******************************************************************** UARS WEEKLY STATUS REPORT - 31 OCTOBER 1997 ******************************************************************** *********** SOLSTICE *********** SOLSTICE continues to operate normally, collecting solar data on all available orbital tracking periods and stellar calibration observations, whenever possible. *********** SUSIM *********** SUSIM was successfully repowered on October 27. Since then, it has gathered its normal solar data without apparent problems. The SUSIM team would like to thank Barbara Holt for her diligent and kindly efforts on behalf of the UARS project. We will miss her. Best of luck, Barb! *********** PEM *********** Nothing received. *********** HALOE *********** HALOE was successfully operating when is was powered off end-of-day October 30, 1997. All engineering parameters were within nominal operating range and the science data products continue to be of excellent quality. *********** MLS *********** MLS was reactivated successfully on Oct 20, in the reduced 85 watt power mode. Full vertical scans were performed Oct 21 thru Oct 25. MLS was powered off on Oct 25 at 23:12 UT. MLS is scheduled to resume south viewing operations on Oct 31. Software for producing the new MLS upper tropospheric humidity product has been delivered to the CDHF, and is now undergoing final tests before being put into production. Humidity is retrieved at UARS pressure surfaces of 147, 215, 316 and 464 hPa. *********** HRDI *********** HRDI is functioning normally, and is planned to be in operation thru the end of Oct. 30. *********** WINDII *********** WINDII is currently off. Initiation of the production under our new Version 5 has been delayed by a number of details that have required attention, but nearly all have been resolved now, and implementation is expected within a few weeks. *********** MPG *********** Routine processing of instrument Daily Activity Plans continues with no problems. The MPG continues to assist the Project Scientist with the scheduling of instrument operations. Personnel change: Barb Holt is leaving the UARS Mission Planning Group to move to a position with Applied Physics Laboratory. *********** CDHF *********** The CDHF received 339 CD-ROM requests as of 31-October-1997. Two new CD-ROM orders were received this week. The CDHF has completed the reprocessing of Extracted Attitude to generate new SSPP files. The CDHF processed current day data through level 3 for all active instruments. Additionally, CDHF personnel reprocessed: (R)= Requested (C) = Complete, (F)= Failed (L) = Days remaining to reprocess. 25 days PEM (3.32) Prod (1350R-510C=840L) 29 days ATT (6.1) Prod (1321R-1321C=0L) MLS (4.9) Engineering in progress The CDHF has completed the preview and load of August 1997 current day data to the DAAC. Pending CDHF software upgrades include IDL 5.0, and OpenIngres 2.0. *********** FOT *********** REPORTING PERIOD This report covers the 17 October 1997 (Orbit 33338, GMT Day 290).through 24 October 1997 (Orbit 33443, GMT Day 298). SPACECRAFT OPERATION The observatory is now in Forward Flight (Southern Hemisphere viewing) and is performing nominally under two-battery operations. The instrument operational changes were: INSTRUMENT OPERATIONAL CHANGES Instrument Time Orbit Comment HRDI 292/2321 33368 Off ACRIM 292/2321 33368 Off SUSIM 292/2321 33368 Off MLS 293/1810 33380 Start Activation MLS 293/2129 33382 Activation Complete The beta angle reached a maximum angle of 46 degrees on 21 October 1997 (DOY 294). The beta angle is now decreasing toward a minimum angle of 0 degrees on 07 November 1997 (DOY 311). Spacecraft battery 1, 2, and 3 performance monitoring continues. Battery 1 remains OFF the charge relay. Battery 2 and Battery 3 are currently maintaining greater than 24.5 end-of-night (EON) load bus voltage. Battery temperatures are stable with a temperature delta between Battery 2 and Battery 3 of 1.1 degrees C. Additional battery performance data for each battery on 18 October 1997 and 24 October 1997 are provided in Appendix D. The clock error ranged from -10.2 to +11.5 msec during this report period. Clock rate adjustments are listed in Appendix C. All instrument and subsystem engineers were advised on the initial excursion of ALERTS or Out-Of-Limits conditions detected by the FOT for this report. A summary is listed below and the details of ALERT and Out-Of-Limits occurrences are listed in Appendix B. % ALERTS = 01 % OUT-OF-LIMITS = 15 The following real-time command sheets were executed for the listed operational element(s) during this report period (see Appendix A). % FOT 04 % ACRIM/SUSIM 01 % HRDI 01 % MLS 01 % SUSIM/CH 03 UARS Anomaly Reports initiated during this report period are listed in Appendix E and summarized below. % FOT 03 TRANSPONDER FREQUENCIES: Transponder A: 97/287 - 2287.496931 Transponder B: 97/295 - 2287.499126 GROUND SYSTEM OPERATION Three (3) operational support problem(s) occurred this period. Anomaly Reports are included in Appendix E. The data loss calculations supplied by Data Capture Facility (DCF) from mission start through UTC Day 97/296 show the observatory data loss to be 20 hours, 41 minutes, 03.981 seconds (an increase of 5 minutes and 40.256 seconds). This is a 0.0388 percent data loss which equals a 99.9612 percent data capture for the mission. The increase of 1.216 seconds occurred over four (4) days: % 1.504 seconds on Day 290 due to insufficient overlap, % 1 minute and 42.752 seconds on Day 291 due to insufficient overlap and an unknown reason, % 3 minutes and 48.192 seconds on Day 292 due to White Sands fail-over, and % 7.808 seconds on Day 294 due to data not recorded. FOT level-0 processing software was tested on the Central Data Handling Facility (CDHF) using files generated by the new Level Zero (LZPR). The LZPR files were processed successfully. Verified functionality of File Transfer Protocol (FTP) options on the UMPG Alpha computer following the installation of Multinet software. The only remaining problem with the UMPG Alpha is the unavailability of Tektronix print support (license pending). Once the Tektronix print driver is installed, the UMPG Alpha (node UMPGAL) will replace UMPG0 (the existing UMPG VAX node) as the operational machine. No testing of the new CMS software release (R7B1V2) occurred this week. The FOT currently does not have a workstation hooked up to the back-up UCMS system (UCMSB), where the new software currently resides in a test environment. FOT investigated the status of the conversion device(s) (CD) located in MSOCC operations area. Apparently, there are some problems with the CDs processing GCMR(s) together with telemetry but UARS can still use them to test receipt of return link telemetry. However, since the FOT is currently operating out of the temporary control center, it may be difficult to configure a parallel test which would require extra terminals connected to the AP system that will receive the IP data. Investigation of the stored command verification problem - time to complete - associated with Applications Processor (AP) software release 10.08 continued. The cause has been identified but rectifying the problem continues. Repercussions of relocating the UCMS and the UCMSB from one side of the control center to the other continued this week. Apparently during the relocation, the lines which connect each system to the CDHF were inadvertently reversed, and the line which was previously connected to UCMSB became connected to the UCMS (and vice versa). This in itself is not a problem except for the fact that the old UCMSB line is apparently RflakyS and works intermittently. After the line problem was noticed, the hardware maintenance personnel and the CMS system managers restored the lines to their original configuration. OTHER SIGNIFICANT EVENTS Monitoring of the magnetic field model performance continues. First, second and third order magnetic field models were generated using MATLAB software. With the graphic capabilities of MATLAB, the progression of the spherical harmonic equations are more easily seen. Procedures were developed to install new flight software patch (revision V62B) to support proper skew wheel speed reversal following the next yaw maneuver. Attempts to test the procedure with the UTTS were unsuccessful due to hardware problems (with the UTTS CDHF rack and the NASCOM line drivers). The task to provide documentation and related information about the UARS CDHF plot software was completed and released in UARS FOT MEMO 97-040, 97-041, and 97-042. FOT continues to develop an updated Power Profile for UARS due to the current status of the Modular Power System. FOT continues to support the new UARS ground system re-engineering effort. The FOT is currently working on providing a floppy disk copy of the current UARS database in ASCII format. Apparently, the database cannot be easily downloaded in an ASCII format from the OBCSTF, so the FOT is working on converting the necessary files using other sources. MEETINGS No UARS Battery telecon was held this week. The next telecon has not been scheduled. FUTURE SIGNIFICANT EVENTS The next UARS Yaw Around Maneuver is currently scheduled for 07 November 1997 at 311/132708. The UARS orbit altitude is dropping slowly and a drag makeup orbit adjust will probably be required in mid-1998. FACILITIES The carpet in the UARS/TOMS Mission Operations Room (MOR) has been replaced and the new semi-circular console is in place. Operations continue from a dedicated room in the EOS area which is across the hall. PERSONNEL CHANGES Rich Calvin, Off-Line Observatory Engineer, submitted his registration effective 03 November 1997 to accept a position with Motorola. Attachments: Appendix A, Real-time Commands Sheets Appendix B, Out-Of-Limits & ALERT Occurrences Appendix C, Clock & Solar Array Rate Corrections Appendix D, UARS Battery Performance Data Appendix E, UARS Anomaly Reports APPENDIX A REAL-TIME COMMAND SHEETS Week ending 24 October 1997 ORBIT AOS NO. SUBSYS REASON ----- --- --- ------ ------- 33349 291/1615 97-519 OBC Clk Adj fr 20.6 to 0.00 msec/day 33368 292/2321 97-520 HRDI Power OFF 33368 292/2321 97-521 ACRIM/SUSIM Power OFF 33370 293/0204 97-522 OBC Clk Adj fr 0.00 to 20.6 msec/day 33382 293/2129 97-523 MLS Power ON 33405 295/1127 97-524 SUSIM/CH RTS To Enable Comp Htr 18 A&B sides 33409 295/1635 97-525 SUSIM/CH RTS To Enable Comp Htr 18A Full-time 33411 295/1957 97-526 SUSIM/CH RTS TO CYCLE CH18A&B ON IN DAYTIME 33417 296/0535 97-527 OBC/CLK Clk Adj fr 20.6 to 0.00 msec/day 33340 297/1825 97-528 OBC Clk Adj fr 0.00 to 20.6 msec/day _______________________________________________________________ APPENDIX B OUT-OF-LIMITS & ALERTS OCCURRENCES Week ending 24 October 1997 The following Out-of-Limit (ALARM) conditions were detected: MNEMONIC STATE DESCRIPTION ORBITS --------- ----- ------------ ------ OBSSOC2 Y-LO Battery 2 Current SOC 33340-33443 SUMEBPBI R-LO SUSIM Pulse Bus Cur 33369-33443 SUMEBQBI R-LO SUSIM Quiet Bus Cur 3369-33443 HRIFESURVTMP Y-HI HRDI IFE Survival Temp 33371,74 QTSISAIF Y-HI SSPP Baseplate by SISA I/F 33376-33443 OBSBATVEON2 Y-LO Battery 2 voltage at EON 33388-33443 OBSBATVEON3 Y-LO Battery 3 voltage at EON 33388-33443 OBSVLBEON Y-LO Load Bus Volts at EON 33385-33443 QTACRIMIF Y-HI SSPP Temp at ACRIM I/F 33399-414 OBSSOC2 R-LO Battery 2 Current SOC 3405-08 OBSVLBEON R-LO Load Bus Volts at EON 33410,18-19,35,38,41,54-55 OBSBATVEON3 R-LO Battery 3 voltage at EON 33410,18-19,31,35,38,40- 41,54-55 QTSSPPMX Y-HI SSPP -X Thermostat 33389-90,405-8 QTSSPPPX Y-HI SSPP +X Thermostat 33405-08,435-6 OBSBATVEON2 R-LO Battery 3 voltage at EON 33410,18-19,24,38,54 The following ALERT occurrences were detected: MNEMONIC DESCRIPTION ORBITS --------- ------------ ------ SOPUPERSTATA SOLSTICE is in an unexpected state 33371-33443 APPENDIX C CLOCK & SOLAR ARRAY RATE CORRECTIONS Week ending 24 October 1997 CLOCK DRIFT RATE ADJUSTMENTS ORBIT TIME CLOCK RATE CHANGE ----- ---- ----------------- 33349 291/16:19 (18 Oct 97) from 20.6 to 00.0 msec/day 33370 293/02:09 (20 Oct 97) from 00.0 to 20.6 msec/day 33417 296/05:39 (23 Oct 97) from 20.6 to 00.0 msec/day 33440 297/18:38 (24 Oct 97) from 00.0 to 20.6 msec/day _______________________________________________________________ APPENDIX D UARS BATTERY PERFORMANCE DATA Week ending 24 October 1997 18 Oct. 1997 - GMT Day 291 Beta = 43.3 deg, SA Pos.= 269 deg DIFF V (mV) TEMP (C) CURR (amp) EON V AVE C/D AVE BAT MAX/MIN MAX/MIN MAX/MIN MIN RATIO DOD(%) --- -------- ------- ---------- ------ ------- ------ 1 +728.0/+728.0 -3.05/-3.99 +0.00/0.00 18.7 0.000 0.00 2 +47.6/-15.4 5.79/4.51 +27.6/-14.9 26.1 1.022 21.5 3 +74.2/-5.60 4.51/3.23 +26.4/-14.9 26.1 1.023 20.7 24 Oct. 1997 - GMT Day 297 Beta = 44.1 deg, SA Pos.= 269 deg DIFF V (mV) TEMP (C) CURR (amp) EON V AVE C/D AVE BAT MAX/MIN MAX/MIN MAX/MIN MIN RATIO DOD(%) --- -------- ------- ---------- ------ ------- ------ 1 +728.0/+728.0 -2.69/-3.68 +0.00/0.00 18.7 0.000 0.00 2 +79.8/+2.80 7.09/5.47 +28.4/-16.0 24.3 1.021 23.3 3 +64.4/-7.00 5.79/4.51 +27.5/-16.1 24.2 1.023 22.6 V/T LEVEL CHANGES ORB# TIME LVL FR-TO ----- -------- ---------- no changes _______________________________________________________________ APPENDIX E UARS ANOMALY REPORTS Week ending 24 October 1997 AR NO. SUBSYS ORBIT TIME TTR PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 97-117 FOT 33360 292/0935 19551 Data Loss/SSA Failover 97-111 FOT 33361 292/1115 14170 Generic Late Acquisition 97-111 FOT 33393 294/1423 14170 Generic Late Acquisition ANOMALY CLOSURE INFORMATION RECEIVED AR NO. SUBSYS ORBIT TIME TTR PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- None this report period ANOMALY INVESTIGATION REPORTS GENERATED AIR NO. SUBSYS ORBIT TIME TTR PROBLEM/DATA LOSS ------- ------ ----- ---- --- ----------------- None this report period