[Isocops] IBEX Orbit #366 ATS ( 7 - 16 May ) - v001 approval

Ken Fairchild fair-play at comcast.net
Tue Apr 25 09:08:29 EDT 2017


All, 

I have looked at the orbit 366 ATS, 



IBEX_2017_127_o0366a_v001.scr, 




and I approve. 




The only constraint violations in 




IBEX_2017_127_o0366a_v001.ccvr 




are from the removal of the 




ACT_SetSpinPulseProtectEnable Enable 



commands (2); the violations are expected. 




The PL commands in the v001 ATS match those in the v002 STF, 




IBEX_2017_127_o0366a_v002.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_2017_127_o0366a_v001.oef, 




and as verified with ibex_orbit. 




There is one star tracker outage. The outage starts 1+ days after apogee and runs for almost two days. 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_Orbit366_Contacts.txt, 




for all contacts (3). 




No battery cell balancing this orbit; we'll do it again in the next orbit. 




The inertial maneuver at perigee of orbit 365 left us pointing in safe directions for the orbit 366 arc A ascending and descending sequences: 




ibex_rotate -o -u 0.714991,0.645183,0.269306 -w ibex-sun -t 2017/05:07:16:17:31 

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

points axis +1.000000,+0.000000,+0.000000 

towards ECI +0.714991,+0.645183,+0.269306 

which is R.A. +42.062 Decl. +15.623 

missing R.A. +44.575 Decl. +16.903 (ibex-sun) 

error is R.A. +2.513 Decl. +1.280 

for a total 2.731 deg 




ibex_rotate -o -u 0.714991,0.645183,0.269306 -w ibex-sun -t 2017/05:11:03:26:12 

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

points axis +1.000000,+0.000000,+0.000000 

towards ECI +0.714991,+0.645183,+0.269306 

which is R.A. +42.062 Decl. +15.623 

missing R.A. +48.064 Decl. +17.842 (ibex-sun) 

error is R.A. +6.002 Decl. +2.219 

for a total 6.161 deg 




The inertial 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 -u 0.661389,0.6922,0.288831 -w ibex-sun -t 2017/05:11:05:09:20 

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

points axis +1.000000,+0.000000,+0.000000 

towards ECI +0.661389,+0.692200,+0.288831 

which is R.A. +46.304 Decl. +16.788 

missing R.A. +48.135 Decl. +17.862 (ibex-sun) 

error is R.A. +1.831 Decl. +1.074 

for a total 2.052 deg 




ibex_rotate -o -u 0.661389,0.6922,0.288831 -w ibex-sun -t 2017/05:11:06:44:26 

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

points axis +1.000000,+0.000000,+0.000000 

towards ECI +0.661389,+0.692200,+0.288831 

which is R.A. +46.304 Decl. +16.788 

missing R.A. +48.201 Decl. +17.880 (ibex-sun) 

error is R.A. +1.897 Decl. +1.092 

for a total 2.114 deg 




ibex_rotate -o -u 0.661389,0.6922,0.288831 -w ibex-sun -t 2017/05:15:12:43:46 

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

points axis +1.000000,+0.000000,+0.000000 

towards ECI +0.661389,+0.692200,+0.288831 

which is R.A. +46.304 Decl. +16.788 

missing R.A. +52.292 Decl. +18.951 (ibex-sun) 

error is R.A. +5.988 Decl. +2.163 

for a total 6.095 deg 




The inertial precession maneuver at perigee leaves us pointing in safe directions at the time of the maneuver and at orbit 367 apogee: 




ibex_rotate -o -u 0.603139,0.735581,0.308453 -w ibex-sun -t 2017/05:15:14:54:34 

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

points axis +1.000000,+0.000000,+0.000000 

towards ECI +0.603139,+0.735581,+0.308453 

which is R.A. +50.650 Decl. +17.966 

missing R.A. +52.374 Decl. +18.970 (ibex-sun) 

error is R.A. +1.724 Decl. +1.004 

for a total 1.919 deg 




ibex_rotate -o -u 0.603139,0.735581,0.308453 -w ibex-sun -t 2017-05-20T10:42:41.819Z 

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

points axis +1.000000,+0.000000,+0.000000 

towards ECI +0.603139,+0.735581,+0.308453 

which is R.A. +50.650 Decl. +17.966 

missing R.A. +57.263 Decl. +20.009 (ibex-sun) 

error is R.A. +6.613 Decl. +2.043 

for a total 6.578 deg 




No Lo O-mode. 




There is no overlap with orbit 365 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: "Timothy Perry" <Timothy.Perry at OrbitalATK.com> 
To: "David Heirtzler" <dfh at cisunix.unh.edu>, "IBEX-FDG" <IBEX.fdg at applieddefense.com>, "IBEXOPS" <IBEXOPS at gmail.com>, "ISOC at New Hampshire" <isocops at lists.sr.unh.edu>, "Ken Fairchild" <fair-play at comcast.net>, "Robert Lockwood" <Robert.Lockwood at OrbitalATK.com>, "Nigel Angold" <nigel.angold at nasa.gov>, "Paul Janzen" <paul.janzen at umontana.edu>, "Timothy Perry" <Timothy.Perry at OrbitalATK.com>, "Michelle Reno" <mreno at swri.edu>, "Ryan Tyler" <Ryan.Tyler at OrbitalATK.com>, "Sheral Wesley" <Sheral.Wesley at OrbitalATK.com> 
Sent: Monday, April 24, 2017 12:28:42 PM 
Subject: IBEX Orbit #366 ATS ( 7 - 16 May ) 



All, 

Attached are the planning products for Orbit #366. Please respond to this email thread with your comments and approvals. 

Approvals are required before COB on April 26. 



Note the following: 

1. No Battery Balancing 



2. IBEX Hi Gain Test 

a. # Start TIME=2017/05:05:13:00:00 

b. # End TIME=2017/05:05:17:15:41 



    1. Command Load Constraint Violation Report 



# Input files: 1 

# IBEX_2017_127_o0366a_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 2017/05/07 14:45:34 UTC 

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

transition to science mode at 2017/05/11 06:14:26 UTC 



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

OTHER MESSAGES 

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

NO MESSAGES. 









Timothy E. Perry 

CRS, IBEX & OCO-2 

Mission Operations 

Tim.perry at orbitalatk.com 

Office (703) 406-5976 

Cell (301) 606-1430 

Corp Cell (571) 447-8977 










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********************* 

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