============ KPT ================= TIME: Fri Mar 14 14:29:20 2014 USER: Todd Ansty ================================== Insert Spice File: /cas/ancillary/ops/NAIF/sp/110818AP_SE_11175_17265.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/140127AP_RE_90165_18018.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/130528BP_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/cas00158.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_4/input.bvh Successfully Read IVT File: pdt_Run_4/input.ivt Successfully Read TLF File: /export/home/eros/D15.0.3d_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_4/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/140127AP_RE_90165_18018.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/130528BP_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/cas00158.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_4/input.bvh Successfully Read IVT File: pdt_Run_4/input.ivt Successfully Read TLF File: /export/home/eros/D15.0.3d_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_4/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: V14.2 ------------------------------ 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: 2014-265T16:53:23.000 Adding/Replacing Vector SKY_NEP to the IVT at UTC Time: 2014-265T16:53:24.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-265T17:23:13.000 ) 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): 2014-265T17:23:14.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN; SECONDARY BODY: NEG_X; SECONDARY INERTIAL: SKY_NEP; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2092.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-265T17:23:21.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: -0.095 0.000 1.150 mrad Profiled Maneuver time (seconds): 11.0039 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-265T17:23:19.000 ) This is Command #4 from the Event List Simulated Maneuver End Time (UTC): 2014-265T17:23:32.120 Turn Magnitude for 7OFFSET (milliradians): 0.5728 PROCESSING Starting on OFFSET Command at 2752.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-265T17:34:21.000 ) This is Command #5 from the Event List QUANTIZED ANGLES: -9.491 0.000 -9.970 mrad Profiled Maneuver time (seconds): 68.4287 Simulated Maneuver End Time (UTC): 2014-265T17:35:29.500 Turn Magnitude for 7OFFSET (milliradians): 14.6065 PROCESSING Starting on PROFILE Command at 2841.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-265T17:35:50.000 ) 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): 2014-265T17:35:54.000 ) This is Command #7 from the Event List QUANTIZED ANGLES: 0.000 0.000 6.519 mrad Profiled Maneuver time (seconds): 1629.8668 Simulated Maneuver End Time (UTC): 2014-265T18:03:03.870 Turn Magnitude for 7DELTA_BASE (milliradians): 6.2777 PROCESSING Starting on PROFILE Command at 4475.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-265T18:03:04.000 ) This is Command #8 from the Event List PROCESSING Starting on DELTA_BODY Command at 4479.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-265T18:03:08.000 ) This is Command #9 from the Event List QUANTIZED ANGLES: 2.588 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.9144 PROCESSING Starting on PROFILE Command at 4513.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-265T18:03:42.000 ) This is Command #10 from the Event List Simulated Maneuver End Time (UTC): 2014-265T18:03:42.000 Turn Magnitude for 7DELTA_BODY (milliradians): 2.5645 PROCESSING Starting on DELTA_BASE Command at 4517.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-265T18:03:46.000 ) This is Command #11 from the Event List QUANTIZED ANGLES: 0.000 0.000 -6.519 mrad Profiled Maneuver time (seconds): 1629.9207 PROCESSING Starting on PROFILE Command at 6147.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-265T18:30:56.000 ) This is Command #12 from the Event List Simulated Maneuver End Time (UTC): 2014-265T18:30:56.000 Turn Magnitude for 7DELTA_BASE (milliradians): 7.2420 PROCESSING Starting on DELTA_BODY Command at 6151.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-265T18:31:00.000 ) This is Command #13 from the Event List QUANTIZED ANGLES: 2.588 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.9144 PROCESSING Starting on PROFILE Command at 6185.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-265T18:31:34.000 ) This is Command #14 from the Event List Simulated Maneuver End Time (UTC): 2014-265T18:31:34.000 Turn Magnitude for 7DELTA_BODY (milliradians): 2.5645 PROCESSING Starting on DELTA_BASE Command at 6189.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-265T18:31:38.000 ) This is Command #15 from the Event List QUANTIZED ANGLES: 0.000 0.000 6.519 mrad Profiled Maneuver time (seconds): 1629.9258 PROCESSING Starting on PROFILE Command at 7819.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-265T18:58:48.000 ) This is Command #16 from the Event List Simulated Maneuver End Time (UTC): 2014-265T18:58:48.000 Turn Magnitude for 7DELTA_BASE (milliradians): 6.3109 PROCESSING Starting on DELTA_BODY Command at 7823.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-265T18:58:52.000 ) This is Command #17 from the Event List QUANTIZED ANGLES: 2.588 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.9144 PROCESSING Starting on PROFILE Command at 7857.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-265T18:59:26.000 ) This is Command #18 from the Event List Simulated Maneuver End Time (UTC): 2014-265T18:59:26.000 Turn Magnitude for 7DELTA_BODY (milliradians): 2.5649 PROCESSING Starting on DELTA_BASE Command at 7861.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-265T18:59:30.000 ) This is Command #19 from the Event List QUANTIZED ANGLES: 0.000 0.000 -6.519 mrad Profiled Maneuver time (seconds): 1629.9563 PROCESSING Starting on PROFILE Command at 9491.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-265T19:26:40.000 ) This is Command #20 from the Event List Simulated Maneuver End Time (UTC): 2014-265T19:26:40.000 Turn Magnitude for 7DELTA_BASE (milliradians): 7.1904 PROCESSING Starting on DELTA_BODY Command at 9495.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-265T19:26:44.000 ) This is Command #21 from the Event List QUANTIZED ANGLES: 2.588 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.9144 PROCESSING Starting on PROFILE Command at 9529.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-265T19:27:18.000 ) This is Command #22 from the Event List Simulated Maneuver End Time (UTC): 2014-265T19:27:18.000 Turn Magnitude for 7DELTA_BODY (milliradians): 2.5649 PROCESSING Starting on DELTA_BASE Command at 9533.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-265T19:27:22.000 ) This is Command #23 from the Event List QUANTIZED ANGLES: 0.000 0.000 6.519 mrad Profiled Maneuver time (seconds): 1629.9410 Simulated Maneuver End Time (UTC): 2014-265T19:54:32.000 Turn Magnitude for 7DELTA_BASE (milliradians): 6.3423 PROCESSING Starting on PROFILE Command at 11180.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-265T19:54:49.000 ) This is Command #24 from the Event List PROCESSING Starting on OFFSET Command at 11183.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-265T19:54:52.000 ) This is Command #25 from the Event List QUANTIZED ANGLES: 0.000 0.000 -23.968 mrad Profiled Maneuver time (seconds): 62.6640 Simulated Maneuver End Time (UTC): 2014-265T19:55:54.750 Turn Magnitude for 7OFFSET (milliradians): 20.5535 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2014-265T20:02:09.000 PROCESSING Starting on PROFILE Command at 11784.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-265T20:04:53.000 ) This is Command #26 from the Event List PROCESSING Starting on TARGET Command at 11785.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-265T20:04:54.000 ) This is Command #27 from the Event List PRIMARY BODY: NEG_Y; PRIMARY INERTIAL: TITAN; SECONDARY BODY: NEG_X; SECONDARY INERTIAL: SKY_NEP; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 11792.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-265T20:05:01.000 ) This is Command #28 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 69.9226 PROCESSING Starting on 89EXE_CMD_SEQ Command at 11850.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-265T20:05:59.000 ) This is Command #29 from the Event List Simulated Maneuver End Time (UTC): 2014-265T20:06:11.000 Turn Magnitude for 7OFFSET (milliradians): 25.6503 EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_4/kpt_eo.plt -----------------------------------