============ KPT ================= TIME: Tue Dec 2 15:07:50 2008 USER: Todd Ansty ================================== Insert Spice File: /cas/ancillary/ops/NAIF/sp/080806AP_SE_08138_10182.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/080527AP_RE_90165_18018.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/070416BP_IRRE_00256_14363.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_25Aug2008_merged.tpc Insert SCLK SCET File: /export/home/eros/PDT/todd/PDT-run/cas00124.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_4/input.bvh Successfully Read IVT File: pdt_Run_4/input.ivt Successfully Read TLF File: /export/home/eros/PDT13.1d/Input/KPT/kpt_defaultForXM.tlf Successfully Read KPT Spice Identification File: /cas/ancillary/ops/SCO/ssid/08_238_param.ssid Successfully Read Input PEF File: pdt_Run_4/temp.pef NOTE: This File Supercedes Any Events held within the Input Configuration File. Successfully Read KPT CMT File: /cas/ancillary/ops/SCO/cmt_limits/POST_PROBE_V11.cmt Insert Spice File: /cas/ancillary/ops/NAIF/sp/080806AP_SE_08138_10182.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/080527AP_RE_90165_18018.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/070416BP_IRRE_00256_14363.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_25Aug2008_merged.tpc Insert SCLK SCET File: /export/home/eros/PDT/todd/PDT-run/cas00124.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_4/input.bvh Successfully Read IVT File: pdt_Run_4/input.ivt Successfully Read TLF File: /export/home/eros/PDT13.1d/Input/KPT/kpt_defaultForXM.tlf Successfully Read KPT Spice Identification File: /cas/ancillary/ops/SCO/ssid/08_238_param.ssid Successfully Read Input PEF File: pdt_Run_4/temp.pef NOTE: This File Supercedes Any Events held within the Input Configuration File. Successfully Read KPT CMT File: /cas/ancillary/ops/SCO/cmt_limits/POST_PROBE_V11.cmt ------------------------------ CSAS-KPT Version: V12.1 ------------------------------ NOTE: Primary Inertial Vector TITAN_LAT_VIEW_146 WILL be propagated by a Chebyshev Polynomial from the IVT. (INITIAL CONDITIONS) NOTE: Secondary Inertial Vector TITAN_FOV_LIMB_146 WILL be propagated by a Chebyshev Polynomial from the IVT. (INITIAL CONDITIONS) ************************************************************ 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_LAT_VIEW_146 to the IVT at UTC Time: 2009-125T20:08:46.000 Adding/Replacing Vector TITAN_FOV_LIMB_146 to the IVT at UTC Time: 2009-125T20:09:01.000 Adding/Replacing Vector TITAN_LAT_VIEW_141 to the IVT at UTC Time: 2009-125T20:33:46.000 Adding/Replacing Vector TITAN_FOV_LIMB_141 to the IVT at UTC Time: 2009-125T20:34:01.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-125T20:39:10.000 ) This is Command #1 from the Event List TARGET / Command #2: Primary Inertial Vector: TITAN_LAT_VIEW_141 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #2: 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 2085.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-125T20:39:11.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_141; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_141; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2092.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-125T20:39:18.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 2.5826 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-125T20:39:16.000 ) This is Command #4 from the Event List Simulated Maneuver End Time (UTC): 2009-125T20:39:20.620 Turn Magnitude for 7OFFSET (milliradians): 0.0419 Adding/Replacing Vector TITAN_LAT_VIEW_142 to the IVT at UTC Time: 2009-125T20:47:21.000 Adding/Replacing Vector TITAN_FOV_LIMB_142 to the IVT at UTC Time: 2009-125T20:47:26.000 PROCESSING Starting on PROFILE Command at 2889.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-125T20:52:35.000 ) This is Command #5 from the Event List TARGET / Command #6: Primary Inertial Vector: TITAN_LAT_VIEW_142 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #6: 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 2890.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-125T20:52:36.000 ) This is Command #6 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_142; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_142; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2897.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-125T20:52:43.000 ) This is Command #7 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 31.1701 Simulated Maneuver End Time (UTC): 2009-125T20:53:14.250 Turn Magnitude for 7OFFSET (milliradians): 2.4285 Adding/Replacing Vector TITAN_LAT_VIEW_141 to the IVT at UTC Time: 2009-125T21:00:56.000 Adding/Replacing Vector TITAN_FOV_LIMB_143 to the IVT at UTC Time: 2009-125T21:01:01.000 PROCESSING Starting on PROFILE Command at 3704.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-125T21:06:10.000 ) This is Command #8 from the Event List TARGET / Command #9: Primary Inertial Vector: TITAN_LAT_VIEW_141 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #9: 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 3705.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-125T21:06:11.000 ) This is Command #9 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_141; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_143; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 3712.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-125T21:06:18.000 ) This is Command #10 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.0302 Simulated Maneuver End Time (UTC): 2009-125T21:06:51.120 Turn Magnitude for 7OFFSET (milliradians): 2.9434 Adding/Replacing Vector TITAN_LAT_VIEW_144 to the IVT at UTC Time: 2009-125T21:14:21.000 Adding/Replacing Vector TITAN_FOV_LIMB_142 to the IVT at UTC Time: 2009-125T21:14:26.000 PROCESSING Starting on PROFILE Command at 4509.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-125T21:19:35.000 ) This is Command #11 from the Event List TARGET / Command #12: Primary Inertial Vector: TITAN_LAT_VIEW_144 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #12: 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 4510.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-125T21:19:36.000 ) This is Command #12 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_144; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_142; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 4517.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-125T21:19:43.000 ) This is Command #13 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 35.2281 Simulated Maneuver End Time (UTC): 2009-125T21:20:18.250 Turn Magnitude for 7OFFSET (milliradians): 3.1392 Adding/Replacing Vector TITAN_LAT_VIEW_146 to the IVT at UTC Time: 2009-125T21:27:46.000 Adding/Replacing Vector TITAN_FOV_LIMB_146 to the IVT at UTC Time: 2009-125T21:28:01.000 PROCESSING Starting on PROFILE Command at 5324.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-125T21:33:10.000 ) This is Command #14 from the Event List TARGET / Command #15: Primary Inertial Vector: TITAN_LAT_VIEW_146 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #15: 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 5325.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-125T21:33:11.000 ) This is Command #15 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_146; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_146; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 5332.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-125T21:33:18.000 ) This is Command #16 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 319.3576 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2009-125T21:34:26.000 PROCESSING Starting on 89EXE_CMD_SEQ Command at 5630.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-125T21:38:16.000 ) This is Command #17 from the Event List Simulated Maneuver End Time (UTC): 2009-125T21:38:37.370 Turn Magnitude for 7OFFSET (milliradians): 300.7744 EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_4/kpt_eo.plt -----------------------------------