******************************************************************** UARS WEEKLY STATUS REPORT - 13 JUL 2001 ******************************************************************** *********** SOLSTICE *********** Nothing received. *********** SUSIM *********** SUSIM has completed its daily solar scans this past week during periods of predicted UARS telemetry. *********** ACRIM *********** Nothing received. *********** PEM *********** ***** ALL PEM COMMUNICATION SHOULD NOW BE THROUGH THE PEM2K:: NODE ***** The PEM team reports that the PEM:: node computer has failed and has been taken off line. PEM:: appears to have hardware problems that take the system down every few hours. Automatic transfer NRT tests to PEM2K from both CDHF2 and CDHFB have succeed and the NRT files have been verified against those captured by PEM, which confirm the NRT process is correct. Thus, PEM confirms NRT data from CDHFB. Thanks to Steve Bove for his work assisting PEM with this process. PEM/AXIS was activated in its half power mode on June 24 and deactivated on June 27. The PEM/AXIS was reactivated in full power mode on July 3. At the current time, AXIS is not generating energy deposition. SwRI is looking into this. Tests of AXIS production code on the rehost computer are continuing. At the present time, PEM energy deposition from its spectrometers is not being generated. Recent data configuration changes have affected PEM software causing multiple failures. These failures are being reviewed by the PEM team. In order to correct for new telemetry requirements, PEM will need to update processing code with a patch delivery. The delivery patch may include changes which would allow the PEM software to execute on a DEC Alpha machine. GSFC is helping PEM with some DEC Alpha particulars which have caused PEM level 3 code to fail on DEC Alpha machines (software below level 3 executes on the DEC Alpha). Updated HEPS calibration parameters have been finalized and are ready for delivery. Updated MEPS quality calibration files have been finalized and are ready for delivery. Level 3 software errors, discovered by Dr. Dean Pesnell, have been fixed; his suggestions have been incorporated with in the PEM production code. Both updated HEPS and MEPS calibration data, along with the Level 3 code changes, will influence the in-situ energy deposition predictions, so new versions of PEM energy deposition Level 3 files will be generated. *Beginning of power orbit day (PEM activation): array current >5 amps, array voltage >53.5 volts, and battery current >2.0 amps. End of power orbit day (PEM deactivation): time in power orbit day >4 minutes, array current <9 amps, and battery currents <0.2 amps. Power orbit day variation: ~39-40 min at yaw to ~50-51 min at maximum beta. *********** HALOE *********** HALOE continues to operate successfully. All engineering parameters are within nominal operating range. HALOE was powered off at the beginning-of-day today as scheduled. Special calibration sequences were commanded during some sunrise and sunset events to verify instrument alignment and end to end gain. *********** MLS *********** Nothing received. *********** HRDI *********** Nothing received. *********** WINDII *********** Nothing received. *********** MPG *********** Daily processing of instrument Daily Activity Plans continues with no problems. *********** CDHF *********** DAAC DATA: - CLAES (output 9) created in August, 1999 has been loaded to the DAAC Transfer Tables. - UKMO,NMC and HALOE created in May, 1999 has been previewed in preparation for sending to the DAAC. UARS CDHF REHOST: - Current day production processing continues to be processed only on the rehost system and is going well. - NRT was moved July 12 to CDHFB. *********** FOT *********** REPORTING PERIOD This report covers 30 June 2001 (Orbit 53581, GMT Day 181) through 06 July 2001 (Orbit 53685, GMT Day 187). 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 SOLSTICE 182/1138 53603 Power On SUSIM 182/1415 53604 Power On ACRIM 182/2116 53609 Power On PEM 183/2339 53625 AXIS On HALOE 184/2257 53640 Power On The beta angle ranged between the angles of 5.6 degrees to 29.3 degrees for this report period. The beta angle is now increasing towards a maximum angle of 78 degrees on 20 July 2001 (DOY 201). 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 23.8 V end-of-night (EON) load bus voltage. Battery temperatures are stable with a temperature delta between Battery 2 and Battery 3 of 1.2 to 1.6 degrees C. Additional battery performance data for each battery on 29 June 2001 and 6 July 2001 are provided in Appendix D. The clock error ranged from Ð8.9 to 0.6 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. ¥ OUT-OF-LIMITS = 00 ¥ ALERTS = 00 The following real-time command sheets were executed for the listed operational element(s) during this report period (see Appendix A). ¥ FOT = 09 ¥ HALOE = 03 ¥ SOLSTICE = 01 ¥ ACRIM = 01 ¥ SUSIM = 04 ¥ HRDI = 02 ¥ PEM = 02 UARS Anomaly Reports initiated during this report period are listed in Appendix E and summarized below. ¥ HALOE = 01 ¥ FOT = 01 One (1) Anomaly Report remained OPEN at the end of this report period (see Appendix E). TRANSPONDER FREQUENCIES: · Transponder A: 00/316 - 2287.496493 · Transponder B: 01/119 - 2287.499116 GROUND SYSTEM OPERATION Two (2) operational support problems 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 01/186 show the observatory data loss to be 302 hours, 44 minutes, 57.624 seconds. This shows a loss of 1 hour, 04 minutes and 12.784 seconds since the last report period. This is a 0.39 percent data loss, which equals a 99.61 percent data capture for the mission. The increase of 1 hour, 04 minutes and 12.784 seconds occurred over five (5) days: · 1 hour and 40.592 seconds on Day 180 due to Station preserving power for YAW maneuver. --No science data was lost · 2 minutes and 07.488 seconds on Day 181 due to No Data -- Overlap · 37.632 seconds on Day 182 due to a Data Hit · 47.072 seconds on Day 183 due to a Data Hit OTHER SIGNIFICANT EVENTS UARS SATELLITE OPERATIONS An instrument anomaly was experienced on 05 May 2001. The instrument involved was the ACRIM II instrument. All ACRIM telemetry for currents and voltages all dropped to zero values suddenly. The ACRIM team in coordination with the UARSFOT conducted analysis and command tests to determine the cause of the anomaly. Analysis shows that the anomaly was caused by failed circuitry in the ACRIM electronics box. The FOT is awaiting a future plan of action from the ACRIM team. The software test team, in conjunction with the FOT, has completed a large portion of the testing for the new front end processor. The new TAC still has yet to undergo DSN and realtime TDRS testing, but has completed simulations of receipt of telemetry, commanding, and NCC/GCMR testing. DSN testing is scheduled for 18 July 2001. UARSFOT will also begin supporting testing of the rehosted UARS ground system. A prototype system has been built in accordance with the UARS documentation and operational database. A meeting will be held on 10 July to determine the test plan. UARS attitude has been adjusted over the course of the last few yaw cycles by loading new alignment matrices for the TAM. Good alignments have been found for both directions of flight and the performance of the TAM should remain stable and accurate. MEETINGS The FOT held the UARS Three TDRS Kickoff Meeting on 03 July 2001. This meeting was established to track the progress and resolve problems of all entities involved in the implementation of the three TDRS mode. This meeting will become a biweekly meeting until the three TDRS mode is operational. FUTURE SIGNIFICANT EVENTS The next UARS Yaw slew is scheduled for 08 August 2001 (DOY 220). This maneuver will be a Forward to Reverse Flight maneuver (Southern Hemisphere viewing). 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 06 July 2001 ORBIT AOS NO. SUBSYS REASON ----- --- --- ------ ------ 53603 182/1138 01-431 SOLSTICE Power ON - Fulltime 53604 182/1415 01-432 SUSIM Power ON - (Partial) 53607 182/1748 01-433 SUSIM Additional Commands 53609 182/2116 01-434 ACRIM Power ON 53618 183/1139 01-432 SUSIM Power ON - CONTINUED 53618 183/1236 01-435 SUSIM Power ON - COMPLETE 53619 183/1319 01-436 PEM ZEPS / HEPS DAY-ONLY 53625 183/2339 01-437 PEM Power ON AXIX 1 & 2 53637 184/1753 01-438 NBTR NOOPS D-185 53640 184/2257 01-439 HALOE Power ON 53644 185/0623 01-438 NBTR NOOPS D-185 53644 185/0623 01-440 HALOE Power ON complete 53646 185/0918 01-441 HALOE SR & SS corrections 53652 185/1755 01-442 NBTR NOOPS D-186 53658 186/0453 01-442 NBTR NOOPS D-186 53668 186/1757 01-443 NBTR NOOPS D-187 53673 187/0441 01-443 NBTR NOOPS D-187 53680 187/1501 01-444 OBC/TAM TAM UPDATE 53681 187/1611 01/443 NBTR NOOPS D-187 53682 187/1758 01-445 NBTR NOOPS D-188 ____________________________________________________________________________ APPENDIX B OUT-OF-LIMITS & ALERTS OCCURRENCES Week ending 06 July 2001 The following Out-Of-Limits occurrences were detected: MNEMONIC STATE DESCRIPTION ORBITS -------- ----- ----------- ------ HACS4 Y-HI GIMBLE LIMIT 53646 HAMFCAT R-HI TELESCOPE BARREL#3 TEMP 53646 HATBLT3 R-HI MAIN FRAME COLD TEMP 53646 The following ALERT occurrences were detected: MNEMONIC DESCRIPTION ORBITS -------- ----------- ------ -None this report period _______________________________________________________________________________ APPENDIX C CLOCK & SOLAR ARRAY RATE CORRECTIONS Week ending 06 July 2001 CLOCK DRIFT RATE ADJUSTMENTS ORBIT TIME CLOCK RATE CHANGE ----- ----- ----------------- -None this report period ___________________________________________________________________________ APPENDIX D UARS BATTERY PERFORMANCE DATA Week ending 06 July 2001 29 June 2001 - GMT Day 180 Beta = 1.7 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/-4.94 +0.0/+0.0 12.0 0.000 0.0 2 +11.2/-100.8 +5.47/+3.87 +28.0/-12.8 24.5 1.040 19.8 3 +22.4/-39.2 +4.51/+2.60 +27.2/-13.2 24.5 1.030 19.5 6 July 2001 - GMT Day 187 Beta = 29.3 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/-4.31 +0.0/+0.0 12.0 0.000 0.0 2 +11.2/-134.4 +5.79/+4.51 +28.4/-14.4 24.8 1.030 20.7 3 +22.4/-56.0 +4.83/+3.23 +28.0/-15.2 24.8 1.020 20.7 V/T LEVEL CHANGES ORB# TIME LVL FR-TO ---- ---- --------- -no changes V/T 5 _______________________________________________________________________________ APPENDIX E UARS ANOMALY REPORTS Week ending 06 July 2001 NEW ANOMALY REPORTS GENERATED AR NO. SUBSYS ORBIT TIME TTR PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 01-040 HALOE 53646 185/0814 N/A HALOE LIMITS OOL 01-041 FOT 53681 187/1634Z 14170 Generic Late Acquisition ANOMALY CLOSURE INFORMATION RECEIVED AR NO. SUBSYS ORBIT TIME TTR PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 01-032 FOT see list June 01 14170 Generic Late Acquisition 01-040 HALOE 53646 185/0814 N/A HALOE LIMITS OOL ANOMALY INVESTIGATION REPORTS GENERATED AR NO. SUBSYS ORBIT TIME TTR PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- -None this report period OPEN ANOMALY REPORTS AR NO. SUBSYS ORBIT TIME TTR PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 01-041 FOT see list July 01 14170 Generic Late Acquisition SEVNTFW01/27