IBEX_2017_190_o0373a_v001.scr,
and I approve.
The only constraint violations in
IBEX_2017_190_o0373a_v001.ccvr
are from proximity of contacts and 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_190_o0373a_v002.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_2017_190_o0373a_v001.oef,
and as verified with ibex_orbit.
There are two star tracker outages. The first starts before orbit 372 15 Re descending and ends 3 1/2 hours after 15 Re ascending. The second starts 2 1/2 hours before perigee and runs for 6 1/2 hours. Some despinning may be required due to the first outage.
There is one moon in Lo FOV session. It starts in arc A and ends in arc B. The ATS start time is four hours after that in the OEF and the ATS end time is 3 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_Orbit373_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 sun precession maneuver at perigee of orbit 372 left us pointing in safe directions for the orbit 373 arc A ascending and descending sequences:
ibex_rotate -o -r +107.801 -d +22.449 -w ibex-sun -t 2017/07:09:12:16:55
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.282545,+0.879972,+0.381861
which is R.A. +107.801 Decl. +22.449
missing R.A. +108.653 Decl. +22.309 (ibex-sun)
error is R.A. +0.852 Decl. +0.140
for a total 0.800 deg
ibex_rotate -o -r +107.801 -d +22.449 -w ibex-sun -t 2017/07:13:01:13:42
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.282545,+0.879972,+0.381861
which is R.A. +107.801 Decl. +22.449
missing R.A. +112.288 Decl. +21.828 (ibex-sun)
error is R.A. +4.487 Decl. +0.621
for a total 4.202 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 -0.321566,0.872816,0.367134 -w ibex-sun -t 2017/07:13:02:56:50
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.321566,+0.872816,+0.367134
which is R.A. +110.225 Decl. +21.539
missing R.A. +112.362 Decl. +21.819 (ibex-sun)
error is R.A. +2.137 Decl. +0.280
for a total 2.006 deg
ibex_rotate -o -u -0.321566,0.872816,0.367134 -w ibex-sun -t 2017/07:13:04:31:56
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.321566,+0.872816,+0.367134
which is R.A. +110.225 Decl. +21.539
missing R.A. +112.431 Decl. +21.810 (ibex-sun)
error is R.A. +2.206 Decl. +0.271
for a total 2.067 deg
ibex_rotate -o -u -0.321566,0.872816,0.367134 -w ibex-sun -t 2017/07:17:14:13:00
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.321566,+0.872816,+0.367134
which is R.A. +110.225 Decl. +21.539
missing R.A. +116.924 Decl. +21.155 (ibex-sun)
error is R.A. +6.699 Decl. +0.384
for a total 6.251 deg
The inertial precession maneuver at perigee leaves us pointing in safe directions at the time of the maneuver and at orbit 374 apogee:
ibex_rotate -o -u -0.393433,0.847229,0.35695 -w ibex-sun -t 2017/07:17:16:26:56
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.393433,+0.847229,+0.356950
which is R.A. +114.909 Decl. +20.913
missing R.A. +117.013 Decl. +21.138 (ibex-sun)
error is R.A. +2.104 Decl. +0.225
for a total 1.977 deg
ibex_rotate -o -u -0.393433,0.847229,0.35695 -w ibex-sun -t 2017-07-22T17:36:35.558Z
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.393433,+0.847229,+0.356950
which is R.A. +114.909 Decl. +20.913
missing R.A. +122.014 Decl. +20.160 (ibex-sun)
error is R.A. +7.105 Decl. +0.753
for a total 6.696 deg
No Lo O-mode.
There is no overlap with orbit 372 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# 373.
Please respond to this email thread with your comments and approvals
Approvals are required before 28 Jun 17 @2100 UTC
Note the following:
1. OEF Generation
Because there was a PERIGEE sun maneuver in Orbit# 372, PERIGEE in Orbit# 371 was used to
generate the OEF
2. Battery Balancing at PERIGEE
Orbit# 373 PERIGEE: Battery Balancing Commands
# 2017-07-18T02:02:42.120Z,Perigee,orbit:373
SetLongEclipseFlag TRUE $TIME=2017/07:18:01:00:00
SetLongEclipseFlag FALSE $TIME=2017/07:18:02:30:00
3. Moon in Lo FOV Commands
# 2017-07-12T06:58:20.524Z,MoonInLoFovStart,orbit:373
# 2017-07-13T08:13:28.981Z,MoonInLoFovStop,orbit:373
Sheral R. Wesley
Sr Systems Engineer
IBEX Mission OPS
CRS/CYGNUS Mission Planning
Bldg. 2 Room 1337
Office (703) 406-5641
Cell (202) 236-0802