IBEX_2016_092_o0322a_Recovery_v001.scr,
and I approve.
The only constraint violations in
IBEX_2016_092_o0322a_Recovery_v001.ccvr
are because we removed the
ACT_SetSpinPulseProtectEnable Enable
commands; the violations are expected.
The PL commands in the v001 ATS match those in the v003 STF,
IBEX_2016_092_o0322a_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_092_o0322a_Recovery_v001.oef,
and as verified with ibex_orbit.
There is one star tracker outage. It starts about a day before 15 Re descending and ends 3- hours before 15 Re descending. Some despinning may be required due to this outage.
There are no moon in Lo FOV sessions.
The ground station command sequences are correct and the timing and bit rates match those in the contacts file,
IBEX_Orbit322_RecoveryContacts.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 321 left us pointing in safe directions for the orbit 322 arc A ascending and descending sequences:
ibex_rotate -o -r +10.481 -d +4.526 -w ibex-sun -t 2016/04:01:19:36:22
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.980249,+0.181342,+0.078911
which is R.A. +10.481 Decl. +4.526
missing R.A. +11.298 Decl. +4.842 (ibex-sun)
error is R.A. +0.817 Decl. +0.316
for a total 0.874 deg
ibex_rotate -o -r +10.481 -d +4.526 -w ibex-sun -t 2016/04:05:18:57:17
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.980249,+0.181342,+0.078911
which is R.A. +10.481 Decl. +4.526
missing R.A. +15.030 Decl. +6.381 (ibex-sun)
error is R.A. +4.549 Decl. +1.855
for a total 4.894 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 +15.098 -d +6.410 -w ibex-sun -t 2016/04:05:20:45:08
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.959446,+0.258842,+0.111642
which is R.A. +15.098 Decl. +6.410
missing R.A. +15.098 Decl. +6.410 (ibex-sun)
error is R.A. +0.000 Decl. +0.000
for a total 0.000 deg
ibex_rotate -o -r +15.098 -d +6.410 -w ibex-sun -t 2016/04:05:22:15:31
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.959446,+0.258842,+0.111642
which is R.A. +15.098 Decl. +6.410
missing R.A. +15.155 Decl. +6.434 (ibex-sun)
error is R.A. +0.057 Decl. +0.024
for a total 0.062 deg
ibex_rotate -o -r +15.098 -d +6.410 -w ibex-sun -t 2016/04:09:22:34:44
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.959446,+0.258842,+0.111642
which is R.A. +15.098 Decl. +6.410
missing R.A. +18.706 Decl. +7.933 (ibex-sun)
error is R.A. +3.608 Decl. +1.523
for a total 3.890 deg
The sun precession maneuver at perigee leaves us pointing in safe directions at the time of the maneuver and at orbit 323 apogee:
ibex_rotate -o -r +18.801 -d +7.970 -w ibex-sun -t 2016/04:10:01:10:49
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.937500,+0.319169,+0.138655
which is R.A. +18.801 Decl. +7.970
missing R.A. +18.801 Decl. +7.970 (ibex-sun)
error is R.A. +0.000 Decl. +0.000
for a total 0.000 deg
ibex_rotate -o -r +18.801 -d +7.970 -w ibex-sun -t 2016-04-15T01:52:50.184Z
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.937500,+0.319169,+0.138655
which is R.A. +18.801 Decl. +7.970
missing R.A. +23.575 Decl. +9.803 (ibex-sun)
error is R.A. +4.774 Decl. +1.833
for a total 5.060 deg
No Lo O-mode.
There is no overlap with orbit 321 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# 322.
Please respond to this email thread with your comments and approvals.
Approvals are required before 22 Mar 16 #1800 UTC
Note the following:
1. Battery Balancing at PERIGEE
Orbit# 322 PERIGEE: Battery Balancing Commands
# 2016-04-10T09:53:50.602Z,Perigee,orbit:322
SetLongEclipseFlag TRUE $TIME=2016/04:10:10:00:00
SetLongEclipseFlag FALSE $TIME=2016/04:10:11:30:00
2. No ACT_SetSpinPulseProtectEnable Enable Commands
3. Apogee Sun Maneuver
4. Perigee Sun Maneuver
5. Command Load Constraint Violation Report
IBEX_2016_092_o0322a_Recovery_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 2016/04/01 17:56:35 UTC
IBX-CLC-016: No command to enable spin pulse protection was found after
transition to science mode at 2016/04/05 21:45:33 UTC
==============
OTHER MESSAGES
==============
NO MESSAGES.
Sheral R. Wesley
IBEX Mission OPS
CRS/CYGNUS Mission Planning
Bldg. 2 Room 1337
Office (703) 406-5641
Cell (202) 236-0802