o0185a_v001.stf
IBEX_2012_307_o0185a_NoLo_v001.stf
IBEX_2012_307_o0185a_Lo_Commands_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_307_o0185a_v001.oef

	Star tracker outage during perigee starts 9 hours after 
completion of inertial maneuver, no conflict.

	Moon in -LO FOV during ascending arc; set-back commands are 
10 hours after start of event; another Moon in -LO FOV during apogee 
ends ~3 hours after -Lo ramp-up; no set-back commands present in 
descending arc.

	No ground station contact commands in any load. Contacts file 
shows contacts at reasonable times, not during maneuvers.

	Battery cell balancing this orbit. Skipped last orbit, should 
do this orbit and next orbit. Commands are > 1 hour from anything, 
and FALSE follows TRUE by 1.5 hours as is appropriate.

	Inertial maneuver at the end of orbit 184 left us pointing in 
a safe direction for ascending and descending macros during first 
half of orbit:

[tapley at ena ~]$ ibex_rotate -o -u -0.786493,-0.561456,-0.257285 -w 
ibex-sun -t 2012/11:03:07:23:01
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  -0.786493,-0.561456,-0.257285
  which is     R.A. +215.522 Decl. -14.909
  missing      R.A. +218.663 Decl. -15.151 (ibex-sun)
  error is     R.A.   +3.141 Decl.  +0.242
  for a total  3.043 deg
[tapley at ena ~]$ ibex_rotate -o -u -0.786493,-0.561456,-0.257285 -w 
ibex-sun -t 2012/11:06:20:18:02
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  -0.786493,-0.561456,-0.257285
  which is     R.A. +215.522 Decl. -14.909
  missing      R.A. +222.066 Decl. -16.230 (ibex-sun)
  error is     R.A.   +6.544 Decl.  +1.321
  for a total  6.441 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 -0.735578,-0.616458,-0.280901  -w 
ibex-sun -t 2012/11:06:22:01:10
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  -0.735578,-0.616458,-0.280901
  which is     R.A. +219.965 Decl. -16.314
  missing      R.A. +222.138 Decl. -16.251 (ibex-sun)
  error is     R.A.   +2.173 Decl.  +0.063
  for a total  2.087 deg
[tapley at ena ~]$ ibex_rotate -o -u -0.735578,-0.616458,-0.280901  -w 
ibex-sun -t 2012/11:06:23:36:16
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  -0.735578,-0.616458,-0.280901
  which is     R.A. +219.965 Decl. -16.314
  missing      R.A. +222.204 Decl. -16.271 (ibex-sun)
  error is     R.A.   +2.239 Decl.  +0.043
  for a total  2.149 deg
[tapley at ena ~]$ ibex_rotate -o -u -0.735578,-0.616458,-0.280901  -w 
ibex-sun -t 2012/11:11:08:26:42
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  -0.735578,-0.616458,-0.280901
  which is     R.A. +219.965 Decl. -16.314
  missing      R.A. +226.729 Decl. -17.522 (ibex-sun)
  error is     R.A.   +6.764 Decl.  +1.208
  for a total  6.583 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 -0.679541,-0.667946,-0.303434 -w 
ibex-sun -t 2012/11:11:16:07:47
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  -0.679541,-0.667946,-0.303434
  which is     R.A. +224.507 Decl. -17.664
  missing      R.A. +227.071 Decl. -17.607 (ibex-sun)
  error is     R.A.   +2.564 Decl.  +0.057
  for a total  2.444 deg
[tapley at ena ~]$ ibex_rotate -o -u -0.679541,-0.667946,-0.303434 -w 
ibex-sun -t 2012-11-16T06:23:37.955Z
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  -0.679541,-0.667946,-0.303434
  which is     R.A. +224.507 Decl. -17.664
  missing      R.A. +231.631 Decl. -18.807 (ibex-sun)
  error is     R.A.   +7.124 Decl.  +1.143
  for a total  6.862 deg

	No -Lo O-mode Commands.

	No overlap to orbit 184 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 back to operating at nominal voltage.


At 13:48 -0400 10/22/12, Ibex Mission Operations wrote:
>Guys,
>   Here are the planning files for the various Orbit# 185 ATS command loads.
>Approvals are required before 25 Oct 12 @ 1800 UTC
>
>1.  IBEX_2012_307_o0185a_v001.scr
>- Nominal ATS commands with the new LUT settings
>- Contains BUS, IBEX_Hi and IBEX_Lo  Payload Commands
>- Contains battery cell balancing commands at Perigee
>- Does NOT contain contact commands
>- CCVR has no command violations
>
>
>2.  IBEX_2012_307_o0185a_NoLo_v001.scr
>- Contains IBEX-Hi Payload  and BUS Commands
>- Contains NO IBEX_Lo Payload Commands
>- Contains Inertial MAneuver Commands
>- Contains battery cell balancing commands at Perigee
>- Does NOT contain contact commands
>- CCVR has no command violations
>
>
>3.  IBEX_2012_307_o0185a_Lo_Commands_v001.scr
>- Contains IBEX_Lo Commands Only
>- Contains Moon in Lo FOV Commands
>- Inertial Maneuver commands are commented out
>- CCVR  violations are from using ONLY IBEX_Lo commands to generate the ATS

-- 
						- 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_o185_MT.doc
Type: application/msword
Size: 93184 bytes
Desc: not available
Url : http://lists.sr.unh.edu/mailman/private/isocops/attachments/20121023/e2499a28/IBEX-CAC_Rev10a_o185_MT-0001.doc 
-------------- next part --------------
A non-text attachment was scrubbed...
Name: IBEX-Lo-CAC-Rev9a_185_MT.doc
Type: application/msword
Size: 80384 bytes
Desc: not available
Url : http://lists.sr.unh.edu/mailman/private/isocops/attachments/20121023/e2499a28/IBEX-Lo-CAC-Rev9a_185_MT-0001.doc 


More information about the Isocops mailing list