All,

Note: Off-pointing at arc B descending is 3.890 deg
          Off-pointing at orbit 323 apogee is 5.060 deg

I have looked at the orbit 322 recovery ATS,

IBEX_2016_092_o0322a_Recovery_v001.scr,


and I approve.


The only constraint violations in


IBEX_2016_092_o0322a_Recovery_v001.ccvr


are because we removed the


ACT_SetSpinPulseProtectEnable Enable


commands; the violations are expected.


The PL commands in the v001 ATS match those in the v003 STF,


IBEX_2016_092_o0322a_v003.stf.


Ascending and descending command sequences are consistent with each other and 15 Re ascending, the apogee maneuver time and 15 Re descending as determined from the OEF,


IBEX_2016_092_o0322a_Recovery_v001.oef,


and as verified with ibex_orbit.


There is one star tracker outage.  It starts about a day before 15 Re descending and ends 3- hours before 15 Re descending.    Some despinning may be required due to this outage.


There are no moon in Lo FOV sessions.


The ground station command sequences are correct and the timing and bit rates match those in the contacts file,


IBEX_Orbit322_RecoveryContacts.txt,


for all contacts (3).


We are doing battery cell balancing this orbit and the balancing commands are correct and offset by enough time from other commands.


The sun precession maneuver at perigee of orbit 321 left us pointing in safe directions for the orbit 322 arc A ascending and descending sequences:


ibex_rotate -o -r +10.481 -d +4.526 -w ibex-sun -t 2016/04:01:19:36:22

Quaternion    +0.000000,+0.000000,+0.000000,+0.000000

 points axis  +1.000000,+0.000000,+0.000000

 towards ECI  +0.980249,+0.181342,+0.078911

 which is     R.A.  +10.481 Decl.  +4.526

 missing      R.A.  +11.298 Decl.  +4.842 (ibex-sun)

 error is     R.A.   +0.817 Decl.  +0.316

 for a total  0.874 deg


ibex_rotate -o -r +10.481 -d +4.526 -w ibex-sun -t 2016/04:05:18:57:17

Quaternion    +0.000000,+0.000000,+0.000000,+0.000000

 points axis  +1.000000,+0.000000,+0.000000

 towards ECI  +0.980249,+0.181342,+0.078911

 which is     R.A.  +10.481 Decl.  +4.526

 missing      R.A.  +15.030 Decl.  +6.381 (ibex-sun)

 error is     R.A.   +4.549 Decl.  +1.855

 for a total  4.894 deg


The sun precession maneuver at apogee leaves us pointing in safe directions at the time of the maneuver and for arc B ascending and descending sequences:


ibex_rotate -o -r +15.098 -d +6.410 -w ibex-sun -t 2016/04:05:20:45:08

Quaternion    +0.000000,+0.000000,+0.000000,+0.000000

 points axis  +1.000000,+0.000000,+0.000000

 towards ECI  +0.959446,+0.258842,+0.111642

 which is     R.A.  +15.098 Decl.  +6.410

 missing      R.A.  +15.098 Decl.  +6.410 (ibex-sun)

 error is     R.A.   +0.000 Decl.  +0.000

 for a total  0.000 deg


ibex_rotate -o -r +15.098 -d +6.410 -w ibex-sun -t 2016/04:05:22:15:31

Quaternion    +0.000000,+0.000000,+0.000000,+0.000000

 points axis  +1.000000,+0.000000,+0.000000

 towards ECI  +0.959446,+0.258842,+0.111642

 which is     R.A.  +15.098 Decl.  +6.410

 missing      R.A.  +15.155 Decl.  +6.434 (ibex-sun)

 error is     R.A.   +0.057 Decl.  +0.024

 for a total  0.062 deg


ibex_rotate -o -r +15.098 -d +6.410 -w ibex-sun -t 2016/04:09:22:34:44

Quaternion    +0.000000,+0.000000,+0.000000,+0.000000

 points axis  +1.000000,+0.000000,+0.000000

 towards ECI  +0.959446,+0.258842,+0.111642

 which is     R.A.  +15.098 Decl.  +6.410

 missing      R.A.  +18.706 Decl.  +7.933 (ibex-sun)

 error is     R.A.   +3.608 Decl.  +1.523

 for a total  3.890 deg


The sun precession maneuver at perigee leaves us pointing in safe directions at the time of the maneuver and at orbit 323 apogee:


ibex_rotate -o -r +18.801 -d +7.970 -w ibex-sun -t 2016/04:10:01:10:49

Quaternion    +0.000000,+0.000000,+0.000000,+0.000000

 points axis  +1.000000,+0.000000,+0.000000

 towards ECI  +0.937500,+0.319169,+0.138655

 which is     R.A.  +18.801 Decl.  +7.970

 missing      R.A.  +18.801 Decl.  +7.970 (ibex-sun)

 error is     R.A.   +0.000 Decl.  +0.000

 for a total  0.000 deg


ibex_rotate -o -r +18.801 -d +7.970 -w ibex-sun -t 2016-04-15T01:52:50.184Z

Quaternion    +0.000000,+0.000000,+0.000000,+0.000000

 points axis  +1.000000,+0.000000,+0.000000

 towards ECI  +0.937500,+0.319169,+0.138655

 which is     R.A.  +18.801 Decl.  +7.970

 missing      R.A.  +23.575 Decl.  +9.803 (ibex-sun)

 error is     R.A.   +4.774 Decl.  +1.833

 for a total  5.060 deg


No Lo O-mode.


There is no overlap with orbit 321 commands by manual inspection or by checking at


http://ibex.unh.edu/cgi-bin/ats.cgi.


Command Approval Checklist is attached.


Ken




From: "Wesley.Sheral" <sheral.wesley@orbitalatk.com>
To: "David Heirtzler" <dheirtzl@atlas.sr.unh.edu>, "IBEX-FDG" <IBEX.fdg@applieddefense.com>, "IBEXOPS" <IBEXOPS@gmail.com>, "ISOC" <isocops@lists.sr.unh.edu>, "Ken Fairchild" <fair-play@comcast.net>, "Lockwood.Robert" <robert.lockwood@orbitalatk.com>, "Michelle Reno" <mreno@swri.edu>, "Nigel Angold" <nigel.angold@nasa.gov>, "Paul Janzen" <paul.janzen@umontana.edu>, "Perry.Tim" <tim.perry@orbitalatk.com>, "Tyler.Ryan" <ryan.tyler@orbitalatk.com>, "Wesley.Sheral" <sheral.wesley@orbitalatk.com>
Sent: Saturday, March 19, 2016 7:14:59 PM
Subject: IBEX ORbit# 322 ATS Approval (1 Apr 16 - 10 Apr 16)

Guys,

Here are the planning files and ATS for Orbit# 322.

Please respond to this email thread with your comments and approvals.

Approvals are required before 22 Mar 16 #1800 UTC

 

Note the following:

1.       Battery Balancing at PERIGEE

Orbit# 322  PERIGEE: Battery Balancing Commands

# 2016-04-10T09:53:50.602Z,Perigee,orbit:322

  SetLongEclipseFlag TRUE $TIME=2016/04:10:10:00:00

  SetLongEclipseFlag FALSE $TIME=2016/04:10:11:30:00

 

2.       No  ACT_SetSpinPulseProtectEnable Enable  Commands

3.       Apogee Sun Maneuver

4.       Perigee Sun Maneuver

5.       Command Load Constraint Violation Report

IBEX_2016_092_o0322a_Recovery_v001.scr

 

==========================

HARD CONSTRAINT VIOLATIONS

==========================

NO VIOLATIONS.

 

==========================

SOFT CONSTRAINT VIOLATIONS

==========================

IBX-CLC-016: No command to enable spin pulse protection was found after

             transition to science mode at 2016/04/01 17:56:35 UTC

IBX-CLC-016: No command to enable spin pulse protection was found after

             transition to science mode at 2016/04/05 21:45:33 UTC

 

==============

OTHER MESSAGES

==============

NO MESSAGES.

 

 

 

Sheral  R. Wesley

IBEX Mission OPS

CRS/CYGNUS Mission Planning

Bldg. 2   Room 1337

Office (703) 406-5641

Cell (202) 236-0802

cid:image001.jpg@01D04F6C.5A1C97F0

 




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