[Isocops] IBEX Orbit# 150 ATS v003 - approve

[Mark Tapley]

All,
	I have looked at the Orbit 150 ATS v003

IBEX_2011_354_o0150a_v003.txt

and I approve.

	No constraint violation per .ccvr file:

IBEX_2011_354_o0150a_v003.ccvr

	The PL commands in the ATS v003 match the STF v002

IBEX_2011_354_o0150a_v003.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_2011_354_o0150a_v002.oef

	No Moon in -Lo FOV PMT setback commands and none needed per the .oef.

	Ground station contact times and rates per

IBEX_Orbit150Contacts_v001.txt

match S/C commands for all 3 contacts.

	No battery cell balancing this orbit.

	Inertial maneuver at the end of orbit 149 left us pointing in 
a safe direction for ascending and descending macros during first 
half of orbit:

[tapley at ena ~]$ ibex_rotate -o -u -0.079562,-0.909403,-0.408235 -w 
ibex-sun -t 2011/12:20:21:39:53
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  -0.079562,-0.909403,-0.408235
  which is     R.A. +265.000 Decl. -24.094
  missing      R.A. +268.362 Decl. -23.419 (ibex-sun)
  error is     R.A.   +3.362 Decl.  +0.675
  for a total  3.151 deg
[tapley at ena ~]$ ibex_rotate -o -u -0.079562,-0.909403,-0.408235 -w 
ibex-sun -t 2011/12:24:11:37:01
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  -0.079562,-0.909403,-0.408235
  which is     R.A. +265.000 Decl. -24.094
  missing      R.A. +272.221 Decl. -23.450 (ibex-sun)
  error is     R.A.   +7.221 Decl.  +0.644
  for a total  6.639 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 0.00223,-0.912503,-0.409063 -w 
ibex-sun -t 2011/12:24:13:11:25
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  +0.002230,-0.912503,-0.409063
  which is     R.A. +270.140 Decl. -24.146
  missing      R.A. +272.293 Decl. -23.449 (ibex-sun)
  error is     R.A.   +2.153 Decl.  +0.697
  for a total  2.090 deg
[tapley at ena ~]$ ibex_rotate -o -u 0.00223,-0.912503,-0.409063 -w 
ibex-sun -t 2011/12:24:14:58:31
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  +0.002230,-0.912503,-0.409063
  which is     R.A. +270.140 Decl. -24.146
  missing      R.A. +272.375 Decl. -23.448 (ibex-sun)
  error is     R.A.   +2.235 Decl.  +0.698
  for a total  2.160 deg
[tapley at ena ~]$ ibex_rotate -o -u 0.00223,-0.912503,-0.409063 -w 
ibex-sun -t 2011/12:28:23:43:23
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  +0.002230,-0.912503,-0.409063
  which is     R.A. +270.140 Decl. -24.146
  missing      R.A. +277.296 Decl. -23.279 (ibex-sun)
  error is     R.A.   +7.156 Decl.  +0.867
  for a total  6.608 deg

	Inertial maneuver at perigee leaves us pointing in a safe 
direction at maneuver and (barely) at following Apogee.

[tapley at ena ~]$ ibex_rotate -o -u 0.081676,-0.909252,-0.408155 -w 
ibex-sun -t 2011/12:29:10:16:53
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  +0.081676,-0.909252,-0.408155
  which is     R.A. +275.133 Decl. -24.089
  missing      R.A. +277.822 Decl. -23.239 (ibex-sun)
  error is     R.A.   +2.689 Decl.  +0.850
  for a total  2.605 deg
[tapley at ena ~]$ ibex_rotate -o -u 0.081676,-0.909252,-0.408155 -w 
ibex-sun -t 2012-01-03T00:42:17.120Z
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
  points axis  +1.000000,+0.000000,+0.000000
  towards ECI  +0.081676,-0.909252,-0.408155
  which is     R.A. +275.133 Decl. -24.089
  missing      R.A. +282.800 Decl. -22.947 (ibex-sun)
  error is     R.A.   +7.667 Decl.  +1.142
  for a total  7.122 deg

	O-mode Commands during arc B only; no start/stop times.

	No overlaps to orbit 148 by manual check or by reference to 
http://ibex.unh.edu/cgi-bin/ats.cgi.

	Command Approval Checklist attached.

	-Hi Neg collimator voltage set to 1400V on arc A only.


At 20:51 -0500 12/7/11, Ibex Mission Operations wrote:
>Guys,
>      Here are the planning files and ATS for Orbit# 150 v003.
>
>Please note the following changes:
>1. The Inertial Maneuver at PERIGEE takes place outside of the eclipse.
>2.  The V003 ATS does not include the commands to set the O-mode 
>start/stop bins
>3.  The CCVR report has no violations

-- 
						- Mark     210-379-4635
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