============ KPT ================= TIME: Mon Dec 14 13:45:31 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_9/input.bvh Successfully Read IVT File: pdt_Run_9/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_9/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_9/input.bvh Successfully Read IVT File: pdt_Run_9/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_9/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: 2010-171T15:57:48.000 Adding/Replacing Vector TITAN_LAT_VIEW_148 to the IVT at UTC Time: 2010-171T16:22:23.000 Adding/Replacing Vector TITAN_FOV_LIMB_148 to the IVT at UTC Time: 2010-171T16:22:28.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T16:27:37.000 ) This is Command #1 from the Event List TARGET / Command #2: Primary Inertial Vector: TITAN_LAT_VIEW_148 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #2: Secondary Inertial Vector: TITAN_FOV_LIMB_148 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): 2010-171T16:27:38.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_148; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_148; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2092.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T16:27:45.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 1235.2449 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T16:27:43.000 ) This is Command #4 from the Event List Simulated Maneuver End Time (UTC): 2010-171T16:48:20.250 Turn Magnitude for 7OFFSET (milliradians): 1704.7176 PROCESSING Starting on PROFILE Command at 3360.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T16:48:53.000 ) This is Command #5 from the Event List Adding/Replacing Vector TITAN_LAT_VIEW_149 to the IVT at UTC Time: 2010-171T16:52:43.000 Adding/Replacing Vector TITAN_FOV_LIMB_149 to the IVT at UTC Time: 2010-171T16:52:58.000 PROCESSING Starting on OFFSET Command at 3622.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T16:53:15.000 ) This is Command #6 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2806 Simulated Maneuver End Time (UTC): 2010-171T16:53:48.370 Turn Magnitude for 7OFFSET (milliradians): 2.5189 PROCESSING Starting on PROFILE Command at 3914.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T16:58:07.000 ) This is Command #7 from the Event List TARGET / Command #8: Primary Inertial Vector: TITAN_LAT_VIEW_149 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #8: Secondary Inertial Vector: TITAN_FOV_LIMB_149 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 3915.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T16:58:08.000 ) This is Command #8 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_149; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_149; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 3922.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T16:58:15.000 ) This is Command #9 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6643 Simulated Maneuver End Time (UTC): 2010-171T17:01:05.750 Turn Magnitude for 7OFFSET (milliradians): 87.3534 Adding/Replacing Vector TITAN_LAT_VIEW_150 to the IVT at UTC Time: 2010-171T17:05:23.000 Adding/Replacing Vector TITAN_FOV_LIMB_150 to the IVT at UTC Time: 2010-171T17:05:38.000 PROCESSING Starting on OFFSET Command at 4382.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T17:05:55.000 ) This is Command #10 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2806 Simulated Maneuver End Time (UTC): 2010-171T17:06:28.370 Turn Magnitude for 7OFFSET (milliradians): 2.5172 PROCESSING Starting on PROFILE Command at 4674.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T17:10:47.000 ) This is Command #11 from the Event List TARGET / Command #12: Primary Inertial Vector: TITAN_LAT_VIEW_150 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #12: Secondary Inertial Vector: TITAN_FOV_LIMB_150 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 4675.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T17:10:48.000 ) This is Command #12 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_150; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_150; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 4682.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T17:10:55.000 ) This is Command #13 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6618 Simulated Maneuver End Time (UTC): 2010-171T17:13:45.750 Turn Magnitude for 7OFFSET (milliradians): 87.3517 Adding/Replacing Vector TITAN_LAT_VIEW_151 to the IVT at UTC Time: 2010-171T17:18:03.000 Adding/Replacing Vector TITAN_FOV_LIMB_151 to the IVT at UTC Time: 2010-171T17:18:18.000 PROCESSING Starting on OFFSET Command at 5142.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T17:18:35.000 ) This is Command #14 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2805 Simulated Maneuver End Time (UTC): 2010-171T17:19:08.370 Turn Magnitude for 7OFFSET (milliradians): 2.5152 PROCESSING Starting on PROFILE Command at 5434.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T17:23:27.000 ) This is Command #15 from the Event List TARGET / Command #16: Primary Inertial Vector: TITAN_LAT_VIEW_151 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #16: Secondary Inertial Vector: TITAN_FOV_LIMB_151 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 5435.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T17:23:28.000 ) This is Command #16 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_151; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_151; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 5442.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T17:23:35.000 ) This is Command #17 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6599 Simulated Maneuver End Time (UTC): 2010-171T17:26:25.750 Turn Magnitude for 7OFFSET (milliradians): 87.3506 Adding/Replacing Vector TITAN_LAT_VIEW_152 to the IVT at UTC Time: 2010-171T17:30:43.000 Adding/Replacing Vector TITAN_FOV_LIMB_152 to the IVT at UTC Time: 2010-171T17:30:58.000 PROCESSING Starting on OFFSET Command at 5902.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T17:31:15.000 ) This is Command #18 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2805 Simulated Maneuver End Time (UTC): 2010-171T17:31:48.370 Turn Magnitude for 7OFFSET (milliradians): 2.5131 PROCESSING Starting on PROFILE Command at 6194.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T17:36:07.000 ) This is Command #19 from the Event List TARGET / Command #20: Primary Inertial Vector: TITAN_LAT_VIEW_152 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #20: Secondary Inertial Vector: TITAN_FOV_LIMB_152 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 6195.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T17:36:08.000 ) This is Command #20 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_152; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_152; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 6202.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T17:36:15.000 ) This is Command #21 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6584 Simulated Maneuver End Time (UTC): 2010-171T17:39:05.750 Turn Magnitude for 7OFFSET (milliradians): 87.3502 Adding/Replacing Vector TITAN_LAT_VIEW_153 to the IVT at UTC Time: 2010-171T17:43:23.000 Adding/Replacing Vector TITAN_FOV_LIMB_153 to the IVT at UTC Time: 2010-171T17:43:38.000 PROCESSING Starting on OFFSET Command at 6662.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T17:43:55.000 ) This is Command #22 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2804 Simulated Maneuver End Time (UTC): 2010-171T17:44:28.370 Turn Magnitude for 7OFFSET (milliradians): 2.5108 PROCESSING Starting on PROFILE Command at 6954.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T17:48:47.000 ) This is Command #23 from the Event List TARGET / Command #24: Primary Inertial Vector: TITAN_LAT_VIEW_153 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #24: Secondary Inertial Vector: TITAN_FOV_LIMB_153 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 6955.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T17:48:48.000 ) This is Command #24 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_153; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_153; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 6962.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T17:48:55.000 ) This is Command #25 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6576 Simulated Maneuver End Time (UTC): 2010-171T17:51:45.750 Turn Magnitude for 7OFFSET (milliradians): 87.3504 Adding/Replacing Vector TITAN_LAT_VIEW_154 to the IVT at UTC Time: 2010-171T17:56:03.000 Adding/Replacing Vector TITAN_FOV_LIMB_154 to the IVT at UTC Time: 2010-171T17:56:18.000 PROCESSING Starting on OFFSET Command at 7422.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T17:56:35.000 ) This is Command #26 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2804 Simulated Maneuver End Time (UTC): 2010-171T17:57:08.370 Turn Magnitude for 7OFFSET (milliradians): 2.5083 PROCESSING Starting on PROFILE Command at 7714.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T18:01:27.000 ) This is Command #27 from the Event List TARGET / Command #28: Primary Inertial Vector: TITAN_LAT_VIEW_154 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #28: Secondary Inertial Vector: TITAN_FOV_LIMB_154 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 7715.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T18:01:28.000 ) This is Command #28 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_154; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_154; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 7722.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T18:01:35.000 ) This is Command #29 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6573 Simulated Maneuver End Time (UTC): 2010-171T18:04:25.750 Turn Magnitude for 7OFFSET (milliradians): 87.3512 Adding/Replacing Vector TITAN_LAT_VIEW_155 to the IVT at UTC Time: 2010-171T18:08:43.000 Adding/Replacing Vector TITAN_FOV_LIMB_155 to the IVT at UTC Time: 2010-171T18:08:58.000 PROCESSING Starting on OFFSET Command at 8182.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T18:09:15.000 ) This is Command #30 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2803 Simulated Maneuver End Time (UTC): 2010-171T18:09:48.370 Turn Magnitude for 7OFFSET (milliradians): 2.5057 PROCESSING Starting on PROFILE Command at 8474.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T18:14:07.000 ) This is Command #31 from the Event List TARGET / Command #32: Primary Inertial Vector: TITAN_LAT_VIEW_155 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #32: Secondary Inertial Vector: TITAN_FOV_LIMB_155 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 8475.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T18:14:08.000 ) This is Command #32 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_155; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_155; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 8482.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T18:14:15.000 ) This is Command #33 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6575 Simulated Maneuver End Time (UTC): 2010-171T18:17:05.750 Turn Magnitude for 7OFFSET (milliradians): 87.3528 Adding/Replacing Vector TITAN_LAT_VIEW_156 to the IVT at UTC Time: 2010-171T18:21:23.000 Adding/Replacing Vector TITAN_FOV_LIMB_156 to the IVT at UTC Time: 2010-171T18:21:38.000 PROCESSING Starting on OFFSET Command at 8942.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T18:21:55.000 ) This is Command #34 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2802 Simulated Maneuver End Time (UTC): 2010-171T18:22:28.370 Turn Magnitude for 7OFFSET (milliradians): 2.5029 PROCESSING Starting on PROFILE Command at 9234.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T18:26:47.000 ) This is Command #35 from the Event List TARGET / Command #36: Primary Inertial Vector: TITAN_LAT_VIEW_156 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #36: Secondary Inertial Vector: TITAN_FOV_LIMB_156 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 9235.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T18:26:48.000 ) This is Command #36 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_156; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_156; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 9242.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T18:26:55.000 ) This is Command #37 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6586 Simulated Maneuver End Time (UTC): 2010-171T18:29:45.750 Turn Magnitude for 7OFFSET (milliradians): 87.3553 Adding/Replacing Vector TITAN_LAT_VIEW_157 to the IVT at UTC Time: 2010-171T18:34:03.000 Adding/Replacing Vector TITAN_FOV_LIMB_157 to the IVT at UTC Time: 2010-171T18:34:18.000 PROCESSING Starting on OFFSET Command at 9702.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T18:34:35.000 ) This is Command #38 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2802 Simulated Maneuver End Time (UTC): 2010-171T18:35:08.370 Turn Magnitude for 7OFFSET (milliradians): 2.5000 PROCESSING Starting on PROFILE Command at 9994.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T18:39:27.000 ) This is Command #39 from the Event List TARGET / Command #40: Primary Inertial Vector: TITAN_LAT_VIEW_157 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #40: Secondary Inertial Vector: TITAN_FOV_LIMB_157 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 9995.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T18:39:28.000 ) This is Command #40 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_157; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_157; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 10002.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T18:39:35.000 ) This is Command #41 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6605 Simulated Maneuver End Time (UTC): 2010-171T18:42:25.750 Turn Magnitude for 7OFFSET (milliradians): 87.3589 Adding/Replacing Vector TITAN_LAT_VIEW_158 to the IVT at UTC Time: 2010-171T18:46:43.000 Adding/Replacing Vector TITAN_FOV_LIMB_158 to the IVT at UTC Time: 2010-171T18:46:58.000 PROCESSING Starting on OFFSET Command at 10462.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T18:47:15.000 ) This is Command #42 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2801 Simulated Maneuver End Time (UTC): 2010-171T18:47:48.370 Turn Magnitude for 7OFFSET (milliradians): 2.4970 PROCESSING Starting on PROFILE Command at 10754.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T18:52:07.000 ) This is Command #43 from the Event List TARGET / Command #44: Primary Inertial Vector: TITAN_LAT_VIEW_158 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #44: Secondary Inertial Vector: TITAN_FOV_LIMB_158 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 10755.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T18:52:08.000 ) This is Command #44 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_158; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_158; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 10762.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T18:52:15.000 ) This is Command #45 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6640 Simulated Maneuver End Time (UTC): 2010-171T18:55:05.750 Turn Magnitude for 7OFFSET (milliradians): 87.3642 Adding/Replacing Vector TITAN_LAT_VIEW_159 to the IVT at UTC Time: 2010-171T18:59:23.000 Adding/Replacing Vector TITAN_FOV_LIMB_159 to the IVT at UTC Time: 2010-171T18:59:38.000 PROCESSING Starting on OFFSET Command at 11222.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T18:59:55.000 ) This is Command #46 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2800 Simulated Maneuver End Time (UTC): 2010-171T19:00:28.370 Turn Magnitude for 7OFFSET (milliradians): 2.4939 PROCESSING Starting on PROFILE Command at 11514.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T19:04:47.000 ) This is Command #47 from the Event List TARGET / Command #48: Primary Inertial Vector: TITAN_LAT_VIEW_159 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #48: Secondary Inertial Vector: TITAN_FOV_LIMB_159 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 11515.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T19:04:48.000 ) This is Command #48 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_159; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_159; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 11522.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T19:04:55.000 ) This is Command #49 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6697 Simulated Maneuver End Time (UTC): 2010-171T19:07:45.750 Turn Magnitude for 7OFFSET (milliradians): 87.3720 Adding/Replacing Vector TITAN_LAT_VIEW_160 to the IVT at UTC Time: 2010-171T19:12:03.000 Adding/Replacing Vector TITAN_FOV_LIMB_160 to the IVT at UTC Time: 2010-171T19:12:18.000 PROCESSING Starting on OFFSET Command at 11982.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T19:12:35.000 ) This is Command #50 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2799 Simulated Maneuver End Time (UTC): 2010-171T19:13:08.370 Turn Magnitude for 7OFFSET (milliradians): 2.4908 PROCESSING Starting on PROFILE Command at 12274.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T19:17:27.000 ) This is Command #51 from the Event List TARGET / Command #52: Primary Inertial Vector: TITAN_LAT_VIEW_160 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #52: Secondary Inertial Vector: TITAN_FOV_LIMB_160 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 12275.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T19:17:28.000 ) This is Command #52 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_160; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_160; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 12282.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T19:17:35.000 ) This is Command #53 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6792 Simulated Maneuver End Time (UTC): 2010-171T19:20:25.750 Turn Magnitude for 7OFFSET (milliradians): 87.3841 Adding/Replacing Vector TITAN_LAT_VIEW_161 to the IVT at UTC Time: 2010-171T19:24:43.000 Adding/Replacing Vector TITAN_FOV_LIMB_161 to the IVT at UTC Time: 2010-171T19:24:58.000 PROCESSING Starting on OFFSET Command at 12742.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T19:25:15.000 ) This is Command #54 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2798 Simulated Maneuver End Time (UTC): 2010-171T19:25:48.370 Turn Magnitude for 7OFFSET (milliradians): 2.4877 PROCESSING Starting on PROFILE Command at 13034.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T19:30:07.000 ) This is Command #55 from the Event List TARGET / Command #56: Primary Inertial Vector: TITAN_LAT_VIEW_161 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #56: Secondary Inertial Vector: TITAN_FOV_LIMB_161 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 13035.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T19:30:08.000 ) This is Command #56 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_161; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_161; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 13042.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T19:30:15.000 ) This is Command #57 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6966 Simulated Maneuver End Time (UTC): 2010-171T19:33:05.750 Turn Magnitude for 7OFFSET (milliradians): 87.4046 Adding/Replacing Vector TITAN_LAT_VIEW_162 to the IVT at UTC Time: 2010-171T19:37:23.000 Adding/Replacing Vector TITAN_FOV_LIMB_162 to the IVT at UTC Time: 2010-171T19:37:38.000 PROCESSING Starting on OFFSET Command at 13502.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T19:37:55.000 ) This is Command #58 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2798 Simulated Maneuver End Time (UTC): 2010-171T19:38:28.370 Turn Magnitude for 7OFFSET (milliradians): 2.4845 PROCESSING Starting on PROFILE Command at 13794.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T19:42:47.000 ) This is Command #59 from the Event List TARGET / Command #60: Primary Inertial Vector: TITAN_LAT_VIEW_162 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #60: Secondary Inertial Vector: TITAN_FOV_LIMB_162 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 13795.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T19:42:48.000 ) This is Command #60 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_162; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_162; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 13802.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T19:42:55.000 ) This is Command #61 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.7321 Simulated Maneuver End Time (UTC): 2010-171T19:45:45.750 Turn Magnitude for 7OFFSET (milliradians): 87.4445 Adding/Replacing Vector TITAN_LAT_VIEW_163 to the IVT at UTC Time: 2010-171T19:50:03.000 Adding/Replacing Vector TITAN_FOV_LIMB_163 to the IVT at UTC Time: 2010-171T19:50:18.000 PROCESSING Starting on OFFSET Command at 14262.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T19:50:35.000 ) This is Command #62 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2797 Simulated Maneuver End Time (UTC): 2010-171T19:51:08.370 Turn Magnitude for 7OFFSET (milliradians): 2.4814 PROCESSING Starting on PROFILE Command at 14554.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T19:55:27.000 ) This is Command #63 from the Event List TARGET / Command #64: Primary Inertial Vector: TITAN_LAT_VIEW_163 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #64: Secondary Inertial Vector: TITAN_FOV_LIMB_163 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 14555.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T19:55:28.000 ) This is Command #64 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_163; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_163; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 14562.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T19:55:35.000 ) This is Command #65 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.8228 Simulated Maneuver End Time (UTC): 2010-171T19:58:25.870 Turn Magnitude for 7OFFSET (milliradians): 87.5429 Adding/Replacing Vector TITAN_LAT_VIEW_164 to the IVT at UTC Time: 2010-171T20:02:43.000 Adding/Replacing Vector TITAN_FOV_LIMB_164 to the IVT at UTC Time: 2010-171T20:02:58.000 PROCESSING Starting on OFFSET Command at 15022.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T20:03:15.000 ) This is Command #66 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2796 Simulated Maneuver End Time (UTC): 2010-171T20:03:48.370 Turn Magnitude for 7OFFSET (milliradians): 2.4784 PROCESSING Starting on PROFILE Command at 15314.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T20:08:07.000 ) This is Command #67 from the Event List TARGET / Command #68: Primary Inertial Vector: TITAN_LAT_VIEW_164 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #68: Secondary Inertial Vector: TITAN_FOV_LIMB_164 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 15315.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T20:08:08.000 ) This is Command #68 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_164; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_164; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 15322.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T20:08:15.000 ) This is Command #69 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 171.1982 Simulated Maneuver End Time (UTC): 2010-171T20:11:06.250 Turn Magnitude for 7OFFSET (milliradians): 87.9401 PROCESSING Starting on OFFSET Command at 15782.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T20:15:55.000 ) This is Command #70 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2795 Simulated Maneuver End Time (UTC): 2010-171T20:16:28.370 Turn Magnitude for 7OFFSET (milliradians): 2.4756 Adding/Replacing Vector TITAN to the IVT at UTC Time: 2010-171T20:16:38.000 PROCESSING Starting on PROFILE Command at 16114.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T20:21:27.000 ) This is Command #71 from the Event List PROCESSING Starting on TARGET Command at 16115.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T20:21:28.000 ) This is Command #72 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 16122.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T20:21:35.000 ) This is Command #73 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 335.2754 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2010-171T20:22:53.000 PROCESSING Starting on 89EXE_CMD_SEQ Command at 16430.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-171T20:26:43.000 ) This is Command #74 from the Event List Simulated Maneuver End Time (UTC): 2010-171T20:27:10.370 Turn Magnitude for 7OFFSET (milliradians): 336.8719 EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_9/kpt_eo.plt -----------------------------------