============ KPT ================= TIME: Wed Oct 22 15:40:47 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: /cas/ancillary/ops/NAIF/sclk/cas00122.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_1/input.bvh Successfully Read IVT File: pdt_Run_1/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_1/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/cas00122.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_1/input.bvh Successfully Read IVT File: pdt_Run_1/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_1/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 ------------------------------ **ERROR: Event #10 at 2009-109T23:20:15.000 Preceeds or occurs simultaneously with Event #9. The Sequence design should be revised to separate these Two Times . ** ************************************************************ 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 SKY_RA_DEC_132 to the IVT at UTC Time: 2009-109T22:15:50.000 Adding/Replacing Vector TITAN_LAT_VIEW_113 to the IVT at UTC Time: 2009-109T22:40:25.000 Adding/Replacing Vector SKY_RA_DEC_133 to the IVT at UTC Time: 2009-109T22:40:50.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-109T22:45:39.000 ) This is Command #1 from the Event List TARGET / Command #2: Primary Inertial Vector: TITAN_LAT_VIEW_113 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): 2009-109T22:45:40.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_113; SECONDARY BODY: POS_X; SECONDARY INERTIAL: SKY_RA_DEC_133; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2092.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-109T22:45:47.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 929.9282 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-109T22:45:45.000 ) This is Command #4 from the Event List Simulated Maneuver End Time (UTC): 2009-109T23:01:17.000 Turn Magnitude for 7OFFSET (milliradians): 1218.1102 PROCESSING Starting on PROFILE Command at 3061.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-109T23:01:56.000 ) This is Command #5 from the Event List PROCESSING Starting on DELTA_BASE Command at 3065.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-109T23:02:00.000 ) This is Command #6 from the Event List QUANTIZED ANGLES: 0.000 0.000 50.046 mrad Profiled Maneuver time (seconds): 1092.6053 Adding/Replacing Vector TITAN_LAT_VIEW_135 to the IVT at UTC Time: 2009-109T23:14:45.000 Adding/Replacing Vector SKY_RA_DEC_134 to the IVT at UTC Time: 2009-109T23:15:20.000 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2009-109T23:18:05.000 PROCESSING Starting on PROFILE Command at 4154.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-109T23:20:09.000 ) This is Command #7 from the Event List TARGET / Command #8: Primary Inertial Vector: TITAN_LAT_VIEW_135 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 4155.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-109T23:20:10.000 ) This is Command #8 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_135; SECONDARY BODY: POS_X; SECONDARY INERTIAL: SKY_RA_DEC_134; Light Time Correction: NO_COR Simulated Maneuver End Time (UTC): 2009-109T23:20:12.620 Turn Magnitude for 7DELTA_BASE (milliradians): 93.8415 PROCESSING Starting on PROFILE Command at 4160.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-109T23:20:15.000 ) This is Command #9 from the Event List PROCESSING Starting on OFFSET Command at 4162.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-109T23:20:17.000 ) This is Command #10 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 127.0922 PROCESSING Starting on 89EXE_CMD_SEQ Command at 4260.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-109T23:21:55.000 ) This is Command #11 from the Event List Simulated Maneuver End Time (UTC): 2009-109T23:22:24.120 Turn Magnitude for 7OFFSET (milliradians): 53.8114 EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_1/kpt_eo.plt -----------------------------------