******************************************************************** UARS WEEKLY STATUS REPORT - 11 OCT 2002 ******************************************************************** *********** SOLSTICE *********** Nothing received. *********** SUSIM *********** SUSIM successfully performed its daily mid-resolution and MgII solar scans during periods of predicted UARS telemetry. Today 10/11/02 marks the 11th year of SUSIM's observations, SUSIM has now collected data for an entire solar cycle. *********** ACRIM *********** Nothing received. *********** PEM *********** PEM continues to work with the GUVI team on the diagnosis of data from the first conjunction period. Analysis of the two conjunction passes showed that the aurora as detected by GUVI was at higher latitude than UARS. GUVI images from other times from the first conjunction period show spatial regions that both GUVI and PEM sampled when aurora was present. Separation is several minutes to 10's of minutes when both instruments saw aurora. A presentation will be made at the November American Meteorological Society meeting on PEM's view of the first conjunction period. PEM has seen no aurora during the second conjunction period. PEM data for a third GUVI-PEM conjunction has been planned. This time period is October 27. Orbit analysis shows that conjunctions will occur between TIMED and UARS at 11:03 UT (IL = 65 deg, MLT = 20 hr, GeoLat = -51 deg, GeoLon = 132 deg) and 11:50 UT (IL = 61 deg, MLT = 8 hr, GeoLat = 52 deg, GeoLon = 295 deg). 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. *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 to support re-engineering of the UARS Mission Operations Concept to develop capabilities for the Science Traceability Mission. Daily processing of instrument Daily Activity Plans continues with no problems. *********** CDHF *********** Nothing received. *********** FOT *********** REPORTING PERIOD This report covers 28 September 2002 (Orbit 60414, GMT Day 271) through 04 October 2002 (Orbit 60534, GMT Day 277). 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 PEM 272/1303 60437 POWER ON AXIS 1 HRDI 276/1835 60500 TO DAY ONLY MODE The beta angle ranged between the angles of 43.6 degrees to 27.1 degrees for this report period. The beta angle is now decreasing towards a minimum angle of 0 degrees on 10 October 2002 (DOY 283). 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 0.96 to 0.97 degrees C. Additional battery performance data for each battery on 28 September and 04 October 2002 are provided in Appendix D. The clock error ranged from -12.6 to 10.4 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 = 04 PEM = 01 HRDI = 01 UARS Anomaly Reports initiated during this report period are listed in Appendix E and summarized below. FOT = 00 Two (2) Anomaly Report remained OPEN at the end of this report period (see Appendix E). GROUND SYSTEM OPERATION Zero (0) 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 new hard disk on the prototype was installed this week. The new build of the Eclipse software has also been installed and can now be tested. Once the testing is completed the software can be released for operations. This will most likely not take place until the ERBS integration is complete. The FOT is also working hard in preparation for the college students that will be in the control center to learn about spacecraft operations. The FOT will try to formulate training materials and structure a learning plan to teach the students. This is all part of the new Educational Outreach initiative/contract, which started on October 1, 2002 for both UARS and TOMS. MEETINGS - The FOT attended the UARS Monthly Status review on 03 October 2002. FUTURE SIGNIFICANT EVENTS The next UARS Yaw slew is scheduled for 10 October 2002 (DOY 283). 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 04 October 2002 ORBIT AOS NO. SUBSYS REASON ----- --- --- ------ ------ 60437 272/1303 02-340 PEM POWER ON AXIS 1 60475 275/0237 02-341 OBC/CLK CLK ADJ FR 0.0 TO 20.6 MSEC/DAY 60494 276/0820 02-342 OBC/CLK CLK ADJ FR 20.6 TO 0.0 MSEC/DAY 60500 276/1835 02-343 HRDI TO DAY-ONLY MODE 60501 276/2016 02-344 OBC/CLK CLK ADJ FR 0.0 TO -20.6 MSEC/DAY 60519 277/2351 02-345 OBC/CLK CLK ADJ FR -20.6 TO 0.0 MSEC/DAY APPENDIX B OUT-OF-LIMITS & ALERTS OCCURRENCES Week ending 04 October 2002 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 04 October 2002 CLOCK DRIFT RATE ADJUSTMENTS ORBIT TIME CLOCK RATE CHANGE ----- ----- ----------------- 60475 275/0241 CLK ADJ FR 0.0 TO 20.6 MSEC/DAY 60494 276/0822 CLK ADJ FR 20.6 TO 0.0 MSEC/DAY 60501 276/2016 CLK ADJ FR 0.0 TO -20.6 MSEC/DAY 60519 277/2353 CLK ADJ FR -20.6 TO 0.0 MSEC/DAY APPENDIX D UARS BATTERY PERFORMANCE DATA Week ending 04 October 2002 27 September 2002 - GMT Day 270 Beta = 49.7 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 -145.6/-11.2 -3.68/-4.63 +00.0/+00.0 08.3 0.000 0.0 2 +11.2/-50.4 +5.14/+3.23 +24.4/-15.2 25.0 1.030 19.8 3 +22.4/-33.6 +3.87/+2.60 +24.0/-15.2 25.0 1.040 19.3 04 October 2002 - GMT Day 277 Beta = 27.1 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 -140.0/-168.0 -3.05/-4.31 +00.0/+00.0 08.3 0.000 0.0 2 +11.2/-89.6 +5.15/+4.19 +28.8/-15.2 24.8 1.030 21.0 3 +22.4/-67.2 +4.19/+3.23 +28.0/-15.2 24.8 1.020 20.5 V/T LEVEL CHANGES ORB# AOS TIME LVL FR-TO ----- -------- --------- -None this report period. APPENDIX E UARS ANOMALY REPORTS Week ending 04 October 2002 NEW ANOMALY REPORTS GENERATED AR NO. SUBSYS ORBIT TIME CDS PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- -None this report period. ANOMALY CLOSURE INFORMATION RECEIVED AR NO. SUBSYS ORBIT TIME CDS PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 02-050 SOLSTICE 60336 265/2037 N/A SOLS UNEXPECTED STATE ANOMALY INVESTIGATION REPORTS GENERATED AR NO. SUBSYS ORBIT TIME CDS PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- -None this report period. OPEN ANOMALY REPORTS AR NO. SUBSYS ORBIT TIME CDS PROBLEM/DATA LOSS ------ ------ ----- ---- --- ----------------- 02-051 FOT 60366 267/1951 30832 GENERIC LATE ACQUISITION 02-052 SOLSTICE 60366 267/1951 N/A LOADING PROBLEM