============ KPT ================= TIME: Wed Jan 5 16:10:43 2011 USER: Todd Ansty ================================== Insert Spice File: /cas/ancillary/ops/NAIF/sp/091005AP_SE_09248_17265.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/100209AP_RE_90165_18018.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/090202BP_IRRE_00256_50017.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/091005AP_PE_09248_17265.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/091005AP_SK_09248_17265.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0009.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck02Sep2010.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_11May2009_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00146.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_1/input.bvh Successfully Read IVT File: pdt_Run_1/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_1/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/091005AP_SE_09248_17265.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/100209AP_RE_90165_18018.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/090202BP_IRRE_00256_50017.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/091005AP_PE_09248_17265.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/091005AP_SK_09248_17265.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0009.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck02Sep2010.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_11May2009_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00146.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_1/input.bvh Successfully Read IVT File: pdt_Run_1/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_1/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: 2011-129T12:23:59.000 Adding/Replacing Vector TITAN_N_POLE_DIR to the IVT at UTC Time: 2011-129T12:24:00.000 Adding/Replacing Vector SKY_RA_DEC_149 to the IVT at UTC Time: 2011-129T12:49:00.000 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2080.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T12:53:45.000 ) This is Command #1 from the Event List PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T12:53:49.000 ) This is Command #2 from the Event List PROCESSING Starting on TARGET Command at 2085.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T12:53:50.000 ) This is Command #3 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN; SECONDARY BODY: POS_X; SECONDARY INERTIAL: SKY_RA_DEC_149; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2092.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T12:53:57.000 ) This is Command #4 from the Event List QUANTIZED ANGLES: -0.095 0.000 1.150 mrad Profiled Maneuver time (seconds): 44.3046 Simulated Maneuver End Time (UTC): 2011-129T12:54:41.370 Turn Magnitude for 7OFFSET (milliradians): 5.9056 PROCESSING Starting on OFFSET Command at 4572.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T13:35:17.000 ) This is Command #5 from the Event List QUANTIZED ANGLES: 7.957 0.000 -7.957 mrad Profiled Maneuver time (seconds): 60.1791 Simulated Maneuver End Time (UTC): 2011-129T13:36:17.250 Turn Magnitude for 7OFFSET (milliradians): 12.1741 PROCESSING Starting on PROFILE Command at 4661.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T13:36:46.000 ) This is Command #6 from the Event List PROCESSING Starting on DELTA_BASE Command at 4665.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T13:36:50.000 ) This is Command #7 from the Event List QUANTIZED ANGLES: 0.000 0.000 16.010 mrad Profiled Maneuver time (seconds): 4002.7734 Simulated Maneuver End Time (UTC): 2011-129T14:43:32.870 Turn Magnitude for 7DELTA_BASE (milliradians): 16.1002 PROCESSING Starting on PROFILE Command at 8669.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T14:43:34.000 ) This is Command #8 from the Event List PROCESSING Starting on DELTA_BODY Command at 8673.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T14:43:38.000 ) This is Command #9 from the Event List QUANTIZED ANGLES: -2.684 0.000 0.000 mrad Profiled Maneuver time (seconds): 46.3375 Simulated Maneuver End Time (UTC): 2011-129T14:44:24.370 Turn Magnitude for 7DELTA_BODY (milliradians): 2.6655 PROCESSING Starting on PROFILE Command at 8720.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T14:44:25.000 ) This is Command #10 from the Event List PROCESSING Starting on DELTA_BASE Command at 8724.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T14:44:29.000 ) This is Command #11 from the Event List QUANTIZED ANGLES: 0.000 0.000 -16.010 mrad Profiled Maneuver time (seconds): 4002.8444 Simulated Maneuver End Time (UTC): 2011-129T15:51:11.870 Turn Magnitude for 7DELTA_BASE (milliradians): 16.0792 PROCESSING Starting on PROFILE Command at 12728.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T15:51:13.000 ) This is Command #12 from the Event List PROCESSING Starting on DELTA_BODY Command at 12732.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T15:51:17.000 ) This is Command #13 from the Event List QUANTIZED ANGLES: -2.684 0.000 0.000 mrad Profiled Maneuver time (seconds): 46.3375 Simulated Maneuver End Time (UTC): 2011-129T15:52:03.370 Turn Magnitude for 7DELTA_BODY (milliradians): 2.6677 PROCESSING Starting on PROFILE Command at 12779.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T15:52:04.000 ) This is Command #14 from the Event List PROCESSING Starting on DELTA_BASE Command at 12783.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T15:52:08.000 ) This is Command #15 from the Event List QUANTIZED ANGLES: 0.000 0.000 16.010 mrad Profiled Maneuver time (seconds): 4002.8866 Simulated Maneuver End Time (UTC): 2011-129T16:58:51.000 Turn Magnitude for 7DELTA_BASE (milliradians): 16.0646 PROCESSING Starting on PROFILE Command at 16787.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T16:58:52.000 ) This is Command #16 from the Event List PROCESSING Starting on DELTA_BODY Command at 16791.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T16:58:56.000 ) This is Command #17 from the Event List QUANTIZED ANGLES: -2.684 0.000 0.000 mrad Profiled Maneuver time (seconds): 46.3376 Simulated Maneuver End Time (UTC): 2011-129T16:59:42.370 Turn Magnitude for 7DELTA_BODY (milliradians): 2.6698 PROCESSING Starting on PROFILE Command at 16838.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T16:59:43.000 ) This is Command #18 from the Event List PROCESSING Starting on DELTA_BASE Command at 16842.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T16:59:47.000 ) This is Command #19 from the Event List QUANTIZED ANGLES: 0.000 0.000 -16.010 mrad Profiled Maneuver time (seconds): 4002.9000 Simulated Maneuver End Time (UTC): 2011-129T18:06:30.000 Turn Magnitude for 7DELTA_BASE (milliradians): 16.0486 PROCESSING Starting on PROFILE Command at 20846.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T18:06:31.000 ) This is Command #20 from the Event List PROCESSING Starting on DELTA_BODY Command at 20850.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T18:06:35.000 ) This is Command #21 from the Event List QUANTIZED ANGLES: -2.684 0.000 0.000 mrad Profiled Maneuver time (seconds): 46.3376 Simulated Maneuver End Time (UTC): 2011-129T18:07:21.370 Turn Magnitude for 7DELTA_BODY (milliradians): 2.6720 PROCESSING Starting on PROFILE Command at 20897.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T18:07:22.000 ) This is Command #22 from the Event List PROCESSING Starting on DELTA_BASE Command at 20901.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T18:07:26.000 ) This is Command #23 from the Event List QUANTIZED ANGLES: 0.000 0.000 16.010 mrad Profiled Maneuver time (seconds): 4002.8846 Simulated Maneuver End Time (UTC): 2011-129T19:14:09.000 Turn Magnitude for 7DELTA_BASE (milliradians): 16.0378 PROCESSING Starting on PROFILE Command at 24905.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T19:14:10.000 ) This is Command #24 from the Event List PROCESSING Starting on DELTA_BODY Command at 24909.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T19:14:14.000 ) This is Command #25 from the Event List QUANTIZED ANGLES: -2.684 0.000 0.000 mrad Profiled Maneuver time (seconds): 46.3377 Simulated Maneuver End Time (UTC): 2011-129T19:15:00.370 Turn Magnitude for 7DELTA_BODY (milliradians): 2.6744 PROCESSING Starting on PROFILE Command at 24956.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T19:15:01.000 ) This is Command #26 from the Event List PROCESSING Starting on DELTA_BASE Command at 24960.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T19:15:05.000 ) This is Command #27 from the Event List QUANTIZED ANGLES: 0.000 0.000 -16.010 mrad Profiled Maneuver time (seconds): 4002.8403 Simulated Maneuver End Time (UTC): 2011-129T20:21:47.870 Turn Magnitude for 7DELTA_BASE (milliradians): 16.0252 PROCESSING Starting on PROFILE Command at 29260.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T20:26:45.000 ) This is Command #28 from the Event List PROCESSING Starting on OFFSET Command at 29263.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T20:26:48.000 ) This is Command #29 from the Event List QUANTIZED ANGLES: -0.095 0.000 1.150 mrad Profiled Maneuver time (seconds): 54.3117 Simulated Maneuver End Time (UTC): 2011-129T20:27:42.370 Turn Magnitude for 7OFFSET (milliradians): 10.5753 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2011-129T21:02:10.000 PROCESSING Starting on PROFILE Command at 31579.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T21:05:24.000 ) This is Command #30 from the Event List PROCESSING Starting on TARGET Command at 31580.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T21:05:25.000 ) 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 31587.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T21:05:32.000 ) This is Command #32 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 44.2203 PROCESSING Starting on 89EXE_CMD_SEQ Command at 31615.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-129T21:06:00.000 ) This is Command #33 from the Event List Simulated Maneuver End Time (UTC): 2011-129T21:06:16.250 Turn Magnitude for 7OFFSET (milliradians): 5.8838 EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_1/kpt_eo.plt -----------------------------------