============ KPT ================= TIME: Fri Aug 14 11:25:58 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/PDT13.3d/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/PDT13.3d/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: V13.1 ------------------------------ SID Suspend Values Theta_1: 0.20 degrees Theta_2: 0.50 degrees Theta_3: 1.50 degrees T_1: 60.00 seconds T_2: 240.00 seconds T_3: 1800.00 seconds T_4: 2400.00 seconds **** WARNING: INITIAL PRIMARY INERTIAL Vector TITAN is present in the Initial IVT, but the Vector Entry has a time interval which does NOT contain the Current Time of interest. THIS CONDITION REQUIRES FIXING IF THIS IS A REAL SEQUENCE. ************************************************************ NOTE: MANEUVER COMMANDS Cause Turning of the Spacecraft 1.125 -> 2.000 seconds following the Command Time - the times shown in this Run Log are times that the Spacecraft Actually Starts Turning. ************************************************************ ************************************************************ NOTE: CONSTRAINT MONITOR IS SELECTED FOR THIS RUN Initial CMT Dynamic Constraints: RCS Max Rates(rad/s): 1.43000000e-02 1.43000000e-02 1.43000000e-02 RCS Max Accel(rad/s/s): 1.52700000e-04 1.24200000e-04 3.24700000e-04 RWA Max Rates(rad/s): 2.46800000e-03 2.96200000e-03 4.88600000e-03 RWA Max Accel(rad/s/s): 1.35300000e-05 1.62300000e-05 2.67800000e-05 ************************************************************ ************************************************************ * * * NOTE: ALL ERRORS, REJECTED COMMANDS, WARNINGS, * * CMT VIOLATIONS, etc, MUST BE FIXED PRIOR * * TO FINAL SEQUENCE GENERATION and UPLINK * ************************************************************ Adding/Replacing Vector TITAN to the IVT at UTC Time: 2010-028T19:28:54.000 Adding/Replacing Vector TITAN_LAT_VIEW_130 to the IVT at UTC Time: 2010-028T19:53:19.000 Adding/Replacing Vector TITAN_FOV_LIMB_130 to the IVT at UTC Time: 2010-028T19:53:34.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-028T19:58:43.000 ) 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): 2010-028T19:58:44.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_130; SECONDARY BODY: POS_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): 2010-028T19:58:51.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 658.6930 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-028T19:58:49.000 ) This is Command #4 from the Event List Simulated Maneuver End Time (UTC): 2010-028T20:09:49.870 Turn Magnitude for 7OFFSET (milliradians): 1066.4307 Adding/Replacing Vector TITAN_LAT_VIEW_131 to the IVT at UTC Time: 2010-028T20:17:19.000 Adding/Replacing Vector TITAN_FOV_LIMB_131 to the IVT at UTC Time: 2010-028T20:17:24.000 PROCESSING Starting on PROFILE Command at 3514.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-028T20:22:33.000 ) This is Command #5 from the Event List TARGET / Command #6: Primary Inertial Vector: TITAN_LAT_VIEW_131 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #6: 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 3515.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-028T20:22:34.000 ) This is Command #6 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_131; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_131; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 3522.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-028T20:22:41.000 ) This is Command #7 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 32.0556 Simulated Maneuver End Time (UTC): 2010-028T20:23:13.250 Turn Magnitude for 7OFFSET (milliradians): 3.5137 Adding/Replacing Vector TITAN_LAT_VIEW_132 to the IVT at UTC Time: 2010-028T20:30:19.000 Adding/Replacing Vector TITAN_FOV_LIMB_132 to the IVT at UTC Time: 2010-028T20:30:24.000 PROCESSING Starting on PROFILE Command at 4294.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-028T20:35:33.000 ) This is Command #8 from the Event List TARGET / Command #9: Primary Inertial Vector: TITAN_LAT_VIEW_132 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #9: 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 4295.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-028T20:35:34.000 ) This is Command #9 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_132; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_132; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 4302.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-028T20:35:41.000 ) This is Command #10 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.6531 Simulated Maneuver End Time (UTC): 2010-028T20:36:14.870 Turn Magnitude for 7OFFSET (milliradians): 1.1956 Adding/Replacing Vector TITAN_LAT_VIEW_133 to the IVT at UTC Time: 2010-028T20:43:09.000 Adding/Replacing Vector TITAN_FOV_LIMB_133 to the IVT at UTC Time: 2010-028T20:43:24.000 PROCESSING Starting on PROFILE Command at 5074.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-028T20:48:33.000 ) This is Command #11 from the Event List TARGET / Command #12: Primary Inertial Vector: TITAN_LAT_VIEW_133 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #12: 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 5075.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-028T20:48:34.000 ) This is Command #12 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_133; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_133; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 5082.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-028T20:48:41.000 ) This is Command #13 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 35.7357 Simulated Maneuver End Time (UTC): 2010-028T20:49:16.870 Turn Magnitude for 7OFFSET (milliradians): 4.9619 Adding/Replacing Vector TITAN_LAT_VIEW_134 to the IVT at UTC Time: 2010-028T20:56:59.000 Adding/Replacing Vector TITAN_FOV_LIMB_134 to the IVT at UTC Time: 2010-028T20:57:04.000 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2010-028T21:01:59.000 PROCESSING Starting on PROFILE Command at 5894.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-028T21:02:13.000 ) This is Command #14 from the Event List TARGET / Command #15: Primary Inertial Vector: TITAN_LAT_VIEW_134 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #15: 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 5895.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-028T21:02:14.000 ) This is Command #15 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_134; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_134; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 5902.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-028T21:02:21.000 ) This is Command #16 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 247.5773 PROCESSING Starting on 89EXE_CMD_SEQ Command at 6110.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-028T21:05:49.000 ) This is Command #17 from the Event List Simulated Maneuver End Time (UTC): 2010-028T21:06:28.750 Turn Magnitude for 7OFFSET (milliradians): 177.6962 EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_2/kpt_eo.plt -----------------------------------