============ KPT ================= TIME: Fri Apr 5 16:34:08 2013 USER: Todd Ansty ================================== Insert Spice File: /cas/ancillary/ops/NAIF/sp/110818AP_SE_11175_17265.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/120308AP_RE_90165_18018.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/120711BP_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/cas00156.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_5/input.bvh Successfully Read IVT File: pdt_Run_5/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_5/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/120308AP_RE_90165_18018.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/120711BP_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/cas00156.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_5/input.bvh Successfully Read IVT File: pdt_Run_5/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_5/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: 2013-286T06:40:03.000 Adding/Replacing Vector TITAN_N_POLE_DIR to the IVT at UTC Time: 2013-286T06:40:04.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T07:09:53.000 ) 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): 2013-286T07:09:54.000 ) 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): 2013-286T07:10:01.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: -0.095 0.000 1.150 mrad Profiled Maneuver time (seconds): 10.9826 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T07:09:59.000 ) This is Command #4 from the Event List Simulated Maneuver End Time (UTC): 2013-286T07:10:12.120 Turn Magnitude for 7OFFSET (milliradians): 0.5648 PROCESSING Starting on OFFSET Command at 2742.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T07:20:51.000 ) This is Command #5 from the Event List QUANTIZED ANGLES: 6.519 0.000 7.478 mrad Profiled Maneuver time (seconds): 56.3656 Simulated Maneuver End Time (UTC): 2013-286T07:21:47.500 Turn Magnitude for 7OFFSET (milliradians): 9.1615 PROCESSING Starting on PROFILE Command at 2831.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T07:22:20.000 ) This is Command #6 from the Event List PROCESSING Starting on DELTA_BASE Command at 2835.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T07:22:24.000 ) This is Command #7 from the Event List QUANTIZED ANGLES: 0.000 0.000 -14.956 mrad Profiled Maneuver time (seconds): 3739.1081 Simulated Maneuver End Time (UTC): 2013-286T08:24:43.250 Turn Magnitude for 7DELTA_BASE (milliradians): 14.6470 PROCESSING Starting on PROFILE Command at 6575.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T08:24:44.000 ) This is Command #8 from the Event List PROCESSING Starting on DELTA_BODY Command at 6579.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T08:24:48.000 ) This is Command #9 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2799 Simulated Maneuver End Time (UTC): 2013-286T08:25:21.500 Turn Magnitude for 7DELTA_BODY (milliradians): 2.4881 PROCESSING Starting on PROFILE Command at 6613.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T08:25:22.000 ) This is Command #10 from the Event List PROCESSING Starting on DELTA_BASE Command at 6617.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T08:25:26.000 ) This is Command #11 from the Event List QUANTIZED ANGLES: 0.000 0.000 14.956 mrad Profiled Maneuver time (seconds): 3739.1635 Simulated Maneuver End Time (UTC): 2013-286T09:27:45.370 Turn Magnitude for 7DELTA_BASE (milliradians): 15.4361 PROCESSING Starting on PROFILE Command at 10357.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T09:27:46.000 ) This is Command #12 from the Event List PROCESSING Starting on DELTA_BODY Command at 10361.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T09:27:50.000 ) This is Command #13 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2799 Simulated Maneuver End Time (UTC): 2013-286T09:28:23.500 Turn Magnitude for 7DELTA_BODY (milliradians): 2.4879 PROCESSING Starting on PROFILE Command at 10395.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T09:28:24.000 ) This is Command #14 from the Event List PROCESSING Starting on DELTA_BASE Command at 10399.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T09:28:28.000 ) This is Command #15 from the Event List QUANTIZED ANGLES: 0.000 0.000 -14.956 mrad Profiled Maneuver time (seconds): 3739.1825 Simulated Maneuver End Time (UTC): 2013-286T10:30:47.370 Turn Magnitude for 7DELTA_BASE (milliradians): 14.5987 PROCESSING Starting on PROFILE Command at 14139.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T10:30:48.000 ) This is Command #16 from the Event List PROCESSING Starting on DELTA_BODY Command at 14143.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T10:30:52.000 ) This is Command #17 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2798 Simulated Maneuver End Time (UTC): 2013-286T10:31:25.500 Turn Magnitude for 7DELTA_BODY (milliradians): 2.4873 PROCESSING Starting on PROFILE Command at 14177.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T10:31:26.000 ) This is Command #18 from the Event List PROCESSING Starting on DELTA_BASE Command at 14181.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T10:31:30.000 ) This is Command #19 from the Event List QUANTIZED ANGLES: 0.000 0.000 14.956 mrad Profiled Maneuver time (seconds): 3739.1927 Simulated Maneuver End Time (UTC): 2013-286T11:33:49.370 Turn Magnitude for 7DELTA_BASE (milliradians): 15.5617 PROCESSING Starting on PROFILE Command at 17921.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T11:33:50.000 ) This is Command #20 from the Event List PROCESSING Starting on DELTA_BODY Command at 17925.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T11:33:54.000 ) This is Command #21 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2798 Simulated Maneuver End Time (UTC): 2013-286T11:34:27.500 Turn Magnitude for 7DELTA_BODY (milliradians): 2.4870 PROCESSING Starting on PROFILE Command at 17959.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T11:34:28.000 ) This is Command #22 from the Event List PROCESSING Starting on DELTA_BASE Command at 17963.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T11:34:32.000 ) This is Command #23 from the Event List QUANTIZED ANGLES: 0.000 0.000 -14.956 mrad Profiled Maneuver time (seconds): 3739.1639 Simulated Maneuver End Time (UTC): 2013-286T12:36:51.370 Turn Magnitude for 7DELTA_BASE (milliradians): 14.5436 PROCESSING Starting on PROFILE Command at 21703.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T12:36:52.000 ) This is Command #24 from the Event List PROCESSING Starting on DELTA_BODY Command at 21707.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T12:36:56.000 ) This is Command #25 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2798 Simulated Maneuver End Time (UTC): 2013-286T12:37:29.500 Turn Magnitude for 7DELTA_BODY (milliradians): 2.4862 PROCESSING Starting on PROFILE Command at 21741.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T12:37:30.000 ) This is Command #26 from the Event List PROCESSING Starting on DELTA_BASE Command at 21745.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T12:37:34.000 ) This is Command #27 from the Event List QUANTIZED ANGLES: 0.000 0.000 14.956 mrad Profiled Maneuver time (seconds): 3739.1293 Simulated Maneuver End Time (UTC): 2013-286T13:39:53.370 Turn Magnitude for 7DELTA_BASE (milliradians): 15.7427 PROCESSING Starting on PROFILE Command at 25485.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T13:39:54.000 ) This is Command #28 from the Event List PROCESSING Starting on DELTA_BODY Command at 25489.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T13:39:58.000 ) This is Command #29 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2798 Simulated Maneuver End Time (UTC): 2013-286T13:40:31.500 Turn Magnitude for 7DELTA_BODY (milliradians): 2.4858 PROCESSING Starting on PROFILE Command at 25523.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T13:40:32.000 ) This is Command #30 from the Event List PROCESSING Starting on DELTA_BASE Command at 25527.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T13:40:36.000 ) This is Command #31 from the Event List QUANTIZED ANGLES: 0.000 0.000 -14.956 mrad Profiled Maneuver time (seconds): 3739.0523 Simulated Maneuver End Time (UTC): 2013-286T14:42:55.250 Turn Magnitude for 7DELTA_BASE (milliradians): 14.4832 PROCESSING Starting on PROFILE Command at 29290.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T14:43:19.000 ) This is Command #32 from the Event List PROCESSING Starting on OFFSET Command at 29293.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T14:43:22.000 ) This is Command #33 from the Event List QUANTIZED ANGLES: -0.095 0.000 1.150 mrad Profiled Maneuver time (seconds): 63.6703 Simulated Maneuver End Time (UTC): 2013-286T14:44:25.870 Turn Magnitude for 7OFFSET (milliradians): 12.0177 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2013-286T14:51:37.000 PROCESSING Starting on PROFILE Command at 30012.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T14:55:21.000 ) This is Command #34 from the Event List PROCESSING Starting on TARGET Command at 30013.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T14:55:22.000 ) This is Command #35 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 30020.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T14:55:29.000 ) This is Command #36 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 10.9881 PROCESSING Starting on 89EXE_CMD_SEQ Command at 30018.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-286T14:55:27.000 ) This is Command #37 from the Event List Simulated Maneuver End Time (UTC): 2013-286T14:55:40.120 Turn Magnitude for 7OFFSET (milliradians): 0.5692 EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_5/kpt_eo.plt -----------------------------------