============ KPT ================= TIME: Fri Feb 27 13:03:34 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/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: /cas/ancillary/ops/NAIF/sclk/cas00130.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_5/input.bvh Successfully Read IVT File: pdt_Run_5/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_5/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: /cas/ancillary/ops/NAIF/sclk/cas00130.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_5/input.bvh Successfully Read IVT File: pdt_Run_5/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_5/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_151 WILL be propagated by a Chebyshev Polynomial from the IVT. (INITIAL CONDITIONS) NOTE: Secondary Inertial Vector TITAN_FOV_LIMB_151 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_151 to the IVT at UTC Time: 2009-205T16:23:34.000 Adding/Replacing Vector TITAN_FOV_LIMB_151 to the IVT at UTC Time: 2009-205T16:23:49.000 Adding/Replacing Vector TITAN_LAT_VIEW_152 to the IVT at UTC Time: 2009-205T16:48:34.000 Adding/Replacing Vector TITAN_FOV_LIMB_152 to the IVT at UTC Time: 2009-205T16:48:49.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-205T16:53:58.000 ) This is Command #1 from the Event List TARGET / Command #2: Primary Inertial Vector: TITAN_LAT_VIEW_152 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #2: 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 2085.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-205T16:53:59.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_152; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_152; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2092.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-205T16:54:06.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 0.4839 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-205T16:54:04.000 ) This is Command #4 from the Event List Simulated Maneuver End Time (UTC): 2009-205T16:54:06.500 Turn Magnitude for 7OFFSET (milliradians): 0.0056 Adding/Replacing Vector TITAN_LAT_VIEW_153 to the IVT at UTC Time: 2009-205T17:01:04.000 Adding/Replacing Vector TITAN_FOV_LIMB_153 to the IVT at UTC Time: 2009-205T17:01:09.000 PROCESSING Starting on PROFILE Command at 2824.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-205T17:06:18.000 ) This is Command #5 from the Event List TARGET / Command #6: Primary Inertial Vector: TITAN_LAT_VIEW_153 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #6: 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 2825.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-205T17:06:19.000 ) This is Command #6 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_153; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_153; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2832.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-205T17:06:26.000 ) This is Command #7 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 11.4733 Simulated Maneuver End Time (UTC): 2009-205T17:06:37.500 Turn Magnitude for 7OFFSET (milliradians): 3.2621 Adding/Replacing Vector TITAN_LAT_VIEW_154 to the IVT at UTC Time: 2009-205T17:13:14.000 Adding/Replacing Vector TITAN_FOV_LIMB_154 to the IVT at UTC Time: 2009-205T17:13:19.000 PROCESSING Starting on PROFILE Command at 3554.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-205T17:18:28.000 ) This is Command #8 from the Event List TARGET / Command #9: Primary Inertial Vector: TITAN_LAT_VIEW_154 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #9: 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 3555.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-205T17:18:29.000 ) This is Command #9 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_154; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_154; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 3562.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-205T17:18:36.000 ) This is Command #10 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 10.7907 Simulated Maneuver End Time (UTC): 2009-205T17:18:46.870 Turn Magnitude for 7OFFSET (milliradians): 2.7802 Adding/Replacing Vector TITAN_LAT_VIEW_155 to the IVT at UTC Time: 2009-205T17:25:34.000 Adding/Replacing Vector TITAN_FOV_LIMB_155 to the IVT at UTC Time: 2009-205T17:25:39.000 PROCESSING Starting on PROFILE Command at 4294.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-205T17:30:48.000 ) This is Command #11 from the Event List TARGET / Command #12: Primary Inertial Vector: TITAN_LAT_VIEW_155 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #12: 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 4295.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-205T17:30:49.000 ) This is Command #12 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_155; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_155; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 4302.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-205T17:30:56.000 ) This is Command #13 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 10.6035 Simulated Maneuver End Time (UTC): 2009-205T17:31:06.620 Turn Magnitude for 7OFFSET (milliradians): 2.5695 Adding/Replacing Vector TITAN to the IVT at UTC Time: 2009-205T17:38:09.000 PROCESSING Starting on PROFILE Command at 5024.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-205T17:42:58.000 ) This is Command #14 from the Event List PROCESSING Starting on TARGET Command at 5025.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-205T17:42:59.000 ) This is Command #15 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 5032.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-205T17:43:06.000 ) This is Command #16 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 318.4670 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2009-205T17:44:14.000 PROCESSING Starting on 89EXE_CMD_SEQ Command at 5330.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-205T17:48:04.000 ) This is Command #17 from the Event List Simulated Maneuver End Time (UTC): 2009-205T17:48:24.500 Turn Magnitude for 7OFFSET (milliradians): 1185.3232 EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_5/kpt_eo.plt -----------------------------------