============ KPT ================= TIME: Tue Jun 19 10:01:17 2012 USER: Todd Ansty ================================== Insert Spice File: /cas/ancillary/ops/NAIF/sp/110818AP_SE_11175_17265.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/110317AP_RE_90165_18018.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/110120BP_IRRE_00256_25017.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/110818AP_PE_11175_17265.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/110818AP_SK_11175_17265.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0010.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck25Aug2011.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_21Jan2011_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00152.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: /export/home/eros/D14.2d_PDT-SWDepot/Input/KPT/kpt_default.tlf Successfully Read KPT Spice Identification File: /cas/ancillary/ops/SCO/ssid/09_131_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_V11.cmt Insert Spice File: /cas/ancillary/ops/NAIF/sp/110818AP_SE_11175_17265.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/110317AP_RE_90165_18018.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/110120BP_IRRE_00256_25017.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/110818AP_PE_11175_17265.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/110818AP_SK_11175_17265.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0010.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck25Aug2011.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_21Jan2011_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00152.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: /export/home/eros/D14.2d_PDT-SWDepot/Input/KPT/kpt_default.tlf Successfully Read KPT Spice Identification File: /cas/ancillary/ops/SCO/ssid/09_131_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_V11.cmt ------------------------------ CSAS-KPT Version: V14.1 ------------------------------ SID Suspend Values Theta_1: 0.20 degrees Theta_2: 0.50 degrees Theta_3: 1.50 degrees T_1: 60.00 seconds T_2: 240.00 seconds T_3: 1800.00 seconds T_4: 2400.00 seconds **** 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: 2012-318T23:52:12.000 Adding/Replacing Vector TITAN_N_POLE_DIR to the IVT at UTC Time: 2012-318T23:52:13.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T00:22:02.000 ) 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): 2012-319T00:22:03.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN; SECONDARY BODY: NEG_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): 2012-319T00:22:10.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 18.0068 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T00:22:08.000 ) This is Command #4 from the Event List Simulated Maneuver End Time (UTC): 2012-319T00:22:28.250 Turn Magnitude for 7OFFSET (milliradians): 1.6973 PROCESSING Starting on OFFSET Command at 2752.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T00:33:10.000 ) This is Command #5 from the Event List QUANTIZED ANGLES: 7.957 0.000 8.436 mrad Profiled Maneuver time (seconds): 62.3248 Simulated Maneuver End Time (UTC): 2012-319T00:34:12.500 Turn Magnitude for 7OFFSET (milliradians): 11.5982 PROCESSING Starting on PROFILE Command at 2841.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T00:34:39.000 ) This is Command #6 from the Event List PROCESSING Starting on DELTA_BASE Command at 2845.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T00:34:43.000 ) This is Command #7 from the Event List QUANTIZED ANGLES: 0.000 0.000 -16.777 mrad Profiled Maneuver time (seconds): 2796.6748 Simulated Maneuver End Time (UTC): 2012-319T01:21:19.870 Turn Magnitude for 7DELTA_BASE (milliradians): 16.3084 PROCESSING Starting on PROFILE Command at 5642.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T01:21:20.000 ) This is Command #8 from the Event List PROCESSING Starting on DELTA_BODY Command at 5646.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T01:21:24.000 ) This is Command #9 from the Event List QUANTIZED ANGLES: -2.780 0.000 0.000 mrad Profiled Maneuver time (seconds): 47.1595 Simulated Maneuver End Time (UTC): 2012-319T01:22:11.370 Turn Magnitude for 7DELTA_BODY (milliradians): 2.7887 PROCESSING Starting on PROFILE Command at 5694.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T01:22:12.000 ) This is Command #10 from the Event List PROCESSING Starting on DELTA_BASE Command at 5698.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T01:22:16.000 ) This is Command #11 from the Event List QUANTIZED ANGLES: 0.000 0.000 16.777 mrad Profiled Maneuver time (seconds): 2796.7329 Simulated Maneuver End Time (UTC): 2012-319T02:08:52.870 Turn Magnitude for 7DELTA_BASE (milliradians): 17.3012 PROCESSING Starting on PROFILE Command at 8495.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T02:08:53.000 ) This is Command #12 from the Event List PROCESSING Starting on DELTA_BODY Command at 8499.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T02:08:57.000 ) This is Command #13 from the Event List QUANTIZED ANGLES: -2.780 0.000 0.000 mrad Profiled Maneuver time (seconds): 47.1595 Simulated Maneuver End Time (UTC): 2012-319T02:09:44.370 Turn Magnitude for 7DELTA_BODY (milliradians): 2.7908 PROCESSING Starting on PROFILE Command at 8547.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T02:09:45.000 ) This is Command #14 from the Event List PROCESSING Starting on DELTA_BASE Command at 8551.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T02:09:49.000 ) This is Command #15 from the Event List QUANTIZED ANGLES: 0.000 0.000 -16.777 mrad Profiled Maneuver time (seconds): 2796.7547 Simulated Maneuver End Time (UTC): 2012-319T02:56:26.000 Turn Magnitude for 7DELTA_BASE (milliradians): 16.2579 PROCESSING Starting on PROFILE Command at 11348.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T02:56:26.000 ) This is Command #16 from the Event List PROCESSING Starting on DELTA_BODY Command at 11352.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T02:56:30.000 ) This is Command #17 from the Event List QUANTIZED ANGLES: -2.780 0.000 0.000 mrad Profiled Maneuver time (seconds): 47.1596 Simulated Maneuver End Time (UTC): 2012-319T02:57:17.370 Turn Magnitude for 7DELTA_BODY (milliradians): 2.7925 PROCESSING Starting on PROFILE Command at 11400.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T02:57:18.000 ) This is Command #18 from the Event List PROCESSING Starting on DELTA_BASE Command at 11404.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T02:57:22.000 ) This is Command #19 from the Event List QUANTIZED ANGLES: 0.000 0.000 16.777 mrad Profiled Maneuver time (seconds): 2796.7706 Simulated Maneuver End Time (UTC): 2012-319T03:43:59.000 Turn Magnitude for 7DELTA_BASE (milliradians): 17.3701 PROCESSING Starting on PROFILE Command at 14201.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T03:43:59.000 ) This is Command #20 from the Event List PROCESSING Starting on DELTA_BODY Command at 14205.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T03:44:03.000 ) This is Command #21 from the Event List QUANTIZED ANGLES: -2.780 0.000 0.000 mrad Profiled Maneuver time (seconds): 47.1596 Simulated Maneuver End Time (UTC): 2012-319T03:44:50.370 Turn Magnitude for 7DELTA_BODY (milliradians): 2.7944 PROCESSING Starting on PROFILE Command at 14253.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T03:44:51.000 ) This is Command #22 from the Event List PROCESSING Starting on DELTA_BASE Command at 14257.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T03:44:55.000 ) This is Command #23 from the Event List QUANTIZED ANGLES: 0.000 0.000 -16.777 mrad Profiled Maneuver time (seconds): 2796.7484 Simulated Maneuver End Time (UTC): 2012-319T04:31:31.870 Turn Magnitude for 7DELTA_BASE (milliradians): 16.2209 PROCESSING Starting on PROFILE Command at 17054.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T04:31:32.000 ) This is Command #24 from the Event List PROCESSING Starting on DELTA_BODY Command at 17058.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T04:31:36.000 ) This is Command #25 from the Event List QUANTIZED ANGLES: -2.780 0.000 0.000 mrad Profiled Maneuver time (seconds): 47.1597 Simulated Maneuver End Time (UTC): 2012-319T04:32:23.370 Turn Magnitude for 7DELTA_BODY (milliradians): 2.7958 PROCESSING Starting on PROFILE Command at 17106.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T04:32:24.000 ) This is Command #26 from the Event List PROCESSING Starting on DELTA_BASE Command at 17110.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T04:32:28.000 ) This is Command #27 from the Event List QUANTIZED ANGLES: 0.000 0.000 16.777 mrad Profiled Maneuver time (seconds): 2796.7218 Simulated Maneuver End Time (UTC): 2012-319T05:19:04.870 Turn Magnitude for 7DELTA_BASE (milliradians): 17.4307 PROCESSING Starting on PROFILE Command at 19930.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T05:19:28.000 ) This is Command #28 from the Event List PROCESSING Starting on OFFSET Command at 19933.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T05:19:31.000 ) This is Command #29 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 55.6030 Simulated Maneuver End Time (UTC): 2012-319T05:20:26.750 Turn Magnitude for 7OFFSET (milliradians): 10.2971 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2012-319T05:31:09.000 PROCESSING Starting on PROFILE Command at 20795.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T05:33:53.000 ) This is Command #30 from the Event List PROCESSING Starting on TARGET Command at 20796.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T05:33:54.000 ) This is Command #31 from the Event List PRIMARY BODY: NEG_Y; PRIMARY INERTIAL: TITAN; SECONDARY BODY: NEG_X; SECONDARY INERTIAL: TITAN_N_POLE_DIR; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 20803.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T05:34:01.000 ) This is Command #32 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 18.0084 Simulated Maneuver End Time (UTC): 2012-319T05:34:19.250 Turn Magnitude for 7OFFSET (milliradians): 1.7044 PROCESSING Starting on 89EXE_CMD_SEQ Command at 20861.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-319T05:34:59.000 ) This is Command #33 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 -----------------------------------