IBEX_2019_314_o0467a_v001.scr,

and I approve.

The only constraint violations in

IBEX_2019_314_o0467a_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_314_o0467a_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_314_o0467a_v001.oef,

and as verified with ibex_orbit.

There is one star tracker outage. The outage starts at perigee of orbit 466 and runs for 1 1/2+ days. Some despinning may be required due to this outage.

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

IBEX_Orbit467_Contacts.txt,

for all contacts (2).

We are not doing battery cell balancing this orbit; we'll do it again in the next orbit.

The inertial maneuver at perigee of orbit 466 left us pointing in safe directions for the orbit 467 arc A ascending and descending sequences:

ibex_rotate -o -u -0.70876,-0.643612,-0.288831 -w ibex-sun -t 2019/11:10:17:22:09

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

points axis +1.000000,+0.000000,+0.000000

towards ECI -0.708760,-0.643612,-0.288831

which is R.A. +222.242 Decl. -16.788

missing R.A. +225.310 Decl. -17.148 (ibex-sun)

error is R.A. +3.068 Decl. +0.360

for a total 2.957 deg

ibex_rotate -o -u -0.70876,-0.643612,-0.288831 -w ibex-sun -t 2019/11:14:22:37:03

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

points axis +1.000000,+0.000000,+0.000000

towards ECI -0.708760,-0.643612,-0.288831

which is R.A. +222.242 Decl. -16.788

missing R.A. +229.487 Decl. -18.237 (ibex-sun)

error is R.A. +7.245 Decl. +1.449

for a total 7.059 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 +229.563 -d -18.255 -w ibex-sun -t 2019/11:15:00:25:11

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

points axis +1.000000,+0.000000,+0.000000

towards ECI -0.615968,-0.722814,-0.313247

which is R.A. +229.563 Decl. -18.255

missing R.A. +229.563 Decl. -18.255 (ibex-sun)

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

for a total 0.000 deg

ibex_rotate -o -r +229.563 -d -18.255 -w ibex-sun -t 2019/11:15:01:55:17

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

points axis +1.000000,+0.000000,+0.000000

towards ECI -0.615968,-0.722814,-0.313247

which is R.A. +229.563 Decl. -18.255

missing R.A. +229.627 Decl. -18.270 (ibex-sun)

error is R.A. +0.064 Decl. +0.015

for a total 0.062 deg

ibex_rotate -o -r +229.563 -d -18.255 -w ibex-sun -t 2019/11:19:05:28:18

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

points axis +1.000000,+0.000000,+0.000000

towards ECI -0.615968,-0.722814,-0.313247

which is R.A. +229.563 Decl. -18.255

missing R.A. +233.994 Decl. -19.306 (ibex-sun)

error is R.A. +4.431 Decl. +1.051

for a total 4.325 deg

The inertial maneuver at perigee leaves us pointing in safe directions at the time of the maneuver and at orbit 468 apogee:

ibex_rotate -o -u -0.584749,-0.74066,-0.330893 -w ibex-sun -t 2019/11:19:08:48:13

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

points axis +1.000000,+0.000000,+0.000000

towards ECI -0.584749,-0.740660,-0.330893

which is R.A. +231.709 Decl. -19.323

missing R.A. +234.147 Decl. -19.347 (ibex-sun)

error is R.A. +2.438 Decl. +0.024

for a total 2.301 deg

ibex_rotate -o -u -0.584749,-0.74066,-0.330893 -w ibex-sun -t 2019-11-24T05:00:11.247Z

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

points axis +1.000000,+0.000000,+0.000000

towards ECI -0.584749,-0.740660,-0.330893

which is R.A. +231.709 Decl. -19.323

missing R.A. +239.138 Decl. -20.406 (ibex-sun)

error is R.A. +7.429 Decl. +1.083

for a total 7.070 deg

No Lo O-mode.

There is no overlap with orbit 466 commands by manual inspection or by checking at

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

Command Approval Checklist is attached.

Ken