IBEX_2016_356_o0351a_v001.scr,
and I approve.
The only constraint violations in
IBEX_2016_356_o0351a_v001.ccvr
are because we removed the
ACT_SetSpinPulseProtectEnable Enable
commands (2); the violations are expected.
The PL commands in the v001 ATS match those in the v003 STF,
IBEX_2016_356_o0351a_v003.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_2016_356_o0351a_v001.oef,
and as verified with ibex_orbit.
There is one star tracker outage. The outage starts 2+ days before apogee and runs for 1 1/2+ days. Some despinning may be required due to this outage.
There is one moon in Lo FOV session in arc A. The ATS start time is about 1 1/2 hours after that in the OEF and the ATS end time is about 2 1/2 hours before 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_Orbit351_Contacts.txt,
for all contacts (2).
No battery cell balancing this orbit; we'll do it again in the next orbit.
The inertial maneuver at perigee of orbit 350 left us pointing in safe directions for the orbit 351 arc A ascending and descending sequences:
ibex_rotate -o -u 0.017073,-0.913279,-0.406976 -w ibex-sun -t 2016/12:21:23:28:24
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.017073,-0.913279,-0.406976
which is R.A. +271.071 Decl. -24.015
missing R.A. +270.379 Decl. -23.452 (ibex-sun)
error is R.A. +0.692 Decl. +0.563
for a total 0.847 deg
ibex_rotate -o -u 0.017073,-0.913279,-0.406976 -w ibex-sun -t 2016/12:26:11:23:37
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.017073,-0.913279,-0.406976
which is R.A. +271.071 Decl. -24.015
missing R.A. +275.283 Decl. -23.373 (ibex-sun)
error is R.A. +4.212 Decl. +0.642
for a total 3.910 deg
The inertial 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 -u 0.098165,-0.909089,-0.40487 -w ibex-sun -t 2016/12:26:13:07:29
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.098165,-0.909090,-0.404870
which is R.A. +276.163 Decl. -23.883
missing R.A. +275.361 Decl. -23.370 (ibex-sun)
error is R.A. +0.802 Decl. +0.513
for a total 0.896 deg
ibex_rotate -o -u 0.098165,-0.909089,-0.40487 -w ibex-sun -t 2016/12:26:14:41:51
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.098165,-0.909090,-0.404870
which is R.A. +276.163 Decl. -23.883
missing R.A. +275.433 Decl. -23.367 (ibex-sun)
error is R.A. +0.730 Decl. +0.516
for a total 0.845 deg
ibex_rotate -o -u 0.098165,-0.909089,-0.40487 -w ibex-sun -t 2016/12:30:07:05:30
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.098165,-0.909090,-0.404870
which is R.A. +276.163 Decl. -23.883
missing R.A. +279.527 Decl. -23.128 (ibex-sun)
error is R.A. +3.364 Decl. +0.755
for a total 3.176 deg
The inertial precession maneuver at perigee leaves us pointing in safe directions at the time of the maneuver and at orbit 352 apogee:
ibex_rotate -o -u 0.181354,-0.898202,-0.400429 -w ibex-sun -t 2016/12:30:09:22:02
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.181354,-0.898202,-0.400429
which is R.A. +281.415 Decl. -23.605
missing R.A. +279.639 Decl. -23.122 (ibex-sun)
error is R.A. +1.776 Decl. +0.483
for a total 1.701 deg
ibex_rotate -o -u 0.181354,-0.898202,-0.400429 -w ibex-sun -t 2017-01-04T09:43:36.601Z
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.181354,-0.898202,-0.400429
which is R.A. +281.415 Decl. -23.605
missing R.A. +285.180 Decl. -22.732 (ibex-sun)
error is R.A. +3.765 Decl. +0.873
for a total 3.569 deg
No Lo O-mode.
There is no overlap with orbit 350 commands by manual inspection or by checking at
http://ibex.unh.edu/cgi-bin/ats.cgi.
Command Approval Checklist is attached.
Ken
Guys,
Here are the planning files and ATS for Orbit# 351 (21 Dec 16 – 30 Dec 16)
Please respond to this email thread with your comments and approvals
Approvals are required before 11 Dec 16 @1400 UTC
Note the following:
1. Moon in Lo FOV Commands
2016-12-22T05:12:35.647Z,MoonInLoFovStart,orbit:351
2016-12-25T14:06:21.621Z,MoonInLoFovStop,orbit:351
Sheral R. Wesley
IBEX Mission OPS
CRS/CYGNUS Mission Planning
Bldg. 2 Room 1337
Office (703) 406-5641
Cell (202) 236-0802