********** KPT Logfile For Engine Only Run ********** *** Date: Thu Apr 6 20:47:42 2006 *** User: Conor Andrew Nixon, 301-286-6757 ***************************************************************** Insert Spice File: /cas/ancillary/ops/NAIF/sp/060323AP_SE_06082_08222.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/051212AP_RE_90165_14363.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/060323AP_PE_06082_08222.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/060323AP_SK_06082_08222.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0008.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck29Apr2005.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_27Feb2006_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00096.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_13/input.bvh Successfully Read IVT File: pdt_Run_13/input.ivt Successfully Read TLF File: /cas/msspath/MSS.D11.0/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.tlf Successfully Read Momentum Models File: /cas/msspath/MSS.D11.0/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.mmf Successfully Read Mass Properties File: /cas/msspath/MSS.D11.0/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.mpf Successfully Read Grnd System Op Modes File: /cas/msspath/MSS.D11.0/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.gso Successfully Read KPT Spice Identification File: /cas/ancillary/ops/SCO/ssid/05_347_param.ssid Successfully Read Input PEF File: pdt_Run_13/temp.pef NOTE: This File Supercedes Any Events held within the Input Configuration File. Successfully Read KPT CMT File: /cas/ancillary/ops/SCO/cmt_limits/POST_PROBE_V11.cmt Insert Spice File: /cas/ancillary/ops/NAIF/sp/060323AP_SE_06082_08222.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/051212AP_RE_90165_14363.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/060323AP_PE_06082_08222.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/060323AP_SK_06082_08222.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0008.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck29Apr2005.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_27Feb2006_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00096.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_13/input.bvh Successfully Read IVT File: pdt_Run_13/input.ivt Successfully Read TLF File: /cas/msspath/MSS.D11.0/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.tlf Successfully Read Momentum Models File: /cas/msspath/MSS.D11.0/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.mmf Successfully Read Mass Properties File: /cas/msspath/MSS.D11.0/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.mpf Successfully Read Grnd System Op Modes File: /cas/msspath/MSS.D11.0/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.gso Successfully Read KPT Spice Identification File: /cas/ancillary/ops/SCO/ssid/05_347_param.ssid Successfully Read Input PEF File: pdt_Run_13/temp.pef NOTE: This File Supercedes Any Events held within the Input Configuration File. Successfully Read KPT CMT File: /cas/ancillary/ops/SCO/cmt_limits/POST_PROBE_V11.cmt ------------------------------ CSAS-KPT Version: V11.00 2004 ------------------------------ **** WARNING: INITIAL PRIMARY INERTIAL Vector TITAN is present in the Initial IVT, but the Vector Entry has a time interval which does NOT contain the Current Time of interest. THIS CONDITION REQUIRES FIXING IF THIS IS A REAL SEQUENCE. ************************************************************ NOTE: MANEUVER COMMANDS Cause Turning of the Spacecraft 1.125 -> 2.000 seconds following the Command Time - the times shown in this Run Log are times that the Spacecraft Actually Starts Turning. ************************************************************ ************************************************************ NOTE: CONSTRAINT MONITOR IS SELECTED FOR THIS RUN Initial CMT Dynamic Constraints: RCS Max Rates(rad/s): 1.43000000e-02 1.43000000e-02 1.43000000e-02 RCS Max Accel(rad/s/s): 1.52700000e-04 1.24200000e-04 3.24700000e-04 RWA Max Rates(rad/s): 2.46800000e-03 2.96200000e-03 4.88600000e-03 RWA Max Accel(rad/s/s): 1.35300000e-05 1.62300000e-05 2.67800000e-05 ************************************************************ ************************************************************ * * * NOTE: ALL ERRORS, REJECTED COMMANDS, WARNINGS, * * CMT VIOLATIONS, etc, MUST BE FIXED PRIOR * * TO FINAL SEQUENCE GENERATION and UPLINK * ************************************************************ Adding/Replacing Vector TITAN to the IVT at UTC Time: 2006-203T02:10:31.000 Adding/Replacing Vector TITAN_N_POLE_DIR to the IVT at UTC Time: 2006-203T02:35:31.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-203T02:40:20.000 ) This is Command #1 from the Event List PROCESSING Starting on TARGET Command at 2085.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-203T02:40:21.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN; SECONDARY BODY: POS_X; SECONDARY INERTIAL: TITAN_N_POLE_DIR; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2092.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-203T02:40:28.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 0.000 0.000 -125.019 mrad Profiled Maneuver time (seconds): 773.1706 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-203T02:40:26.000 ) This is Command #4 from the Event List PROCESSING Starting on OFFSET Command at 3412.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-203T03:02:28.000 ) This is Command #5 from the Event List QUANTIZED ANGLES: 0.000 0.000 -55.031 mrad Profiled Maneuver time (seconds): 115.4609 PROCESSING Starting on PROFILE Command at 3531.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-203T03:04:27.000 ) This is Command #6 from the Event List PROCESSING Starting on DELTA_BASE Command at 3535.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-203T03:04:31.000 ) This is Command #7 from the Event List QUANTIZED ANGLES: 0.000 0.000 83.985 mrad Profiled Maneuver time (seconds): 6999.3977 PROCESSING Starting on PROFILE Command at 10545.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-203T05:01:21.000 ) This is Command #8 from the Event List PROCESSING Starting on OFFSET Command at 10552.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-203T05:01:28.000 ) This is Command #9 from the Event List QUANTIZED ANGLES: 0.000 0.000 60.016 mrad Profiled Maneuver time (seconds): 76.9196 PROCESSING Starting on PROFILE Command at 11084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-203T05:10:20.000 ) This is Command #10 from the Event List PROCESSING Starting on TARGET Command at 11085.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-203T05:10:21.000 ) This is Command #11 from the Event List PRIMARY BODY: ISS_NAC; PRIMARY INERTIAL: TITAN; SECONDARY BODY: NEG_X; SECONDARY INERTIAL: SUN; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 11092.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-203T05:10:28.000 ) This is Command #12 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 781.9082 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2006-203T05:20:36.000 PROCESSING Starting on 89EXE_CMD_SEQ Command at 11930.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-203T05:24:26.000 ) This is Command #13 from the Event List EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_13/kpt_eo.plt -----------------------------------