******************************************************************** UARS WEEKLY STATUS REPORT - 20 Feb 2004 ******************************************************************** *********** SOLSTICE *********** During this week SOLSTICE continued to operate in good health gathering solar data on all available orbital tracking periods. On average, we received 53% of each day's data amounting to about 350 minutes of solar observing time per day. *********** SUSIM *********** SUSIM successfully gathered all of its daily mid (1.1 nm) resolution, Mg II, occultation, solar pointing offset and high resolution continuous monitoring scans during this past week for periods of UARS real-time telemetry or onboard tape recording. *********** PEM *********** Level 2 PEM HEPSA data files are being reprocessed for submission to the DAAC. This data has been designated as version 2; however, there is no format difference from the version 1 data format. Version 2 HEPSA data is being generated because it was discovered that there exists processing errors within some of the HEPSA version 1 data files. Thus, if you are using any HEPSA version 1 data files from the DAAC, please replace them with the version 2 data files. Currently, HEPSA data between 1991274 and 2003149 has been reprocessed and archived at the GSFC DAAC. Level 2 PEM MEPS data file documentation is complete and submitted to the DAAC. MEPS data files are version 1. Processed MEPS data files at the DAAC archive are between 1991274 and 1993299. MEPS data files between 1993300 and 1993329 are waiting for DAAC collection. PEM continues to receive NMC data files from NOAA. No problems have been encountered. NOAA has changed the binary structure of the NMC data and PEM is now receiving two data streams, one in the original VAX format and the other from their new binary format. The PEM data from the GUVI conjunction periods may be found at http://wwwpem.space.swri.edu/guvi-pem.html. *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 *********** Nothing received. *********** MLS *********** Nothing received. *********** HRDI *********** Nothing received. *********** WINDII *********** Nothing received. *********** MPG *********** The MPG continues to serve as the point-of-contact for UARS instrument operations in support of the Science Traceability Mission of UARS. Daily processing of instrument Daily Activity Plans continues with no problems. *********** CDHF *********** Nothing received. *********** FOT *********** REPORTING PERIOD This report covers 07 February 2004 (Orbit 67886, GMT Day 038) through 13 February 2004 (Orbit 67990, GMT Day 044). 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 NONE THIS REPORT PERIOD The beta angle ranged between the angles of 40.8 degrees to 27.3 degrees for this report period. The beta angle is now decreasing towards a minimum angle of 0 degrees on 21 February 2004 (DOY 052). 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 23.6 V end-of-night (EON) load bus voltage. Battery temperatures are stable with a temperature delta between Battery 2 and Battery 3 of 1.27 to 1.29 degrees C. Additional battery performance data for each battery on 06 February and 13 February 2004 are provided in Appendix D. The clock error ranged from 10.1 to -11.1 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 = 02 UARS Anomaly Reports initiated during this report period are listed in Appendix E and summarized below. FOT = 03 Four (4) Anomaly Reports remained OPEN at the end of this report period (see Appendix E). GROUND SYSTEM OPERATION Three (3) operational support problems occurred this period. Anomaly Reports are included in Appendix E. The data loss calculations are no longer being supplied by Data Capture Facility (DCF). OTHER SIGNIFICANT EVENTS UARS SATELLITE OPERATIONS The problem with the new CMS code was found this week. Two local variables, which effectively set the length of the ephemeris tables, were deleted and put into a global variable. This change caused both tables to be built to the length of the TDRS ephemeris. Thus the spacecraft ephemeris load was incorrectly sized and produced the signature of good data then zero fill, which was seen in the anomalous load(s). These variables were fixed and a new release of the CMS code was delivered to the CMS backup machine. While this version is being tested, the FOT will build all loads on the old version of the CMS code, except the 3-TDRS ephemeris that must be built on the new version. The FOT will also continue to perform their manual checks to insure the ephemeris loads are being built correctly. MEETINGS The FOT held a meeting on 09 February 2004 to discuss the CMS code problem and the results of the analysis performed the previous week. FUTURE SIGNIFICANT EVENTS The next UARS Yaw slew is scheduled for 21 February 2004 (DOY 052). This maneuver will be a Forward to Reverse Flight maneuver (Northern Hemisphere viewing). Attachments: Appendix A, Real-time Command 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 13 February 2004 ORBIT AOS NO. SUBSYS REASON ----- --- --- ------ ------ 67918 040/0330 04-052 OBC/CLK CLK ADJ FR 0.0 TO 20.6 MSEC/DAY 67936 041/0729 04-053 OBC/CLK CLK ADJ FR 20.6 TO 0.0 MSEC/DAY APPENDIX B OUT-OF-LIMITS & ALERTS OCCURRENCES Week ending 13 February 2004 The following Out-Of-Limits occurrences were detected: MNEMONIC STATE DESCRIPTION ORBITS -------- ----- ----------- ------ -None this report period. The following ALERT occurrences were detected: MNEMONIC DESCRIPTION ORBITS -------- ----------- ------ -None this report period. APPENDIX C CLOCK & SOLAR ARRAY RATE CORRECTIONS Week ending 13 February 2004 CLOCK DRIFT RATE ADJUSTMENTS ORBIT TIME CLOCK RATE CHANGE ----- ----- ----------------- 67918 040/0332 CLK ADJ FR 0.0 TO 20.6 MSEC/DAY 67936 041/0734 CLK ADJ FR 20.6 TO 0.0 MSEC/DAY APPENDIX D UARS BATTERY PERFORMANCE DATA Week ending 13 February 2004 06 February 2004 - GMT Day 037 Beta = 40.8 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 -700.0/-700.0 -3.05/-4.31 +00.0/+00.0 07.0 0.00 0.0 2 +16.8/-145.6 +5.47/+4.51 +26.8/-15.2 25.1 1.03 20.2 3 +11.2/-100.8 +4.51/+3.23 +26.4/-15.2 25.1 1.02 19.9 13 February 2004 - GMT Day 044 Beta = 27.3 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 -700.0/-700.0 -3.05/-3.99 +00.0/+00.0 07.0 0.00 0.0 2 +11.2/-089.6 +6.43/+5.14 +28.8/-15.2 24.0 1.04 20.7 3 +11.2/-134.4 +5.14/+3.87 +28.0/-15.2 24.0 1.03 20.5 V/T LEVEL CHANGES ORB# AOS TIME LVL FR-TO ----- -------- --------- -None this report period APPENDIX E UARS ANOMALY REPORTS Week ending 13 February 2004 NEW ANOMALY REPORTS GENERATED AR NO. SUBSYS ORBIT TIME CDS PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 04-010 FOT 67934 041/0409 35016 4 Sec Data Dropout 04-011 FOT 67942 041/1747 30832 Generic Late Acquisition 04-012 FOT 67965 043/0643 35015 Late Acq & No GCMRs/UPDs ANOMALY CLOSURE INFORMATION RECEIVED AR NO. SUBSYS ORBIT TIME CDS PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 04-001 FOT See List Jan 04 30832 Generic Late Acquisition ANOMALY INVESTIGATION REPORTS GENERATED AIR NO. SUBSYS ORBIT TIME CDS PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- -None this report period. OPEN ANOMALY REPORTS AR NO. SUBSYS ORBIT TIME CDS PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 04-009 FOT 67854 035/2126 N/A EPHEMERIS REJECTED 04-011 FOT See List Feb 04 30832 Generic Late Acquisition 04-010 FOT 67934 041/0409 35016 4 Sec Data Dropout 04-012 FOT 67965 043/0643 35015 Late Acq & No GCMRs/UPDs