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am1weekly_2003-200_2003-206

Mission Operations Days: 2003/200 to 2003/206
July 19, 2003 00:00:00 GMT to July 25, 2003 00:00:00 GMT


Terra Spacecraft and MODIS Instrument Status:

AM-1 "Terra" is in Normal Mode
PFM MODIS is in A-Side Nominal Science Mode
(Cross Strapped with FR B)
Component State(s) Comment
Blackbody A On (290K); B Off Nominal Science Mode
Calibration Electronics A On; B Off Nominal Science Mode
Control Processor A On; B Off Nominal Science Mode
Nadir Door Unlatched, Open Nominal Science Mode
Space View Door Unlatched, Open Nominal Science Mode
Solar Diffuser Door Unlatched, Screened New permanent configuration
FDDI Formatter A On; B Off Nominal Science Mode
FDDI Port A On; B Off Nominal Science Mode
FIFO Memory #1 & #2 On; #3 & #4 Off Nominal Science Mode
Format Processor A Off; B On Nominal Science Mode
Power Supplies #1 On, #2 Off Nominal Science Mode
PV VIS FPA A On; B Off Nominal Science Mode
PV NIR FPA A On; B Off Nominal Science Mode
PV SMIR FPA A On; B Off Nominal Science Mode
PV LWIR FPA A On; B Off Nominal Science Mode
PC LWIR FPA A On; B Off Nominal Science Mode
RC Outgas Heaters All 3 (CS, IS, OS) Off Nominal Science Mode
RC LWIR FPA Heater On (83K) Nominal Science Mode
RC SMIR FPA Heater Off Nominal Science Mode
Scan Assembly A On; B Off Nominal Science Mode
SDSM Off Nominal Science Mode
SRCA Off Nominal Science Mode
PS1 Survival Heater Enabled Nominal Science Mode
PS2 Survival Heater Enabled Nominal Science Mode
Timing Generator A On; B Off Nominal Science Mode
Flight Software Rev BD + 11 sets of patches
  • CP07 to Survival Mode - No SDD to closed command (1 patch)
  • CP07 to Safe Mode - No FR OFF Command (1 patch)
  • CP07 to Safe Mode - No SDD to closed command (1 patch)
  • CP07 to Science Mode - Turn on FRB instead of FRA (1 patch)
  • CP07 to Outgas and Science Mode - Turn on FRB instead of FRA (1 patch)
  • FR Error Counting and Statistics (2 patches)
  • FR 1000ms time code patches (3 patches)
  • FR Band 5 Gain Change (20 commands)
  • FR BB Ideal Output Values (1 patch)
  • FR A EEPROM KME Fast 1 word patch (1 patch)
  • FR B EEPROM KME Fast 1 word patch (1 patch)
Nominal Science Mode
Inhibit Ids Set none Nominal Science Mode
TMON 66 Disabled Nominal Science Mode
TMON 67 Disabled Nominal Science Mode
TMON 68 Enabled Nominal Science Mode
TMON 69 Disabled Nominal Science Mode

This Week’s Completed MODIS Activities:

Saturday, July 19, 2003

None

Sunday, July 20, 2003

None

Monday, July 21, 2003

None

Tuesday, July 22, 2003

2003/203 21:26:31-21:35:19 ATC MOD_OA16_SDSM_SCRN_NO_DOOR_A.4 OA16: SD/SDSM Screened - A Side, No Door Movement

Wednesday, July 23, 2003

2003/204 09:00:00 ATC MOD_OA26_BB_270K_A.1 Set blackbody temperature to 270K on the A Side

Thursday, July 24, 2003

2003/205 03:00:00 ATC MOD_OA26_BB_280K_A.1 Set blackbody temperature to 280K on the A Side
2003/205 07:00:00 ATC MOD_OA26_BB_285K_A.1 Set blackbody temperature to 285K on the A Side
2003/205 10:00:00 ATC MOD_OA26_BB_290K_A.1 Set blackbody temperature to 290K on the A Side
2003/205 14:00:00 ATC MOD_OA26_BB_315K_A.1 Set blackbody temperature to 315K on the A Side
2003/205 14:00:30 ATC MOD_OA26_BB_DCYCLE_FULL.1 Set blackbody heater duty cycle to FULL
2003/205 17:00:00 ATC MOD_OA26_BB_270K_A.1 Set blackbody temperature to 270K on the A Side
2003/205 17:00:30 ATC MOD_OA26_BB_DCYCLE_THIRD.1 Set blackbody heater duty cycle to THIRD

Friday, July 25, 2003

2003/206 13:00:00 ATC MOD_OA26_BB_290K_A.1 Set blackbody temperature to 290K on the A Side

This Week’s Scheduled MODIS Activities Not Completed:

None

Upcoming MODIS Events:

July calibrations will include weekly SDSM, an SRCA Full Radiometric, semi-monthly SRCA 10 Watt radiometric, an SRCA Full Spatial, an SRCA Full Spectral, a blackbody heating, and a lunar roll calibration.

Saturday, July 26, 2003

None

Sunday, July 27, 2003

None

Monday, July 28, 2003

2003/209 15:01:02-15:52:40 ATC MOD_OA22_SRCA_FULL_SPECT_1A.4 OA-22: SRCA Full Spectral Calibration Part 1 - A Side
Data Collect Centered on S/C Night (15:19:26-15:53:30)
2003/209 16:56:29-17:31:13 ATC MOD_OA22_SRCA_FULL_SPECT_2A.4 OA-22: SRCA Full Spectral Calibration Part 2 - A Side
Data Collect Centered on S/C Night (16:58:19-17:32:23)
2003/209 18:18:43-19:09:59 ATC MOD_OA22_SRCA_FULL_SPECT_3A.4 OA-22: SRCA Full Spectral Calibration Part 3 - A Side
Data Collect Centered on S/C Night (18:37:13-19:11:16)
2003/209 20:12:40-20:50:37 ATC MOD_OA22_SRCA_FULL_SPECT_4A.3 OA-22: SRCA Full Spectral Calibration Part 4 - A Side
Data Collect Centered on S/C Night (20:16:07-20:50:09)

Tuesday, July 29, 2003

Contingency for Terra Inclination Maneuver; the commands in this activity are inhibited.
2003/210 14:56:13-14:57:54 MOD_CLOSE_NAD_SVD.1 (101 seconds prior to S/C day, orbit 19211)

2003/210 21:33:09-21:41:47 ATC MOD_OA16_SDSM_SCRN_NO_DOOR_A.4 OA16: SD/SDSM Screened - A Side, No Door Movement
2003/210 22:30:24-23:03:55 ATC MOD_OA19_SRCA_FULL_RAD_A.3 OA-19: SRCA Full Radiometric Calibration - A Side
Data Collect Centered on S/C Night (22:38:20-23:12:23)

Wednesday, July 30, 2003

2002/211 21:22:52-22:20:22 ATC MOD_OA23_SRCA_FULL_SPAT_A.2 OA-23: SRCA Full Spatial Calibration - A Side
Data Collect Centered on S/C Night (21:42:48-22:16:50)

Thursday, July 31, 2003

Contingency for Terra Inclination Maneuver; the commands in this activity are inhibited.
2003/212 16:22:54-16:24:35 MOD_CLOSE_NAD_SVD.1 (101 seconds prior to S/C day, orbit 19241)

Friday, August 1, 2003

None

Maneuvers:

The next MODIS lunar calibration will be on August 168, 2003 (DOY 2003/228). Data collection will be from 19:24:54 -19:31:24 GMT, and the roll angle will be -5.1828 degrees.

Three Terra inclination maneuvers were originally planned for July 8, August 5, and August 7, 2003. For each inclination maneuver, a contingency activity will be scheduled in the stored command load to close the MODIS Space View and Nadir doors prior to entering daylight following the maneuver, but the commands will be inhibited after the spacecraft successfully returns to a nominal attitude. See below for a report of the progress of the Inclination Maneuvers.

The July 8, 2003 (DOY 2003/189) Terra Inclination Maneuver was postponed. The cause was the unavailable TDRS Coverage for the maneuver contact. TDRS 275 had gone into safe mode the previous day, limiting contact coverage. The Inclination Maneuver was rescheduled to July 10, 2003 (DOY 2003/191).

The July 10, 2003 (DOY 2003/191) Terra Inclination Maneuver was aborted. The cause was the CRP (Command Return Processor) Unix machine rebooted itself just before the burn. Command and Telemetry data was lost for about 5 minutes while the CRP was restarting. Once the CRP was restarted there was not enough time to do the real time commanding. The stored commands then slewed the spacecraft back to its nominal pointing. The Inclination Maneuver was rescheduled to July 16, 2003 (DOY 2003/197).

The times of the low fidelity pointing and yaw period for DOY 2003/192 are listed below.

2003/191 14:02:00 Low Fidelity Pointing
2003/191 15:33:45 -90 degree Yaw Start
2003/191 16:03:29 +90 degree Yaw End
2003/191 17:35:00 High Fidelity Pointing

The July 16, 2003 (DOY 2003/197) Terra Inclination Maneuver was postponed. ASTER was not in the correct mode for maneuver. ASTER is usually in a Standby Mode throughout maneuvers but this time there were calibrations and other activities for ASTER in the ATC during the planned maneuver timeframe. The ASTER Team indicated that they were ok to still perform maneuver as is. The FOT Leads, however, felt that was an unknown and unnecessary risk. This would have been the first time ASTER performed any activities while the spacecraft was in Thruster Control. Also, the TIR CPHTS is known to become somewhat unstable during burns (especially long duration burns like the Inclination). The ASTER activities would have performed a TIR short- term calibration while the CPHTS loop was most unstable. Initial thoughts are that this would have help in the stability of the loop, but this was not evaluated. The other choice was to Inhibit ASTER Commands for the Maneuver. The only problem with that plan is ASTER would not be able to return to nominal operations until the next ATC load started executing (best case 8 hours, worst case and probably more likely 32 hours) without taking observations. Weighing the risks, the FOT postponed the maneuver. There currently is no rescheduled date for the maneuver.

The Flight Software Inhibit IDs 34 and 58, which inhibit MODIS Door Power and Movements in ATC Loads, were set on DOY 2003/197 (as planned for the Inclination). Since no nominal Terra door movements via ATC Loads are planned in the future, the IDs were left set. They will be left set until they are cleared during the next rescheduled Inclination Maneuver (date of maneuver to be determined).

The two additional Terra inclination maneuvers that were planned for August 5, 2003 and August 7, 2003 have been rescheduled to July 29, 2003 and July 31, 2003.

Terra will perform a Drag Make Up (DMU) Maneuver on Tuesday, July 22, 2003 (DOY 2003/203) at 17:43:09 GMT.

MODIS Anomalies:

None

General Instrument Comments:

MODIS is in Science Mode, using all A-side components, but cross-strapped to Formatter B, with the blackbody maintained at 290K and the Solar Diffuser Door at the Screened position.

MODIS Telemetry Trends:

Nominal telemetry trending is ongoing.

Non-MODIS Significant Events:

The EMOS mission status webpage (which includes instrument data loss records) can be found at the following URL. Note that a password is now required to access the EOS mission links web pages. There are directions at the URL below for how to obtain a username/password.

http://jupiter02.gsfc.nasa.gov/links/links.htm

Limited Life Item Status:

SRCA 10W Lamp #1: 213.6 of 500 hours
SRCA 10W Lamp #2: 159.5 of 500 hours
SRCA 10W Lamp #3: 168.7 of 500 hours
SRCA 10W Lamp #4: 62.2 of 500 hours

SRCA 1W Lamp #1: 562.0 of 4000 hours
SRCA 1W Lamp #2: 276.7 of 4000 hours

Solar Diffuser Door: 2146 of 3022 Movements
Nadir Aperture Door: 536 of 1316 Movements
Space View Door: 439 of 1316 Movements