[Isocops] IBEX Orbit# 319 ATS Approval - v002 approval

Ken Fairchild fair-play at comcast.net
Wed Feb 24 23:22:43 EST 2016


All, 

Note: Off-pointing at arc B descending is 3.902 deg 
Off-pointing at orbit 320 apogee is 5.076 deg 

I have looked at the orbit 319 recovery ATS, 



IBEX_2016_065_o0319a_Recovery_v002.scr , 



and I approve. 



The only constraint violations in 



IBEX_2016_065_o0319a_Recovery_v001.ccvr 



are related to long contacts and the orbit 318 eclipse and are expected. 



The PL commands in the v002 ATS match those in the v002 STF, 



IBEX_2016_065_o0319a_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_2016_065_o0319a_Recovery_v001.oef, 



and as verified with ibex_orbit. 



There is one star tracker outage. It starts 1 1/2+ days after apogee and runs for almost 2 days. Some despinning may be required due to this outage. 



There is one moon in Lo FOV session in arc B. The ATS start time is about 6 hours before that in the OEF and the ATS end time is about 4 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_Orbit319_RecoveryContacts.txt, 



for all contacts in the ATS (2). The commands for the APL contact will be in a separate ATS. 



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 318 left us pointing in safe directions for the orbit 319 arc A ascending and descending sequences: 



ibex_rotate -o -r +345.534 -d -6.164 -w ibex-sun -t 2016/03:05:14:26:02 

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

points axis +1.000000,+0.000000,+0.000000 

towards ECI +0.962698,-0.248361,-0.107375 

which is R.A. +345.534 Decl. -6.164 

missing R.A. +346.424 Decl. -5.825 (ibex-sun) 

error is R.A. +0.890 Decl. +0.339 

for a total 0.948 deg 



ibex_rotate -o -r +345.534 -d -6.164 -w ibex-sun -t 2016/03:09:12:08:22 

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

points axis +1.000000,+0.000000,+0.000000 

towards ECI +0.962698,-0.248361,-0.107375 

which is R.A. +345.534 Decl. -6.164 

missing R.A. +350.098 Decl. -4.297 (ibex-sun) 

error is R.A. +4.564 Decl. +1.867 

for a total 4.913 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 +350.166 -d -4.267 -w ibex-sun -t 2016/03:09:13:56:30 

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

points axis +1.000000,+0.000000,+0.000000 

towards ECI +0.982576,-0.170321,-0.074404 

which is R.A. +350.166 Decl. -4.267 

missing R.A. +350.166 Decl. -4.267 (ibex-sun) 

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

for a total 0.000 deg 




ibex_rotate -o -r +350.166 -d -4.267 -w ibex-sun -t 2016/03:09:15:26:36 

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

points axis +1.000000,+0.000000,+0.000000 

towards ECI +0.982576,-0.170321,-0.074404 

which is R.A. +350.166 Decl. -4.267 

missing R.A. +350.223 Decl. -4.242 (ibex-sun) 

error is R.A. +0.057 Decl. +0.025 

for a total 0.062 deg 



ibex_rotate -o -r +350.166 -d -4.267 -w ibex-sun -t 2016/03:13:14:13:49 

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

points axis +1.000000,+0.000000,+0.000000 

towards ECI +0.982576,-0.170321,-0.074404 

which is R.A. +350.166 Decl. -4.267 

missing R.A. +353.742 Decl. -2.688 (ibex-sun) 

error is R.A. +3.576 Decl. +1.579 

for a total 3.902 deg 



The sun precession maneuver at perigee leaves us pointing in safe directions at the time of the maneuver and at orbit 320 apogee: 



ibex_rotate -o -r +353.833 -d -2.650 -w ibex-sun -t 2016/03:13:16:38:41 

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

points axis +1.000000,+0.000000,+0.000000 

towards ECI +0.993150,-0.107312,-0.046235 

which is R.A. +353.833 Decl. -2.650 

missing R.A. +353.833 Decl. -2.650 (ibex-sun) 

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

for a total 0.001 deg 



ibex_rotate -o -r +353.833 -d -2.650 -w ibex-sun -t 2016-03-18T16:08:47.925Z 

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

points axis +1.000000,+0.000000,+0.000000 

towards ECI +0.993150,-0.107312,-0.046235 

which is R.A. +353.833 Decl. -2.650 

missing R.A. +358.513 Decl. -0.678 (ibex-sun) 

error is R.A. +4.680 Decl. +1.972 

for a total 5.076 deg 



No Lo O-mode. 



The transmitter off command from the last contact in orbit 318 occurs after the ascending bus commands in the orbit 319 ATS. 



Command Approval Checklist is attached. 



Ken 

----- Original Message -----

From: "Wesley.Sheral" <sheral.wesley at orbitalatk.com> 
To: "Stephen Lutz" <stephen.lutz at applieddefense.com>, "David Heirtzler" <dheirtzl at atlas.sr.unh.edu>, "IBEX-FDG" <IBEX.fdg at applieddefense.com>, "IBEXOPS" <IBEXOPS at gmail.com>, "ISOC" <isocops at lists.sr.unh.edu>, "Ken Fairchild" <fair-play at comcast.net>, "Lockwood.Robert" <robert.lockwood at orbitalatk.com>, "Michelle Reno" <mreno at swri.edu>, "Nigel Angold" <nigel.angold at nasa.gov>, "Paul Janzen" <paul.janzen at umontana.edu>, "Perry.Tim" <tim.perry at orbitalatk.com>, "Tyler.Ryan" <ryan.tyler at orbitalatk.com>, "Wesley.Sheral" <sheral.wesley at orbitalatk.com> 
Sent: Saturday, February 20, 2016 6:15:53 PM 
Subject: IBEX Orbit# 319 ATS Approval 



Guys, 

Here are the planning files and ATS for Orbit# 319. 

Comments and approvals are required before 24 Feb 16 @1200 UTC 



Note the following: 

1. Apogee and Perigee Sun Maneuvers 

2. Perigee Battery Balancing 

Orbit # 319 PERIGEE: Battery Balancing Commands 

# 2016-03-14T01:58:28.407Z,Perigee,orbit:319 

SetLongEclipseFlag TRUE $TIME=2016/03:14:01:00:00 

SetLongEclipseFlag FALSE $TIME=2016/03:14:02:30:00 



3. APL-18 Contact commands will be uploaded later 

4. 1 hour contacts until we have recovered from Star Tracker Anomaly 

5. Command Load Constraint Violation Report 

IBEX_2016_065_o0319a_Recovery_v001.scr 



========================== 

HARD CONSTRAINT VIOLATIONS 

========================== 

NO VIOLATIONS. 



========================== 

SOFT CONSTRAINT VIOLATIONS 

========================== 

IBX-CLC-006: Planned transmission at 2016/03/05 12:55:00 UTC - 2016/03/10 

15:28:00 UTC exceeds the maximum contiguous transmission time of 

5400 seconds 

IBX-CLC-006: Planned transmission at 2016/03/10 15:28:00 UTC - 2016/03/10 

16:32:00 UTC is preceded by one or more additional transmissions 

which, when combined, exceed the maximum transmission time of 5400 

seconds within a 18000-second window (total planned transmission 

time this window is 21840.000 seconds) 

IBX-CLC-015: Battery charge falls below minimum from 2016/03/05 17:26:14 UTC - 

2016/03/10 22:09:00 UTC. Lowest charge level is 0.000000 

watt-minutes during this interval. 



============== 

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 







------------------------------------------------------------------------------ 

Notice: This e-mail is intended solely for use of the individual or entity to which it is addressed and may contain information that is proprietary, privileged and exempt from disclosure under applicable law. If the reader is not the intended recipient or agent responsible for delivering the message to the intended recipient, you are hereby notified that any dissemination, distribution or copying of this communication is strictly prohibited. This communication may also contain data subject to U.S. export laws. If so, that data subject to the International Traffic in Arms Regulation cannot be disseminated, distributed or copied to foreign nationals, residing in the U.S. or abroad, absent the express prior approval of the U.S. Department of State. If you have received this communication in error, please notify the sender by reply e-mail and destroy the e-mail message and any physical copies made of the communication. Thank you. 
********** ********** 

-------------- next part --------------
An HTML attachment was scrubbed...
URL: http://lists.sr.unh.edu/pipermail/isocops/attachments/20160225/0a8a7b22/attachment-0001.html 
-------------- next part --------------
A non-text attachment was scrubbed...
Name: image001.jpg
Type: image/jpeg
Size: 2392 bytes
Desc: image001.jpg
Url : http://lists.sr.unh.edu/pipermail/isocops/attachments/20160225/0a8a7b22/image001-0001.jpg 
-------------- next part --------------
A non-text attachment was scrubbed...
Name: IBEX-Command-Approval-Checklist-Rev15-o0319-recovery_KWF.doc
Type: application/msword
Size: 121856 bytes
Desc: not available
Url : http://lists.sr.unh.edu/pipermail/isocops/attachments/20160225/0a8a7b22/IBEX-Command-Approval-Checklist-Rev15-o0319-recovery_KWF-0001.doc 


More information about the Isocops mailing list