============ KPT ================= TIME: Mon Dec 14 13:17:45 2009 USER: Todd Ansty ================================== Insert Spice File: /cas/ancillary/ops/NAIF/sp/091005AP_SE_09248_17265.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/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/cpck07Oct2009.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_11May2009_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00137.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_6/input.bvh Successfully Read IVT File: pdt_Run_6/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_6/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/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/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/cpck07Oct2009.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_11May2009_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00137.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_6/input.bvh Successfully Read IVT File: pdt_Run_6/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_6/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: 2010-155T16:38:32.000 Adding/Replacing Vector TITAN_LAT_VIEW_130 to the IVT at UTC Time: 2010-155T17:03:07.000 Adding/Replacing Vector TITAN_FOV_LIMB_130 to the IVT at UTC Time: 2010-155T17:03:12.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T17:08:21.000 ) This is Command #1 from the Event List TARGET / Command #2: Primary Inertial Vector: TITAN_LAT_VIEW_130 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #2: Secondary Inertial Vector: TITAN_FOV_LIMB_130 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 2085.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T17:08:22.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_130; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_130; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2092.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T17:08:29.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 169.8051 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T17:08:27.000 ) This is Command #4 from the Event List Simulated Maneuver End Time (UTC): 2010-155T17:11:18.870 Turn Magnitude for 7OFFSET (milliradians): 85.5342 Adding/Replacing Vector TITAN_LAT_VIEW_131 to the IVT at UTC Time: 2010-155T17:15:37.000 Adding/Replacing Vector TITAN_FOV_LIMB_131 to the IVT at UTC Time: 2010-155T17:15:52.000 PROCESSING Starting on OFFSET Command at 2557.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T17:16:14.000 ) This is Command #5 from the Event List QUANTIZED ANGLES: 2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2810 Simulated Maneuver End Time (UTC): 2010-155T17:16:47.370 Turn Magnitude for 7OFFSET (milliradians): 2.5322 PROCESSING Starting on PROFILE Command at 2844.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T17:21:01.000 ) This is Command #6 from the Event List TARGET / Command #7: Primary Inertial Vector: TITAN_LAT_VIEW_131 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #7: Secondary Inertial Vector: TITAN_FOV_LIMB_131 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 2845.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T17:21:02.000 ) This is Command #7 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_131; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_131; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2852.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T17:21:09.000 ) This is Command #8 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 182.7586 Simulated Maneuver End Time (UTC): 2010-155T17:24:11.870 Turn Magnitude for 7OFFSET (milliradians): 100.2611 Adding/Replacing Vector TITAN_LAT_VIEW_132 to the IVT at UTC Time: 2010-155T17:28:07.000 Adding/Replacing Vector TITAN_FOV_LIMB_132 to the IVT at UTC Time: 2010-155T17:28:22.000 PROCESSING Starting on OFFSET Command at 3307.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T17:28:44.000 ) This is Command #9 from the Event List QUANTIZED ANGLES: 2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2810 Simulated Maneuver End Time (UTC): 2010-155T17:29:17.370 Turn Magnitude for 7OFFSET (milliradians): 2.5327 PROCESSING Starting on PROFILE Command at 3594.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T17:33:31.000 ) This is Command #10 from the Event List TARGET / Command #11: Primary Inertial Vector: TITAN_LAT_VIEW_132 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #11: Secondary Inertial Vector: TITAN_FOV_LIMB_132 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 3595.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T17:33:32.000 ) This is Command #11 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_132; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_132; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 3602.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T17:33:39.000 ) This is Command #12 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 174.0533 Simulated Maneuver End Time (UTC): 2010-155T17:36:33.120 Turn Magnitude for 7OFFSET (milliradians): 90.9094 Adding/Replacing Vector TITAN_LAT_VIEW_133 to the IVT at UTC Time: 2010-155T17:40:37.000 Adding/Replacing Vector TITAN_FOV_LIMB_133 to the IVT at UTC Time: 2010-155T17:40:52.000 PROCESSING Starting on OFFSET Command at 4057.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T17:41:14.000 ) This is Command #13 from the Event List QUANTIZED ANGLES: 2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2810 Simulated Maneuver End Time (UTC): 2010-155T17:41:47.370 Turn Magnitude for 7OFFSET (milliradians): 2.5335 PROCESSING Starting on PROFILE Command at 4344.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T17:46:01.000 ) This is Command #14 from the Event List TARGET / Command #15: Primary Inertial Vector: TITAN_LAT_VIEW_133 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #15: Secondary Inertial Vector: TITAN_FOV_LIMB_133 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 4345.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T17:46:02.000 ) This is Command #15 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_133; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_133; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 4352.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T17:46:09.000 ) This is Command #16 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 172.2926 Simulated Maneuver End Time (UTC): 2010-155T17:49:01.370 Turn Magnitude for 7OFFSET (milliradians): 89.0671 Adding/Replacing Vector TITAN_LAT_VIEW_134 to the IVT at UTC Time: 2010-155T17:53:07.000 Adding/Replacing Vector TITAN_FOV_LIMB_134 to the IVT at UTC Time: 2010-155T17:53:22.000 PROCESSING Starting on OFFSET Command at 4807.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T17:53:44.000 ) This is Command #17 from the Event List QUANTIZED ANGLES: 2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2810 Simulated Maneuver End Time (UTC): 2010-155T17:54:17.370 Turn Magnitude for 7OFFSET (milliradians): 2.5343 PROCESSING Starting on PROFILE Command at 5094.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T17:58:31.000 ) This is Command #18 from the Event List TARGET / Command #19: Primary Inertial Vector: TITAN_LAT_VIEW_134 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #19: Secondary Inertial Vector: TITAN_FOV_LIMB_134 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 5095.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T17:58:32.000 ) This is Command #19 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_134; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_134; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 5102.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T17:58:39.000 ) This is Command #20 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 171.6257 Simulated Maneuver End Time (UTC): 2010-155T18:01:30.750 Turn Magnitude for 7OFFSET (milliradians): 88.3720 Adding/Replacing Vector TITAN_LAT_VIEW_135 to the IVT at UTC Time: 2010-155T18:05:37.000 Adding/Replacing Vector TITAN_FOV_LIMB_135 to the IVT at UTC Time: 2010-155T18:05:52.000 PROCESSING Starting on OFFSET Command at 5557.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T18:06:14.000 ) This is Command #21 from the Event List QUANTIZED ANGLES: 2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2810 Simulated Maneuver End Time (UTC): 2010-155T18:06:47.370 Turn Magnitude for 7OFFSET (milliradians): 2.5350 PROCESSING Starting on PROFILE Command at 5844.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T18:11:01.000 ) This is Command #22 from the Event List TARGET / Command #23: Primary Inertial Vector: TITAN_LAT_VIEW_135 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #23: Secondary Inertial Vector: TITAN_FOV_LIMB_135 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 5845.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T18:11:02.000 ) This is Command #23 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_135; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_135; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 5852.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T18:11:09.000 ) This is Command #24 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 171.3028 Simulated Maneuver End Time (UTC): 2010-155T18:14:00.370 Turn Magnitude for 7OFFSET (milliradians): 88.0353 Adding/Replacing Vector TITAN_LAT_VIEW_136 to the IVT at UTC Time: 2010-155T18:18:07.000 Adding/Replacing Vector TITAN_FOV_LIMB_136 to the IVT at UTC Time: 2010-155T18:18:22.000 PROCESSING Starting on OFFSET Command at 6307.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T18:18:44.000 ) This is Command #25 from the Event List QUANTIZED ANGLES: 2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2810 Simulated Maneuver End Time (UTC): 2010-155T18:19:17.370 Turn Magnitude for 7OFFSET (milliradians): 2.5357 PROCESSING Starting on PROFILE Command at 6594.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T18:23:31.000 ) This is Command #26 from the Event List TARGET / Command #27: Primary Inertial Vector: TITAN_LAT_VIEW_136 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #27: Secondary Inertial Vector: TITAN_FOV_LIMB_136 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 6595.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T18:23:32.000 ) This is Command #27 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_136; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_136; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 6602.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T18:23:39.000 ) This is Command #28 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 171.1232 Simulated Maneuver End Time (UTC): 2010-155T18:26:30.120 Turn Magnitude for 7OFFSET (milliradians): 87.8477 Adding/Replacing Vector TITAN_LAT_VIEW_137 to the IVT at UTC Time: 2010-155T18:31:37.000 Adding/Replacing Vector TITAN_FOV_LIMB_137 to the IVT at UTC Time: 2010-155T18:31:52.000 PROCESSING Starting on OFFSET Command at 7117.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T18:32:14.000 ) This is Command #29 from the Event List QUANTIZED ANGLES: 2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2811 Simulated Maneuver End Time (UTC): 2010-155T18:32:47.370 Turn Magnitude for 7OFFSET (milliradians): 2.5365 PROCESSING Starting on PROFILE Command at 7404.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T18:37:01.000 ) This is Command #30 from the Event List TARGET / Command #31: Primary Inertial Vector: TITAN_LAT_VIEW_137 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #31: Secondary Inertial Vector: TITAN_FOV_LIMB_137 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 7405.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T18:37:02.000 ) This is Command #31 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_137; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_137; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 7412.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T18:37:09.000 ) This is Command #32 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 171.0128 Simulated Maneuver End Time (UTC): 2010-155T18:40:00.120 Turn Magnitude for 7OFFSET (milliradians): 87.7323 Adding/Replacing Vector TITAN_LAT_VIEW_138 to the IVT at UTC Time: 2010-155T18:45:07.000 Adding/Replacing Vector TITAN_FOV_LIMB_138 to the IVT at UTC Time: 2010-155T18:45:22.000 PROCESSING Starting on OFFSET Command at 7927.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T18:45:44.000 ) This is Command #33 from the Event List QUANTIZED ANGLES: 2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2811 Simulated Maneuver End Time (UTC): 2010-155T18:46:17.370 Turn Magnitude for 7OFFSET (milliradians): 2.5371 PROCESSING Starting on PROFILE Command at 8214.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T18:50:31.000 ) This is Command #34 from the Event List TARGET / Command #35: Primary Inertial Vector: TITAN_LAT_VIEW_138 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #35: Secondary Inertial Vector: TITAN_FOV_LIMB_138 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 8215.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T18:50:32.000 ) This is Command #35 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_138; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_138; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 8222.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T18:50:39.000 ) This is Command #36 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.9416 Simulated Maneuver End Time (UTC): 2010-155T18:53:30.000 Turn Magnitude for 7OFFSET (milliradians): 87.6577 Adding/Replacing Vector TITAN_LAT_VIEW_139 to the IVT at UTC Time: 2010-155T18:58:37.000 Adding/Replacing Vector TITAN_FOV_LIMB_139 to the IVT at UTC Time: 2010-155T18:58:52.000 PROCESSING Starting on OFFSET Command at 8737.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T18:59:14.000 ) This is Command #37 from the Event List QUANTIZED ANGLES: 2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2811 Simulated Maneuver End Time (UTC): 2010-155T18:59:47.370 Turn Magnitude for 7OFFSET (milliradians): 2.5377 PROCESSING Starting on PROFILE Command at 9024.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T19:04:01.000 ) This is Command #38 from the Event List TARGET / Command #39: Primary Inertial Vector: TITAN_LAT_VIEW_139 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #39: Secondary Inertial Vector: TITAN_FOV_LIMB_139 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 9025.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T19:04:02.000 ) This is Command #39 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_139; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_139; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 9032.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T19:04:09.000 ) This is Command #40 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.8937 Simulated Maneuver End Time (UTC): 2010-155T19:07:00.000 Turn Magnitude for 7OFFSET (milliradians): 87.6075 Adding/Replacing Vector TITAN_LAT_VIEW_140 to the IVT at UTC Time: 2010-155T19:12:07.000 Adding/Replacing Vector TITAN_FOV_LIMB_140 to the IVT at UTC Time: 2010-155T19:12:22.000 PROCESSING Starting on OFFSET Command at 9547.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T19:12:44.000 ) This is Command #41 from the Event List QUANTIZED ANGLES: 2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2811 Simulated Maneuver End Time (UTC): 2010-155T19:13:17.370 Turn Magnitude for 7OFFSET (milliradians): 2.5381 PROCESSING Starting on PROFILE Command at 9834.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T19:17:31.000 ) This is Command #42 from the Event List TARGET / Command #43: Primary Inertial Vector: TITAN_LAT_VIEW_140 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #43: Secondary Inertial Vector: TITAN_FOV_LIMB_140 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 9835.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T19:17:32.000 ) This is Command #43 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_140; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_140; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 9842.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T19:17:39.000 ) This is Command #44 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.8608 Simulated Maneuver End Time (UTC): 2010-155T19:20:29.870 Turn Magnitude for 7OFFSET (milliradians): 87.5729 Adding/Replacing Vector TITAN_LAT_VIEW_141 to the IVT at UTC Time: 2010-155T19:25:37.000 Adding/Replacing Vector TITAN_FOV_LIMB_141 to the IVT at UTC Time: 2010-155T19:25:52.000 PROCESSING Starting on OFFSET Command at 10357.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T19:26:14.000 ) This is Command #45 from the Event List QUANTIZED ANGLES: 2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2811 Simulated Maneuver End Time (UTC): 2010-155T19:26:47.370 Turn Magnitude for 7OFFSET (milliradians): 2.5383 PROCESSING Starting on PROFILE Command at 10644.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T19:31:01.000 ) This is Command #46 from the Event List TARGET / Command #47: Primary Inertial Vector: TITAN_LAT_VIEW_141 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #47: Secondary Inertial Vector: TITAN_FOV_LIMB_141 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 10645.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T19:31:02.000 ) This is Command #47 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_141; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_141; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 10652.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T19:31:09.000 ) This is Command #48 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.8380 Simulated Maneuver End Time (UTC): 2010-155T19:33:59.870 Turn Magnitude for 7OFFSET (milliradians): 87.5489 Adding/Replacing Vector TITAN_LAT_VIEW_142 to the IVT at UTC Time: 2010-155T19:39:07.000 Adding/Replacing Vector TITAN_FOV_LIMB_142 to the IVT at UTC Time: 2010-155T19:39:22.000 PROCESSING Starting on OFFSET Command at 11167.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T19:39:44.000 ) This is Command #49 from the Event List QUANTIZED ANGLES: 2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2811 Simulated Maneuver End Time (UTC): 2010-155T19:40:17.370 Turn Magnitude for 7OFFSET (milliradians): 2.5383 PROCESSING Starting on PROFILE Command at 11454.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T19:44:31.000 ) This is Command #50 from the Event List TARGET / Command #51: Primary Inertial Vector: TITAN_LAT_VIEW_142 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #51: Secondary Inertial Vector: TITAN_FOV_LIMB_142 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 11455.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T19:44:32.000 ) This is Command #51 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_142; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_142; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 11462.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T19:44:39.000 ) This is Command #52 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.8224 Simulated Maneuver End Time (UTC): 2010-155T19:47:29.870 Turn Magnitude for 7OFFSET (milliradians): 87.5324 Adding/Replacing Vector TITAN_LAT_VIEW_143 to the IVT at UTC Time: 2010-155T19:52:37.000 Adding/Replacing Vector TITAN_FOV_LIMB_143 to the IVT at UTC Time: 2010-155T19:52:52.000 PROCESSING Starting on OFFSET Command at 11977.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T19:53:14.000 ) This is Command #53 from the Event List QUANTIZED ANGLES: 2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2811 Simulated Maneuver End Time (UTC): 2010-155T19:53:47.370 Turn Magnitude for 7OFFSET (milliradians): 2.5380 PROCESSING Starting on PROFILE Command at 12264.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T19:58:01.000 ) This is Command #54 from the Event List TARGET / Command #55: Primary Inertial Vector: TITAN_LAT_VIEW_143 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #55: Secondary Inertial Vector: TITAN_FOV_LIMB_143 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 12265.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T19:58:02.000 ) This is Command #55 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_143; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_143; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 12272.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T19:58:09.000 ) This is Command #56 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.8122 Simulated Maneuver End Time (UTC): 2010-155T20:00:59.870 Turn Magnitude for 7OFFSET (milliradians): 87.5215 Adding/Replacing Vector TITAN_LAT_VIEW_144 to the IVT at UTC Time: 2010-155T20:06:07.000 Adding/Replacing Vector TITAN_FOV_LIMB_144 to the IVT at UTC Time: 2010-155T20:06:22.000 PROCESSING Starting on OFFSET Command at 12787.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T20:06:44.000 ) This is Command #57 from the Event List QUANTIZED ANGLES: 2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2811 Simulated Maneuver End Time (UTC): 2010-155T20:07:17.370 Turn Magnitude for 7OFFSET (milliradians): 2.5375 PROCESSING Starting on PROFILE Command at 13074.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T20:11:31.000 ) This is Command #58 from the Event List TARGET / Command #59: Primary Inertial Vector: TITAN_LAT_VIEW_144 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #59: Secondary Inertial Vector: TITAN_FOV_LIMB_144 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 13075.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T20:11:32.000 ) This is Command #59 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_144; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_144; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 13082.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T20:11:39.000 ) This is Command #60 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.8062 Simulated Maneuver End Time (UTC): 2010-155T20:14:29.870 Turn Magnitude for 7OFFSET (milliradians): 87.5152 Adding/Replacing Vector TITAN_LAT_VIEW_145 to the IVT at UTC Time: 2010-155T20:19:37.000 Adding/Replacing Vector TITAN_FOV_LIMB_145 to the IVT at UTC Time: 2010-155T20:19:52.000 PROCESSING Starting on OFFSET Command at 13597.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T20:20:14.000 ) This is Command #61 from the Event List QUANTIZED ANGLES: 2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2810 Simulated Maneuver End Time (UTC): 2010-155T20:20:47.370 Turn Magnitude for 7OFFSET (milliradians): 2.5366 PROCESSING Starting on PROFILE Command at 13884.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T20:25:01.000 ) This is Command #62 from the Event List TARGET / Command #63: Primary Inertial Vector: TITAN_LAT_VIEW_145 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #63: Secondary Inertial Vector: TITAN_FOV_LIMB_145 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 13885.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T20:25:02.000 ) This is Command #63 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_145; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_145; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 13892.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T20:25:09.000 ) This is Command #64 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.8037 Simulated Maneuver End Time (UTC): 2010-155T20:27:59.870 Turn Magnitude for 7OFFSET (milliradians): 87.5126 Adding/Replacing Vector TITAN_LAT_VIEW_146 to the IVT at UTC Time: 2010-155T20:33:07.000 Adding/Replacing Vector TITAN_FOV_LIMB_146 to the IVT at UTC Time: 2010-155T20:33:22.000 PROCESSING Starting on OFFSET Command at 14407.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T20:33:44.000 ) This is Command #65 from the Event List QUANTIZED ANGLES: 2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2810 Simulated Maneuver End Time (UTC): 2010-155T20:34:17.370 Turn Magnitude for 7OFFSET (milliradians): 2.5352 PROCESSING Starting on PROFILE Command at 14694.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T20:38:31.000 ) This is Command #66 from the Event List TARGET / Command #67: Primary Inertial Vector: TITAN_LAT_VIEW_146 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #67: Secondary Inertial Vector: TITAN_FOV_LIMB_146 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 14695.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T20:38:32.000 ) This is Command #67 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_146; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_146; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 14702.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T20:38:39.000 ) This is Command #68 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.8045 Simulated Maneuver End Time (UTC): 2010-155T20:41:29.870 Turn Magnitude for 7OFFSET (milliradians): 87.5132 Adding/Replacing Vector TITAN_LAT_VIEW_147 to the IVT at UTC Time: 2010-155T20:46:37.000 Adding/Replacing Vector TITAN_FOV_LIMB_147 to the IVT at UTC Time: 2010-155T20:46:52.000 PROCESSING Starting on OFFSET Command at 15217.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T20:47:14.000 ) This is Command #69 from the Event List QUANTIZED ANGLES: 2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2810 Simulated Maneuver End Time (UTC): 2010-155T20:47:47.370 Turn Magnitude for 7OFFSET (milliradians): 2.5335 PROCESSING Starting on PROFILE Command at 15504.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T20:52:01.000 ) This is Command #70 from the Event List TARGET / Command #71: Primary Inertial Vector: TITAN_LAT_VIEW_147 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #71: Secondary Inertial Vector: TITAN_FOV_LIMB_147 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 15505.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T20:52:02.000 ) This is Command #71 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_147; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_147; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 15512.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T20:52:09.000 ) This is Command #72 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.8081 Simulated Maneuver End Time (UTC): 2010-155T20:54:59.870 Turn Magnitude for 7OFFSET (milliradians): 87.5170 PROCESSING Starting on OFFSET Command at 16027.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T21:00:44.000 ) This is Command #73 from the Event List QUANTIZED ANGLES: 2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2809 Adding/Replacing Vector TITAN to the IVT at UTC Time: 2010-155T21:01:02.000 Simulated Maneuver End Time (UTC): 2010-155T21:01:17.370 Turn Magnitude for 7OFFSET (milliradians): 2.5312 PROCESSING Starting on PROFILE Command at 16334.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T21:05:51.000 ) This is Command #74 from the Event List PROCESSING Starting on TARGET Command at 16335.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T21:05:52.000 ) This is Command #75 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 16342.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T21:05:59.000 ) This is Command #76 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 1190.5599 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2010-155T21:21:37.000 PROCESSING Starting on 89EXE_CMD_SEQ Command at 17510.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-155T21:25:27.000 ) This is Command #77 from the Event List Simulated Maneuver End Time (UTC): 2010-155T21:25:49.620 Turn Magnitude for 7OFFSET (milliradians): 1631.0197 EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_6/kpt_eo.plt -----------------------------------