[Isocops] IBEX Orbit #465 ATS Approval ( 23 Oct - 01 Nov 2019 ) - v001 approval

KEN FAIRCHILD fair-play at comcast.net
Thu Oct 10 17:44:33 EDT 2019


All,


I have looked at the orbit 465 ATS,


IBEX_2019_296_o0465a_v001.scr,


and I approve.


The only constraint violations in


IBEX_2019_296_o0465a_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_296_o0465a_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_296_o0465a_v001.oef,


and as verified with ibex_orbit.


There are no star tracker outages.


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


IBEX_Orbit465_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 inertial precession maneuver at perigee of orbit 464 left us pointing in safe directions for the orbit 465 arc A ascending and descending sequences:


ibex_rotate -o -u -0.892817,-0.409593,-0.187381 -w ibex-sun -t 2019/10:23:15:06:57

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

points axis +1.000000,+0.000000,+0.000000

towards ECI -0.892817,-0.409593,-0.187381

which is R.A. +204.644 Decl. -10.800

missing R.A. +207.589 Decl. -11.373 (ibex-sun)

error is R.A. +2.945 Decl. +0.573

for a total 2.946 deg


ibex_rotate -o -u -0.892817,-0.409593,-0.187381 -w ibex-sun -t 2019/10:27:05:51:50

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

points axis +1.000000,+0.000000,+0.000000

towards ECI -0.892817,-0.409593,-0.187381

which is R.A. +204.644 Decl. -10.800

missing R.A. +210.931 Decl. -12.564 (ibex-sun)

error is R.A. +6.287 Decl. +1.764

for a total 6.404 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 -0.854528,-0.472426,-0.21586 -w ibex-sun -t 2019/10:27:07:33:48

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

points axis +1.000000,+0.000000,+0.000000

towards ECI -0.854528,-0.472426,-0.215860

which is R.A. +208.936 Decl. -12.466

missing R.A. +210.998 Decl. -12.587 (ibex-sun)

error is R.A. +2.062 Decl. +0.121

for a total 2.017 deg


ibex_rotate -o -u -0.854528,-0.472426,-0.21586 -w ibex-sun -t 2019/10:27:09:10:04

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

points axis +1.000000,+0.000000,+0.000000

towards ECI -0.854528,-0.472426,-0.215860

which is R.A. +208.936 Decl. -12.466

missing R.A. +211.062 Decl. -12.608 (ibex-sun)

error is R.A. +2.126 Decl. +0.142

for a total 2.080 deg


ibex_rotate -o -u -0.854528,-0.472426,-0.21586 -w ibex-sun -t 2019/10:31:19:19:31

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

points axis +1.000000,+0.000000,+0.000000

towards ECI -0.854528,-0.472426,-0.215860

which is R.A. +208.936 Decl. -12.466

missing R.A. +215.456 Decl. -14.095 (ibex-sun)

error is R.A. +6.520 Decl. +1.629

for a total 6.551 deg


The inertial precession maneuver at perigee leaves us pointing in safe directions at the time of the maneuver and at orbit 466 apogee:


ibex_rotate -o -u -0.811712,-0.532222,-0.24055 -w ibex-sun -t 2019/10:31:22:39:00

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

points axis +1.000000,+0.000000,+0.000000

towards ECI -0.811712,-0.532222,-0.240550

which is R.A. +213.252 Decl. -13.919

missing R.A. +215.597 Decl. -14.148 (ibex-sun)

error is R.A. +2.345 Decl. +0.229

for a total 2.287 deg


ibex_rotate -o -u -0.811712,-0.532222,-0.24055 -w ibex-sun -t 2019-11-05T18:28:45.896Z

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

points axis +1.000000,+0.000000,+0.000000

towards ECI -0.811712,-0.532222,-0.240550

which is R.A. +213.252 Decl. -13.919

missing R.A. +220.234 Decl. -15.638 (ibex-sun)

error is R.A. +6.982 Decl. +1.719

for a total 6.966 deg


No Lo O-mode.


There is no overlap with orbit 464 commands by manual inspection or by checking at


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


Command Approval Checklist is attached.


Ken

> On October 8, 2019 at 6:36 PM "Perry, Timothy" <Timothy.Perry at ngc.com> wrote:
> 
> 
>     All,
> 
>        Attached are the planning files for Orbit #465
> 
>     Please respond to this thread with comments and approvals.  
> 
>     Approvals are required by COB on 12 Oct 2019.  
> 
> 
>     Please note the following:
> 
>     1.       Battery Balancing
> 
>         # Orbit 465 Battery Balancing 
> 
>         # 2019-11-01T05:14:46.194Z,Perigee,orbit:465
> 
>           @ECT_SetLongEclipseFlag TRUE $TIME=2019/11:01:05:00:00
> 
>          @ECT_SetLongEclipseFlag FALSE $TIME=2019/11:01:06:30:00
> 
>      
> 
>     2.       @ Inertial maneuvers
> 
>      
> 
>     3.       Command Load Constraint Violation Report (CCVR)
> 
>         ==========================
> 
>         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 2019/10/23 12:34:18 UTC
> 
>         IBX-CLC-016: No command to enable spin pulse protection was found after
> 
>                      transition to science mode at 2019/10/27 08:40:04 UTC
> 
>          
> 
>         ==============
> 
>         OTHER MESSAGES
> 
>         ==============
> 
>         NO MESSAGES.
> 
>          
> 
>      
> 
>      
> 
>      
> 
>     Timothy E.Perry
> 
>     CRS IBEX OCO-2
> 
>     Mission Operations
> 
>     timothy.perry at ngc.com
> 
>     Office (703) 406-5976
> 
>     Cell (301) 606-1430
> 
>      
> 
>     [cid:image001.png at 01D542D6.6047A400]
> 
>      
> 
>      
> 
> 
> 
>     ---------------------------------------------
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>     *********************
> 


 
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