ACE Weekly 07/11/03 - 07/17/03 All ACE spacecraft subsystems are performing nominally. An attitude maneuver was successfully executed on 07/11/03. The next attitude maneuver is scheduled for 07/25/03. ============================================================================ Orbit Events: The next SEV transit will occur during the 09/01/03 - 09/23/03 time frame. Expected minimum SEV angle will be 1.77 degrees. ============================================================================ OCRs Executed: NONE ============================================================================ Ongoing Activities: TAPS: Trending, Analysis and Plotting System (TAPS) development continues with emphasis being placed on fixing the DRs attributed to the current release. Testing is progressing on both TAPS#1 and TAPS#2. ---------------------------------------------------------------------------- Automation (ROBOTT): FOT testing of ROBOTT Release 0.1 is ongoing. Testing of CRON began this week and it is running well to date. The Automation Team is performing testing on the Command & Control system. The first release to the FOT is still TBD. ============================================================================ Anomalies: DOY 03192 (7/11/2003) - ACE Anomaly G03-0059 - GDS 26m (DSS-16) Loss of Telemetry / TCP Halt At 14:34:33, during the attitude maneuver, telemetry dropped out. At the time of the drop out, the FOT was at pulse 40 of a 58 pulse maneuver. The FOT informed DSS-16 of the data loss but the operator stated everything was nominal at the station. The FOT contacted JPL Comm concerning the data loss and then DSS-16 called back, after checking their equipment, to confirm the problem was at the station (TCP Halt). The operator said it would be 2 minutes until data resumed. At 14:40:12, telemetry resumed and the FOT verified the completion of the maneuver. FDF checked and confirmed the maneuver was successful. IMPACT: Unable to monitor attitude maneuver. DR# G103022 DOY 03192 (7/11/2003) - ACE Anomaly G03-0060 - GDS 26m (DSS-16) Gap In Ground Receiver AGC The ground receiver AGC values from DSS-16 have a gap between -119.83009 and -124.56311. All of the values we receive are outside of this range. Checking past values has shown that this has been happening since DOY 03083 when 26m Upgrade equipment was installed (but only with DSS-16). IMPACT: Causes problems for RF trending. DR# G102948 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ Glen A. Miller ACE Flight Operations Observatory Engineer Honeywell Technology Solutions Inc. Goddard Space Flight Center Building 14, Room W10A Mail Stop 428.2 Greenbelt, MD 20771 Office: 301-286-7071 Pager: 800-425-3174 Fax: 301-286-1729 Email: gamiller@pop500.gsfc.nasa.gov ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~