[Isocops] IBEX Orbit #267 ATS (Nov 18 - 26) Part 2

Marty Quinn martyq92 at gmail.com
Thu Nov 6 14:12:58 EST 2014


Hi All,

I approve orbit 267 ATS. Command Approval Checklist is attached. There is
no battery cell balancing and no Moon in FOV this orbit.

---------------------------------------------------------
ibex_orbit position times are in sync with the Command Checklist times.
---------------------------------------------------------
[msq at ena ibexops]$ ibex_orbit -r 267 -D apogee -R E
0267
2014/11:22:11:44:43 1980/01:06:00:00:00

[msq at ena ibexops]$ ibex_orbit -r 267 -D perigee -R E
0267
2014/11:27:00:33:08 1980/01:06:00:00:00

[msq at ena ibexops]$ ibex_orbit -r 267 -D 14 -R E
0267
2014/11:18:08:36:30 2014/11:26:14:33:32

[msq at ena ibexops]$ ibex_orbit -r 267 -D 15 -R E
0267
2014/11:18:10:15:08 2014/11:26:12:56:09

---------------------------------------------------------
Spacecraft pointing positions for Orbit 267.
---------------------------------------------------------
Perigee Orbit 266 pointing:
 ibex_rotate -o -u -0.604779,-0.726703,-0.325799 -w ibex-sun -t
2014/11:17:13:22:28
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
 points axis  +1.000000,+0.000000,+0.000000
 towards ECI  -0.604779,-0.726703,-0.325799
 which is     R.A. +230.232 Decl. -19.014
 missing      R.A. +232.563 Decl. -18.983 (ibex-sun)
 error is     R.A.   +2.331 Decl.  +0.031
 for a total  2.204 deg



#At beginning of Orbit 267 ascending Arc A
ibex_rotate -o -u -0.604779,-0.726703,-0.325799 -w ibex-sun -t
2014/11:18:10:15:10
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
 points axis  +1.000000,+0.000000,+0.000000
 towards ECI  -0.604779,-0.726703,-0.325799
 which is     R.A. +230.232 Decl. -19.014
 missing      R.A. +233.474 Decl. -19.212 (ibex-sun)
 error is     R.A.   +3.242 Decl.  +0.198
 for a total  3.070 deg


#At end of descending Arc A
ibex_rotate -o -u -0.604779,-0.726703,-0.325799 -w ibex-sun -t
2014/11:22:00:10:47
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
 points axis  +1.000000,+0.000000,+0.000000
 towards ECI  -0.604779,-0.726703,-0.325799
 which is     R.A. +230.232 Decl. -19.014
 missing      R.A. +237.082 Decl. -20.032 (ibex-sun)
 error is     R.A.   +6.850 Decl.  +1.019
 for a total  6.535 deg

#Apogee Orbit 267 pointing:
ibex_rotate -o -u -0.538608,-0.768955,-0.344397 -w ibex-sun -t
2014/11:22:01:53:55
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
 points axis  +1.000000,+0.000000,+0.000000
 towards ECI  -0.538608,-0.768955,-0.344397
 which is     R.A. +234.991 Decl. -20.145
 missing      R.A. +237.156 Decl. -20.048 (ibex-sun)
 error is     R.A.   +2.165 Decl.  +0.097
 for a total  2.035 deg

#At beginning of ascending Arc B
ibex_rotate -o -u -0.538608,-0.768955,-0.344397 -w ibex-sun -t
2014/11:22:03:29:01
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
 points axis  +1.000000,+0.000000,+0.000000
 towards ECI  -0.538608,-0.768955,-0.344397
 which is     R.A. +234.991 Decl. -20.145
 missing      R.A. +237.224 Decl. -20.062 (ibex-sun)
 error is     R.A.   +2.233 Decl.  +0.083
 for a total  2.099 deg

#At end of descending Arc B
ibex_rotate -o -u -0.538608,-0.768955,-0.344397 -w ibex-sun -t
2014/11:26:12:53:01
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
 points axis  +1.000000,+0.000000,+0.000000
 towards ECI  -0.538608,-0.768955,-0.344397
 which is     R.A. +234.991 Decl. -20.145
 missing      R.A. +241.975 Decl. -20.931 (ibex-sun)
 error is     R.A.   +6.984 Decl.  +0.786
 for a total  6.587 deg

#Perigee Orbit 267 pointing:
ibex_rotate -o -u -0.470294,-0.805716,-0.360062 -w ibex-sun -t
2014/11:26:15:12:37
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
 points axis  +1.000000,+0.000000,+0.000000
 towards ECI  -0.470294,-0.805716,-0.360062
 which is     R.A. +239.728 Decl. -21.104
 missing      R.A. +242.087 Decl. -20.950 (ibex-sun)
 error is     R.A.   +2.358 Decl.  +0.154
 for a total  2.207 deg


Regards,

Marty



Marty Quinn
GISLAB/Space Science Center UNH
marty.quinn at unh.edu <marty at drsrl.com>
603 988-7107

On Wed, Nov 5, 2014 at 9:26 AM, Tim Perry <Perry.Tim at orbital.com> wrote:

>
>
> All,
>    Here are the planning files and ATS for Orbit# 267 Version 2. Since I
> found that I had used the forecast OEF to generate the 267 OEF vs using the
> 266 OEF
> I felt it would be easier to just rerun the 267 products. So here are the
> Version 2 products.
> Since Sheral is on vacation I also filled out the ATS checklist for
> Orbit#267.
> Please respond to this email thread with questions, comments and approvals.
> Approvals are required before COB 6 Nov 14.
>    Thanks
>        Tim
>
>
> # Filename:            IBEX_2014_321_o0267a_v002.ccvr
> # File type:           Command Load Constraint Violation Report (CCVR)
> #
> # Create time:         2014/309.133754
> # Plan period start:   2014/322.103100
> # Plan period stop:    2014/331.103000
> # Default time format: UTC
> #
> # Input files:         1
> #   IBEX_2014_321_o0267a_v002.scr
>
> ==========================
> HARD CONSTRAINT VIOLATIONS
> ==========================
> NO VIOLATIONS.
>
> ==========================
> SOFT CONSTRAINT VIOLATIONS
> ==========================
> NO VIOLATIONS.
>
> ==============
> OTHER MESSAGES
> ==============
> NO MESSAGES.
>
> (See attached file: IBEX_2014_321_o0267a_v002.txt)(See attached file:
> IBEX_Sch_Req2014_Orbit267_v002.txt)(See attached file:
> IBEX_2014_321_o0267a_v002.oef)(See attached file:
> IBEX_2014_321_o0267a_v002.ccvr)(See attached file:
> IBEX-Command-Approval-Checklist-Rev14_267_TEP_V2.docx)
> Timothy E. Perry
> CYGNUS Mission Planning
> IBEX Mission Ops Lead
> perry.tim at orbital.com
> Office: (703) 406-5976
> Cell:(301) 606-1430
>
>
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