[Isocops] IBEX Orbit# 441 ATS Approval (19 - 28 March 2019) - v001 approval

KEN FAIRCHILD fair-play at comcast.net
Thu Mar 7 22:45:45 EST 2019


All,


Note: Angle at orbit 441 arc B descending after the apogee sun precession maneuver: 3.964 deg


I have looked at the orbit 441 ATS,


IBEX_2019_078_o0441a_v001.scr,


and I approve.


The only constraint violations in


IBEX_2019_078_o0441a_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_2019_078_o0441a_v002.stf.


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


IBEX_2019_078_o0441a_v001.oef,


and as verified with ibex_orbit.


There are two star tracker outages.  The first starts before 15 Re descending in orbit 440 and runs for about 2 days.  The second starts 2+ days before apogee and runs for 3+ days.  Some despinning may be required due to these outages.


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


IBEX_Orbit441_Contacts.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 440 left us pointing in safe directions for the orbit 441 arc A ascending and descending sequences:


ibex_rotate -o -r +358.510 -d -0.632 -w ibex-sun -t 2019/03:20:06:08:09

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

points axis +1.000000,+0.000000,+0.000000

towards ECI +0.999601,-0.026001,-0.011030

which is R.A. +358.510 Decl. -0.632

missing R.A. +359.158 Decl. -0.387 (ibex-sun)

error is R.A. +0.648 Decl. +0.245

for a total 0.693 deg


ibex_rotate -o -r +358.510 -d -0.632 -w ibex-sun -t 2019/03:24:08:21:51

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

points axis +1.000000,+0.000000,+0.000000

towards ECI +0.999601,-0.026001,-0.011030

which is R.A. +358.510 Decl. -0.632

missing R.A. +2.986 Decl. +1.294 (ibex-sun)

error is R.A. +355.524 Decl. +1.926

for a total 4.872 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 +3.053 -d +1.325 -w ibex-sun -t 2019/03:24:10:09:59

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

points axis +1.000000,+0.000000,+0.000000

towards ECI +0.998314,+0.053245,+0.023124

which is R.A. +3.053 Decl. +1.325

missing R.A. +3.053 Decl. +1.325 (ibex-sun)

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

for a total 0.001 deg


ibex_rotate -o -r +3.053 -d +1.325 -w ibex-sun -t 2019/03:24:11:40:05

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

points axis +1.000000,+0.000000,+0.000000

towards ECI +0.998314,+0.053245,+0.023124

which is R.A. +3.053 Decl. +1.325

missing R.A. +3.110 Decl. +1.350 (ibex-sun)

error is R.A. +0.057 Decl. +0.025

for a total 0.062 deg


ibex_rotate -o -r +3.053 -d +1.325 -w ibex-sun -t 2019/03:28:13:24:40

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

points axis +1.000000,+0.000000,+0.000000

towards ECI +0.998314,+0.053245,+0.023124

which is R.A. +3.053 Decl. +1.325

missing R.A. +6.688 Decl. +2.912 (ibex-sun)

error is R.A. +3.635 Decl. +1.587

for a total 3.964 deg


The inertial maneuver at perigee leaves us pointing in safe directions at the time of the maneuver and at orbit 442 apogee:


ibex_rotate -o -u 0.995481,0.090333,0.029282 -w ibex-sun -t 2019/03:28:16:37:26

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

points axis +1.000000,+0.000000,+0.000000

towards ECI +0.995481,+0.090333,+0.029282

which is R.A. +5.185 Decl. +1.678

missing R.A. +6.808 Decl. +2.957 (ibex-sun)

error is R.A. +1.623 Decl. +1.279

for a total 2.065 deg


ibex_rotate -o -u 0.995481,0.090333,0.029282 -w ibex-sun -t 2019-04-02T12:58:30.243Z

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

points axis +1.000000,+0.000000,+0.000000

towards ECI +0.995481,+0.090333,+0.029282

which is R.A. +5.185 Decl. +1.678

missing R.A.+11.357 Decl. +4.880 (ibex-sun)

error is R.A. +6.172 Decl. +3.202

for a total 6.943 deg


No Lo O-Mode.


There is no overlap with orbit 440 commands by manual inspection or by checking at


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


Command Approval Checklist is attached.


Ken


> On March 6, 2019 at 11:08 AM "Perry, Timothy" <Timothy.Perry at ngc.com> wrote:
> 
> 
>     All,
> 
>        Attached are the planning files for Orbit #441.
> 
>     Please respond to this thread with comments and approvals.
> 
>     Approvals are required by COB 09 March 2019.
> 
>      
> 
>     Please Note the following:
> 
>     1.       # Orbit 441 Battery Balancing 
> 
>         # 2019-03-28T23:25:33.907Z,Perigee,orbit:441
> 
>           @ECT_SetLongEclipseFlag TRUE $TIME=2019/03:28:23:00:00
> 
>           @ECT_SetLongEclipseFlag FALSE $TIME=2019/03:29:00:30:00
> 
>          
> 
>     2.       Apogee Sun Maneuver @ 2019/03:24:09:54:59
> 
>      
> 
>     3.       The APL pass was replaced with a USAK01 contact
> 
>         IBEX,APL,CANCELED,03/28/19,087,21:30:00,03/28/19,87,22:30:00,,LAHO 2-320K IBEX-1 Orbit # 441 SSR_Dump/Tracking Contact
> 
>         IBEX,USAK01,ADD,03/28/19,087,21:30:00,03/28/19,087,22:30:00,,LAHO 160K IBEX-1 Orbit # 441 SSR_Dump/Tracking Contact
> 
>      
> 
>     4.       The Second perigee Pass is at 15 re asc and will double as the Hi Background Test End pass. This will be in the Orbit # 442 ATS
> 
>     IBEX,USHI01,ADD,03/29/19,088,10:00:00,03/29/19,088,11:00:00,,LAHO 64K IBEX-1 Orbit # 442 Hi background Test End/Tracking Contact 15 re
> 
>      
> 
>     5.       IBEX_2019_078_o0441a_v001_.ccvr
> 
>         # Input files:         1
> 
>         #   IBEX_2019_078_o0441a_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 2019/03/20 03:35:09 UTC
> 
>         IBX-CLC-016: No command to enable spin pulse protection was found after
> 
>                      transition to science mode at 2019/03/24 11:10:05 UTC
> 
>          
> 
>         ==============
> 
>         OTHER MESSAGES
> 
>         ==============
> 
>         NO MESSAGES.
> 
>      
> 
>     Timothy E. Perry
> 
>     Mission Operations
> 
>     CRS, IBEX, OCO-2 & TESS
> 
>     RAPTOR Test Team
> 
>     timothy.perry at ngc.com mailto:timothy.perry at ngc.com
> 
>     Office (703) 406-5976
> 
>     Cell (301) 606-1430
> 
>      
> 
>      
> 
> 
> 
>     ---------------------------------------------
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>     *********************
> 


 
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