============ KPT ================= TIME: Mon Sep 14 11:03:27 2009 USER: Todd Ansty ================================== Insert Spice File: /cas/ancillary/ops/NAIF/sp/080806AP_SE_08138_10182.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/090507AP_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/080806AP_PE_08138_10182.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/080806AP_SK_08138_10182.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0009.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck15May2008.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_11May2009_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00133.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/PDT13.4d/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/080806AP_SE_08138_10182.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/090507AP_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/080806AP_PE_08138_10182.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/080806AP_SK_08138_10182.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0009.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck15May2008.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_11May2009_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00133.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/PDT13.4d/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: V13.2 ------------------------------ 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: 2009-361T09:37:29.000 Adding/Replacing Vector SKY_RA_DEC_130 to the IVT at UTC Time: 2009-361T10:02:29.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T10:07:18.000 ) 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): 2009-361T10:07:19.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN; SECONDARY BODY: POS_X; SECONDARY INERTIAL: SKY_RA_DEC_130; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2092.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T10:07:26.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 7.957 -87.245 -10.737 mrad Profiled Maneuver time (seconds): 460.0820 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T10:07:24.000 ) This is Command #4 from the Event List Simulated Maneuver End Time (UTC): 2009-361T10:15:06.250 Turn Magnitude for 7OFFSET (milliradians): 617.4769 PROCESSING Starting on PROFILE Command at 2632.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T10:16:26.000 ) This is Command #5 from the Event List PROCESSING Starting on DELTA_BASE Command at 2636.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T10:16:30.000 ) This is Command #6 from the Event List QUANTIZED ANGLES: 0.000 0.000 21.475 mrad Profiled Maneuver time (seconds): 1646.9067 Simulated Maneuver End Time (UTC): 2009-361T10:43:57.120 Turn Magnitude for 7DELTA_BASE (milliradians): 21.3454 PROCESSING Starting on PROFILE Command at 4290.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T10:44:04.000 ) This is Command #7 from the Event List PROCESSING Starting on DELTA_BODY Command at 4294.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T10:44:08.000 ) This is Command #8 from the Event List QUANTIZED ANGLES: -2.684 0.000 0.000 mrad Profiled Maneuver time (seconds): 46.3372 Simulated Maneuver End Time (UTC): 2009-361T10:44:54.500 Turn Magnitude for 7DELTA_BODY (milliradians): 2.6563 PROCESSING Starting on PROFILE Command at 4341.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T10:44:55.000 ) This is Command #9 from the Event List PROCESSING Starting on DELTA_BASE Command at 4345.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T10:44:59.000 ) This is Command #10 from the Event List QUANTIZED ANGLES: 0.000 0.000 -21.475 mrad Profiled Maneuver time (seconds): 1646.9407 Simulated Maneuver End Time (UTC): 2009-361T11:12:26.120 Turn Magnitude for 7DELTA_BASE (milliradians): 21.6137 PROCESSING Starting on PROFILE Command at 5999.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T11:12:33.000 ) This is Command #11 from the Event List PROCESSING Starting on DELTA_BODY Command at 6003.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T11:12:37.000 ) This is Command #12 from the Event List QUANTIZED ANGLES: -2.684 0.000 0.000 mrad Profiled Maneuver time (seconds): 46.3372 Simulated Maneuver End Time (UTC): 2009-361T11:13:23.500 Turn Magnitude for 7DELTA_BODY (milliradians): 2.6561 PROCESSING Starting on PROFILE Command at 6050.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T11:13:24.000 ) This is Command #13 from the Event List PROCESSING Starting on DELTA_BASE Command at 6054.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T11:13:28.000 ) This is Command #14 from the Event List QUANTIZED ANGLES: 0.000 0.000 21.475 mrad Profiled Maneuver time (seconds): 1646.9579 Simulated Maneuver End Time (UTC): 2009-361T11:40:55.120 Turn Magnitude for 7DELTA_BASE (milliradians): 21.4231 PROCESSING Starting on PROFILE Command at 7708.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T11:41:02.000 ) This is Command #15 from the Event List PROCESSING Starting on DELTA_BODY Command at 7712.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T11:41:06.000 ) This is Command #16 from the Event List QUANTIZED ANGLES: -2.684 0.000 0.000 mrad Profiled Maneuver time (seconds): 46.3372 Simulated Maneuver End Time (UTC): 2009-361T11:41:52.500 Turn Magnitude for 7DELTA_BODY (milliradians): 2.6558 PROCESSING Starting on PROFILE Command at 7759.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T11:41:53.000 ) This is Command #17 from the Event List PROCESSING Starting on DELTA_BASE Command at 7763.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T11:41:57.000 ) This is Command #18 from the Event List QUANTIZED ANGLES: 0.000 0.000 -21.475 mrad Profiled Maneuver time (seconds): 1646.9674 Simulated Maneuver End Time (UTC): 2009-361T12:09:24.120 Turn Magnitude for 7DELTA_BASE (milliradians): 21.5309 PROCESSING Starting on PROFILE Command at 9417.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T12:09:31.000 ) This is Command #19 from the Event List PROCESSING Starting on DELTA_BODY Command at 9421.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T12:09:35.000 ) This is Command #20 from the Event List QUANTIZED ANGLES: -2.684 0.000 0.000 mrad Profiled Maneuver time (seconds): 46.3372 Simulated Maneuver End Time (UTC): 2009-361T12:10:21.500 Turn Magnitude for 7DELTA_BODY (milliradians): 2.6554 PROCESSING Starting on PROFILE Command at 9468.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T12:10:22.000 ) This is Command #21 from the Event List PROCESSING Starting on DELTA_BASE Command at 9472.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T12:10:26.000 ) This is Command #22 from the Event List QUANTIZED ANGLES: 0.000 0.000 21.475 mrad Profiled Maneuver time (seconds): 1646.9618 Simulated Maneuver End Time (UTC): 2009-361T12:37:53.120 Turn Magnitude for 7DELTA_BASE (milliradians): 21.5140 PROCESSING Starting on PROFILE Command at 11126.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T12:38:00.000 ) This is Command #23 from the Event List PROCESSING Starting on DELTA_BODY Command at 11130.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T12:38:04.000 ) This is Command #24 from the Event List QUANTIZED ANGLES: -2.684 0.000 0.000 mrad Profiled Maneuver time (seconds): 46.3372 Simulated Maneuver End Time (UTC): 2009-361T12:38:50.500 Turn Magnitude for 7DELTA_BODY (milliradians): 2.6549 PROCESSING Starting on PROFILE Command at 11177.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T12:38:51.000 ) This is Command #25 from the Event List PROCESSING Starting on DELTA_BASE Command at 11181.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T12:38:55.000 ) This is Command #26 from the Event List QUANTIZED ANGLES: 0.000 0.000 -21.475 mrad Profiled Maneuver time (seconds): 1646.9467 Simulated Maneuver End Time (UTC): 2009-361T13:06:22.120 Turn Magnitude for 7DELTA_BASE (milliradians): 21.4344 PROCESSING Starting on PROFILE Command at 12835.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T13:06:29.000 ) This is Command #27 from the Event List PROCESSING Starting on DELTA_BODY Command at 12839.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T13:06:33.000 ) This is Command #28 from the Event List QUANTIZED ANGLES: -2.684 0.000 0.000 mrad Profiled Maneuver time (seconds): 46.3372 Simulated Maneuver End Time (UTC): 2009-361T13:07:19.500 Turn Magnitude for 7DELTA_BODY (milliradians): 2.6543 PROCESSING Starting on PROFILE Command at 12886.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T13:07:20.000 ) This is Command #29 from the Event List PROCESSING Starting on DELTA_BASE Command at 12890.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T13:07:24.000 ) This is Command #30 from the Event List QUANTIZED ANGLES: 0.000 0.000 21.475 mrad Profiled Maneuver time (seconds): 1646.9186 Simulated Maneuver End Time (UTC): 2009-361T13:34:51.120 Turn Magnitude for 7DELTA_BASE (milliradians): 21.6226 PROCESSING Starting on PROFILE Command at 14544.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T13:34:58.000 ) This is Command #31 from the Event List PROCESSING Starting on DELTA_BODY Command at 14548.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T13:35:02.000 ) This is Command #32 from the Event List QUANTIZED ANGLES: -2.684 0.000 0.000 mrad Profiled Maneuver time (seconds): 46.3372 Simulated Maneuver End Time (UTC): 2009-361T13:35:48.500 Turn Magnitude for 7DELTA_BODY (milliradians): 2.6535 PROCESSING Starting on PROFILE Command at 14595.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T13:35:49.000 ) This is Command #33 from the Event List PROCESSING Starting on DELTA_BASE Command at 14599.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T13:35:53.000 ) This is Command #34 from the Event List QUANTIZED ANGLES: 0.000 0.000 -21.475 mrad Profiled Maneuver time (seconds): 1646.8787 Simulated Maneuver End Time (UTC): 2009-361T14:03:20.120 Turn Magnitude for 7DELTA_BASE (milliradians): 21.3195 PROCESSING Starting on PROFILE Command at 16519.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T14:07:53.000 ) This is Command #35 from the Event List PROCESSING Starting on TARGET Command at 16520.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T14:07:54.000 ) This is Command #36 from the Event List PRIMARY BODY: NEG_Y; PRIMARY INERTIAL: TITAN; SECONDARY BODY: NEG_X; SECONDARY INERTIAL: SUN; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 16527.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T14:08:01.000 ) This is Command #37 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 457.1121 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2009-361T14:12:09.000 Simulated Maneuver End Time (UTC): 2009-361T14:15:38.250 Turn Magnitude for 7OFFSET (milliradians): 610.2010 PROCESSING Starting on 89EXE_CMD_SEQ Command at 17005.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-361T14:15:59.000 ) This is Command #38 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 -----------------------------------