[Isocops] V002 of the IBEX Orbit# 96 ATS (3 Oct - 12 Oct 10) - approve

[Mark Tapley]

All,
	I have looked at v002 of the Orbit 96 ATS, and I approve.

	Ken reports the ATS matches the STF, excepting some 
differences in new-line characters.

	Constraint violations with v001 (too-long contact time, 
corrected in v002) and PL state not known (happens a lot these days, 
I'm ignoring that) are acceptable.

	List of scheduled ground contacts not sent; I have not 
checked that the SC times match the ground times, except for the 
last, as described in the changed-contact email; that one does match.

	The maneuver points us in a safe direction at the time of the 
maneuver, and at the succeeding ascending and descending times:

[tapley at ena ~]$ ibex_rotate -o -u 
-0.9467415116417425,-0.29556684164603686,-0.12775269959454927 -w 
ibex-Sun -t 2010/10:11:09:03:33
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  -0.946742,-0.295567,-0.127753
  which is     R.A. +197.338 Decl.  -7.340
  missing      R.A. +196.412 Decl.  -7.000 (ibex-Sun)
  error is     R.A.   +0.926 Decl.  +0.340
  for a total  0.979 deg
[tapley at ena ~]$ ibex_rotate -o -u 
-0.9467415116417425,-0.29556684164603686,-0.12775269959454927 -w 
ibex-Sun -t 2010-10-12T00:47:53.752Z
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  -0.946742,-0.295567,-0.127753
  which is     R.A. +197.338 Decl.  -7.340
  missing      R.A. +196.993 Decl.  -7.201 (ibex-Sun)
  error is     R.A.   +0.345 Decl.  +0.139
  for a total  0.370 deg
[tapley at ena ~]$ ibex_rotate -o -u 
-0.9467415116417425,-0.29556684164603686,-0.12775269959454927 -w 
ibex-Sun -t 2010-10-18T19:57:07.741Z
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  -0.946742,-0.295567,-0.127753
  which is     R.A. +197.338 Decl.  -7.340
  missing      R.A. +203.321 Decl.  -9.759 (ibex-Sun)
  error is     R.A.   +5.983 Decl.  +2.420
  for a total  6.392 deg

	Battery cell balancing is an hour away from anything.

	More O-mode coming in Orbit 97.

At 19:06 -0400 9/24/10, Ibex Mission Operations wrote:
>Guys,
>    Here is V002 of the ATS for Orbit# 96.  I have shortened the 
>contact time listed below in UTC as per Chelle Reno
>
>#  Orbit# 96 Tracking Contact 
>   @ECT_SetRelay stx,on $TIME=2010/10:12:01:58:00
>   @FMI_SetDownlink64K $TIME=2010/10:12:01:58:02
>   @FMI_SetBilevelOutputControlReg STXMODE_Strobe,ON $TIME=2010/10:12:01:58:04
>   @FMI_SetBilevelOutputControlReg COHERENT,ON $TIME=2010/10:12:01:58:06
>   @ECT_SetRelay stx,off $TIME=2010/10:12:02:37:00
>
>On Fri, Sep 24, 2010 at 3:53 PM, Reno, Michelle 
><<mailto:mreno at swri.edu>mreno at swri.edu> wrote:
>
>Sheral, please reduce the contact from 90 minutes. The P/L team will 
>have to deal with a partial dump if the first pass fails.
>
>
>
>
>
>--
>Sheral R. Wesley
>SPVR., Satellite Operations
>IBEX Mission OPS
>(304) 279-6678
>
>Content-type: text/plain; charset=US-ASCII; name=IBEX_2010_276_00_00_v002.txt
>Content-transfer-encoding: 7BIT
>Content-disposition: attachment; filename=IBEX_2010_276_00_00_v002.txt
>X-Attachment-Id: f_gehnurhi0
>
>Attachment converted: Eowyn:IBEX_2010_276_00_00_v002.txt (TEXT/QED1) 
>(00645DDE)


-- 
						- Mark     210-379-4635
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