============ KPT ================= TIME: Fri Nov 11 12:36:13 2011 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/naif0009.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/cas00149.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_12/input.bvh Successfully Read IVT File: pdt_Run_12/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_12/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/naif0009.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/cas00149.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_12/input.bvh Successfully Read IVT File: pdt_Run_12/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_12/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: 2012-158T07:54:04.000 Adding/Replacing Vector SKY_RA_DEC_178 to the IVT at UTC Time: 2012-158T07:54:05.000 Adding/Replacing Vector TITAN_N_POLE_DIR to the IVT at UTC Time: 2012-158T08:19:05.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T08:23:54.000 ) 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): 2012-158T08:23:55.000 ) 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): 2012-158T08:24:02.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 7.957 0.000 -9.012 mrad Profiled Maneuver time (seconds): 454.1928 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T08:24:00.000 ) This is Command #4 from the Event List Simulated Maneuver End Time (UTC): 2012-158T08:31:36.250 Turn Magnitude for 7OFFSET (milliradians): 603.0832 PROCESSING Starting on PROFILE Command at 2602.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T08:32:32.000 ) This is Command #5 from the Event List PROCESSING Starting on DELTA_BASE Command at 2606.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T08:32:36.000 ) This is Command #6 from the Event List QUANTIZED ANGLES: 0.000 0.000 8.916 mrad Profiled Maneuver time (seconds): 991.5409 Simulated Maneuver End Time (UTC): 2012-158T08:49:07.620 Turn Magnitude for 7DELTA_BASE (milliradians): 9.3158 PROCESSING Starting on PROFILE Command at 3598.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T08:49:08.000 ) This is Command #7 from the Event List PROCESSING Starting on DELTA_BODY Command at 3602.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T08:49:12.000 ) This is Command #8 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 44.6494 Simulated Maneuver End Time (UTC): 2012-158T08:49:56.750 Turn Magnitude for 7DELTA_BODY (milliradians): 2.4768 PROCESSING Starting on PROFILE Command at 3647.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T08:49:57.000 ) This is Command #9 from the Event List PROCESSING Starting on DELTA_BASE Command at 3651.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T08:50:01.000 ) This is Command #10 from the Event List QUANTIZED ANGLES: 0.000 0.000 -8.916 mrad Profiled Maneuver time (seconds): 991.5464 Simulated Maneuver End Time (UTC): 2012-158T09:06:32.620 Turn Magnitude for 7DELTA_BASE (milliradians): 8.5308 PROCESSING Starting on PROFILE Command at 4643.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T09:06:33.000 ) This is Command #11 from the Event List PROCESSING Starting on DELTA_BODY Command at 4647.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T09:06:37.000 ) This is Command #12 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 44.6494 Simulated Maneuver End Time (UTC): 2012-158T09:07:21.750 Turn Magnitude for 7DELTA_BODY (milliradians): 2.4775 PROCESSING Starting on PROFILE Command at 4692.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T09:07:22.000 ) This is Command #13 from the Event List PROCESSING Starting on DELTA_BASE Command at 4696.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T09:07:26.000 ) This is Command #14 from the Event List QUANTIZED ANGLES: 0.000 0.000 8.916 mrad Profiled Maneuver time (seconds): 991.5678 Simulated Maneuver End Time (UTC): 2012-158T09:23:57.620 Turn Magnitude for 7DELTA_BASE (milliradians): 9.3119 PROCESSING Starting on PROFILE Command at 5688.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T09:23:58.000 ) This is Command #15 from the Event List PROCESSING Starting on DELTA_BODY Command at 5692.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T09:24:02.000 ) This is Command #16 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 44.6494 Simulated Maneuver End Time (UTC): 2012-158T09:24:46.750 Turn Magnitude for 7DELTA_BODY (milliradians): 2.4783 PROCESSING Starting on PROFILE Command at 5737.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T09:24:47.000 ) This is Command #17 from the Event List PROCESSING Starting on DELTA_BASE Command at 5741.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T09:24:51.000 ) This is Command #18 from the Event List QUANTIZED ANGLES: 0.000 0.000 -8.916 mrad Profiled Maneuver time (seconds): 991.5611 Simulated Maneuver End Time (UTC): 2012-158T09:41:22.620 Turn Magnitude for 7DELTA_BASE (milliradians): 8.5314 PROCESSING Starting on PROFILE Command at 6733.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T09:41:23.000 ) This is Command #19 from the Event List PROCESSING Starting on DELTA_BODY Command at 6737.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T09:41:27.000 ) This is Command #20 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 44.6494 Simulated Maneuver End Time (UTC): 2012-158T09:42:11.750 Turn Magnitude for 7DELTA_BODY (milliradians): 2.4790 PROCESSING Starting on PROFILE Command at 6782.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T09:42:12.000 ) This is Command #21 from the Event List PROCESSING Starting on DELTA_BASE Command at 6786.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T09:42:16.000 ) This is Command #22 from the Event List QUANTIZED ANGLES: 0.000 0.000 8.916 mrad Profiled Maneuver time (seconds): 991.5701 Simulated Maneuver End Time (UTC): 2012-158T09:58:47.620 Turn Magnitude for 7DELTA_BASE (milliradians): 9.3100 PROCESSING Starting on PROFILE Command at 7778.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T09:58:48.000 ) This is Command #23 from the Event List PROCESSING Starting on DELTA_BODY Command at 7782.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T09:58:52.000 ) This is Command #24 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 44.6494 Simulated Maneuver End Time (UTC): 2012-158T09:59:36.750 Turn Magnitude for 7DELTA_BODY (milliradians): 2.4798 PROCESSING Starting on PROFILE Command at 7827.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T09:59:37.000 ) This is Command #25 from the Event List PROCESSING Starting on DELTA_BASE Command at 7831.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T09:59:41.000 ) This is Command #26 from the Event List QUANTIZED ANGLES: 0.000 0.000 -8.916 mrad Profiled Maneuver time (seconds): 991.5512 Simulated Maneuver End Time (UTC): 2012-158T10:16:12.620 Turn Magnitude for 7DELTA_BASE (milliradians): 8.5300 PROCESSING Starting on PROFILE Command at 8823.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T10:16:13.000 ) This is Command #27 from the Event List PROCESSING Starting on DELTA_BODY Command at 8827.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T10:16:17.000 ) This is Command #28 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 44.6495 Simulated Maneuver End Time (UTC): 2012-158T10:17:01.750 Turn Magnitude for 7DELTA_BODY (milliradians): 2.4806 PROCESSING Starting on PROFILE Command at 8872.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T10:17:02.000 ) This is Command #29 from the Event List PROCESSING Starting on DELTA_BASE Command at 8876.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T10:17:06.000 ) This is Command #30 from the Event List QUANTIZED ANGLES: 0.000 0.000 8.916 mrad Profiled Maneuver time (seconds): 991.5480 Simulated Maneuver End Time (UTC): 2012-158T10:33:37.620 Turn Magnitude for 7DELTA_BASE (milliradians): 9.3104 PROCESSING Starting on PROFILE Command at 9868.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T10:33:38.000 ) This is Command #31 from the Event List PROCESSING Starting on DELTA_BODY Command at 9872.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T10:33:42.000 ) This is Command #32 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 44.6495 Simulated Maneuver End Time (UTC): 2012-158T10:34:26.750 Turn Magnitude for 7DELTA_BODY (milliradians): 2.4814 PROCESSING Starting on PROFILE Command at 9917.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T10:34:27.000 ) This is Command #33 from the Event List PROCESSING Starting on DELTA_BASE Command at 9921.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T10:34:31.000 ) This is Command #34 from the Event List QUANTIZED ANGLES: 0.000 0.000 -8.916 mrad Profiled Maneuver time (seconds): 991.5168 Simulated Maneuver End Time (UTC): 2012-158T10:51:02.620 Turn Magnitude for 7DELTA_BASE (milliradians): 8.5263 Adding/Replacing Vector SKY_RA_DEC_179 to the IVT at UTC Time: 2012-158T10:53:56.000 PROCESSING Starting on PROFILE Command at 11375.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T10:58:45.000 ) This is Command #35 from the Event List PROCESSING Starting on TARGET Command at 11376.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T10:58:46.000 ) This is Command #36 from the Event List PRIMARY BODY: NEG_Y; PRIMARY INERTIAL: TITAN; SECONDARY BODY: NEG_X; SECONDARY INERTIAL: SKY_RA_DEC_179; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 11383.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T10:58:53.000 ) This is Command #37 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 454.2970 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2012-158T11:02:31.000 PROCESSING Starting on 89EXE_CMD_SEQ Command at 11831.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-158T11:06:21.000 ) This is Command #38 from the Event List Simulated Maneuver End Time (UTC): 2012-158T11:06:27.370 Turn Magnitude for 7OFFSET (milliradians): 603.4120 EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_12/kpt_eo.plt -----------------------------------