********** KPT Logfile For Engine Only Run ********** *** Date: Tue Nov 8 19:41:46 2005 *** User: Conor Andrew Nixon, 301-286-6757 ***************************************************************** Insert Spice File: /cas/ancillary/ops/NAIF/sp/050720AP_SE_05119_08222.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/050923AP_RE_04002_09011.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/050720AP_PE_05119_08222.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/050720AP_SK_05119_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_08Apr2005_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00093.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_2/input.bvh Successfully Read IVT File: pdt_Run_2/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_098_param.ssid Successfully Read Input PEF File: pdt_Run_2/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_V10.cmt Insert Spice File: /cas/ancillary/ops/NAIF/sp/050720AP_SE_05119_08222.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/050923AP_RE_04002_09011.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/050720AP_PE_05119_08222.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/050720AP_SK_05119_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_08Apr2005_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00093.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_2/input.bvh Successfully Read IVT File: pdt_Run_2/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_098_param.ssid Successfully Read Input PEF File: pdt_Run_2/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_V10.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): 1.54400000e-04 1.25500000e-04 3.29100000e-04 RWA Max Rates(rad/s): 2.45900000e-03 2.95000000e-03 4.88000000e-03 RWA Max Accel(rad/s/s): 1.34800000e-05 1.61700000e-05 2.67400000e-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: 2006-076T07:50:03.000 Adding/Replacing Vector SATURN_N_POLE_DIR to the IVT at UTC Time: 2006-076T07:50:05.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-076T08:19:54.000 ) 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): 2006-076T08:19:55.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: SATURN_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): 2006-076T08:20:02.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: -2.013 0.000 0.000 mrad Profiled Maneuver time (seconds): 29.3805 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-076T08:20:00.000 ) This is Command #4 from the Event List PROCESSING Starting on OFFSET Command at 6772.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-076T09:38:02.000 ) This is Command #5 from the Event List QUANTIZED ANGLES: 0.000 0.000 9.970 mrad Profiled Maneuver time (seconds): 45.8176 PROCESSING Starting on OFFSET Command at 7972.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-076T09:58:02.000 ) This is Command #6 from the Event List QUANTIZED ANGLES: -2.013 0.000 0.000 mrad Profiled Maneuver time (seconds): 45.8173 PROCESSING Starting on OFFSET Command at 11572.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-076T10:58:02.000 ) This is Command #7 from the Event List QUANTIZED ANGLES: 0.000 0.000 9.970 mrad Profiled Maneuver time (seconds): 45.8176 PROCESSING Starting on OFFSET Command at 12892.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-076T11:20:02.000 ) This is Command #8 from the Event List QUANTIZED ANGLES: -2.013 0.000 0.000 mrad Profiled Maneuver time (seconds): 45.8173 PROCESSING Starting on OFFSET Command at 16492.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-076T12:20:02.000 ) This is Command #9 from the Event List QUANTIZED ANGLES: 0.000 0.000 9.970 mrad Profiled Maneuver time (seconds): 45.8176 PROCESSING Starting on OFFSET Command at 17692.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-076T12:40:02.000 ) This is Command #10 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 43.5779 PROCESSING Starting on OFFSET Command at 21292.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-076T13:40:02.000 ) This is Command #11 from the Event List QUANTIZED ANGLES: 0.000 0.000 9.970 mrad Profiled Maneuver time (seconds): 43.5783 PROCESSING Starting on OFFSET Command at 22492.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-076T14:00:02.000 ) This is Command #12 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 43.5779 PROCESSING Starting on OFFSET Command at 26092.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-076T15:00:02.000 ) This is Command #13 from the Event List QUANTIZED ANGLES: 0.000 0.000 9.970 mrad Profiled Maneuver time (seconds): 43.5783 PROCESSING Starting on OFFSET Command at 27292.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-076T15:20:02.000 ) This is Command #14 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 43.5779 PROCESSING Starting on OFFSET Command at 30892.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-076T16:20:02.000 ) This is Command #15 from the Event List QUANTIZED ANGLES: 0.000 0.000 9.970 mrad Profiled Maneuver time (seconds): 43.5782 PROCESSING Starting on OFFSET Command at 32092.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-076T16:40:02.000 ) This is Command #16 from the Event List QUANTIZED ANGLES: 2.972 0.000 0.000 mrad Profiled Maneuver time (seconds): 48.0961 PROCESSING Starting on OFFSET Command at 35692.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-076T17:40:02.000 ) This is Command #17 from the Event List QUANTIZED ANGLES: 0.000 0.000 9.012 mrad Profiled Maneuver time (seconds): 46.5399 PROCESSING Starting on OFFSET Command at 36892.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-076T18:00:02.000 ) This is Command #18 from the Event List QUANTIZED ANGLES: 2.972 0.000 0.000 mrad Profiled Maneuver time (seconds): 46.5397 PROCESSING Starting on OFFSET Command at 40492.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-076T19:00:02.000 ) This is Command #19 from the Event List QUANTIZED ANGLES: 0.000 0.000 9.970 mrad Profiled Maneuver time (seconds): 48.0964 PROCESSING Starting on OFFSET Command at 41692.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-076T19:20:02.000 ) This is Command #20 from the Event List QUANTIZED ANGLES: 2.972 0.000 0.000 mrad Profiled Maneuver time (seconds): 48.0961 PROCESSING Starting on OFFSET Command at 45292.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-076T20:20:02.000 ) This is Command #21 from the Event List QUANTIZED ANGLES: 0.000 0.000 9.970 mrad Profiled Maneuver time (seconds): 48.0964 PROCESSING Starting on OFFSET Command at 46492.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-076T20:40:02.000 ) This is Command #22 from the Event List QUANTIZED ANGLES: 2.972 0.000 0.000 mrad Profiled Maneuver time (seconds): 48.0961 PROCESSING Starting on OFFSET Command at 50092.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-076T21:40:02.000 ) This is Command #23 from the Event List QUANTIZED ANGLES: 0.000 0.000 9.970 mrad Profiled Maneuver time (seconds): 48.0964 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2006-076T22:14:10.000 PROCESSING Starting on PROFILE Command at 52244.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-076T22:15:54.000 ) This is Command #24 from the Event List PROCESSING Starting on TARGET Command at 52245.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-076T22:15:55.000 ) This is Command #25 from the Event List PRIMARY BODY: ISS_NAC; PRIMARY INERTIAL: TITAN; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: SATURN_N_POLE_DIR; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 52252.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-076T22:16:02.000 ) This is Command #26 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 41.0602 PROCESSING Starting on 89EXE_CMD_SEQ Command at 52420.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-076T22:18:50.000 ) This is Command #27 from the Event List EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_2/kpt_eo.plt -----------------------------------