[Isocops] IBEX ORbit# 322 ATS Approval (1 Apr 16 - 10 Apr 16) - v001 approval

Ken Fairchild fair-play at comcast.net
Mon Mar 21 19:17:42 EDT 2016


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 



----- Original Message -----

From: "Wesley.Sheral" <sheral.wesley at orbitalatk.com> 
To: "David Heirtzler" <dheirtzl at atlas.sr.unh.edu>, "IBEX-FDG" <IBEX.fdg at applieddefense.com>, "IBEXOPS" <IBEXOPS at gmail.com>, "ISOC" <isocops at lists.sr.unh.edu>, "Ken Fairchild" <fair-play at comcast.net>, "Lockwood.Robert" <robert.lockwood at orbitalatk.com>, "Michelle Reno" <mreno at swri.edu>, "Nigel Angold" <nigel.angold at nasa.gov>, "Paul Janzen" <paul.janzen at umontana.edu>, "Perry.Tim" <tim.perry at orbitalatk.com>, "Tyler.Ryan" <ryan.tyler at orbitalatk.com>, "Wesley.Sheral" <sheral.wesley at 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 







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