IBEX_2017_136_o0367a_v001.scr,

and I approve.

The only constraint violations in

IBEX_2017_136_o0367a_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_136_o0367a_v002.stf,

except that the ATS has an SSR_DUMP_NEW command.  This is expected as APL is being used for a dump pass.

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_136_o0367a_v001.oef,

and as verified with ibex_orbit.

There are no star tracker outages.

There is one moon in Lo FOV session in arc A.  The ATS start time is almost 5 hours after that in the OEF and the ATS end time is about 2 hours after that in the OEF.  These differences are not unusual.

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

IBEX_Orbit367_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 maneuver at perigee of orbit 366 left us pointing in safe directions for the orbit 367 arc A ascending and descending sequences:

ibex_rotate -o -u 0.603139,0.735581,0.308453 -w ibex-sun -t 2017/05:16:12:38:53

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.  +53.245 Decl. +19.133 (ibex-sun)

 error is     R.A.   +2.595 Decl.  +1.167

 for a total  2.723 deg

ibex_rotate -o -u 0.603139,0.735581,0.308453 -w ibex-sun -t 2017/05:19:23:09:51

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.  +56.776 Decl. +19.902 (ibex-sun)

 error is     R.A.   +6.126 Decl.  +1.936

 for a total  6.109 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 0.543251,0.774347,0.324446 -w ibex-sun -t 2017/05:20:00:52:59

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

 points axis  +1.000000,+0.000000,+0.000000

 towards ECI  +0.543251,+0.774347,+0.324446

 which is     R.A.  +54.948 Decl. +18.932

 missing      R.A.  +56.849 Decl. +19.918 (ibex-sun)

 error is     R.A.   +1.901 Decl.  +0.986

 for a total  2.046 deg

ibex_rotate -o -u 0.543251,0.774347,0.324446 -w ibex-sun -t 2017/05:20:02:28:05

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

 points axis  +1.000000,+0.000000,+0.000000

 towards ECI  +0.543251,+0.774347,+0.324446

 which is     R.A.  +54.948 Decl. +18.932

 missing      R.A.  +56.916 Decl. +19.932 (ibex-sun)

 error is     R.A.   +1.968 Decl.  +1.000

 for a total  2.108 deg

ibex_rotate -o -u 0.543251,0.774347,0.324446 -w ibex-sun -t 2017/05:24:08:47:31

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

 points axis  +1.000000,+0.000000,+0.000000

 towards ECI  +0.543251,+0.774347,+0.324446

 which is     R.A.  +54.948 Decl. +18.932

 missing      R.A.  +61.123 Decl. +20.808 (ibex-sun)

 error is     R.A.   +6.175 Decl.  +1.876

 for a total  6.103 deg

The inertial precession maneuver at perigee leaves us pointing in safe directions at the time of the maneuver and at orbit 368 apogee:

ibex_rotate -o -u 0.478535,0.809384,0.340445 -w ibex-sun -t 2017/05:24:10:59:53

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

 points axis  +1.000000,+0.000000,+0.000000

 towards ECI  +0.478535,+0.809384,+0.340445

 which is     R.A.  +59.407 Decl. +19.904

 missing      R.A.  +61.209 Decl. +20.822 (ibex-sun)

 error is     R.A.   +1.802 Decl.  +0.918

 for a total  1.923 deg

ibex_rotate -o -u 0.478535,0.809384,0.340445 -w ibex-sun -t 2017-05-29T09:44:50.595Z

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

 points axis  +1.000000,+0.000000,+0.000000

 towards ECI  +0.478535,+0.809384,+0.340445

 which is     R.A.  +59.407 Decl. +19.904

 missing      R.A.  +66.303 Decl. +21.625 (ibex-sun)

 error is     R.A.   +6.896 Decl.  +1.721

 for a total  6.673 deg

No Lo O-mode.

There is no overlap with orbit 366 commands by manual inspection or by checking at

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

Command Approval Checklist is attached.

Ken