============ KPT ================= TIME: Mon Nov 3 14:41:30 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_2/input.bvh Successfully Read IVT File: pdt_Run_2/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_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/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_2/input.bvh Successfully Read IVT File: pdt_Run_2/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_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: V12.1 ------------------------------ **** 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: 2009-086T14:13:40.000 Adding/Replacing Vector TITAN_N_POLE_DIR to the IVT at UTC Time: 2009-086T14:13:41.000 Adding/Replacing Vector TITAN_FRAME_1 to the IVT at UTC Time: 2009-086T14:38:39.000 Adding/Replacing Vector TITAN_LAT_LON_132 to the IVT at UTC Time: 2009-086T14:38:41.000 Adding/Replacing Vector SKY_RA_DEC_138 to the IVT at UTC Time: 2009-086T14:38:42.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-086T14:43:30.000 ) This is Command #1 from the Event List NOTE: Primary Inertial Vector TITAN_LAT_LON_132 WILL be propagated by a ROTATE_VEC from the IVT. PROCESSING Starting on TARGET Command at 2085.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-086T14:43:31.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_LON_132; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: SKY_RA_DEC_138; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2092.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-086T14:43:38.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 0.000 0.000 -25.023 mrad Profiled Maneuver time (seconds): 367.1407 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-086T14:43:36.000 ) This is Command #4 from the Event List Simulated Maneuver End Time (UTC): 2009-086T14:49:45.370 Turn Magnitude for 7OFFSET (milliradians): 405.0486 PROCESSING Starting on OFFSET Command at 3992.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-086T15:15:18.000 ) This is Command #5 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 69.0383 Simulated Maneuver End Time (UTC): 2009-086T15:16:27.250 Turn Magnitude for 7OFFSET (milliradians): 25.0462 PROCESSING Starting on PROFILE Command at 12474.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-086T17:36:40.000 ) This is Command #6 from the Event List PROCESSING Starting on TARGET Command at 12475.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-086T17:36:41.000 ) This is Command #7 from the Event List PRIMARY BODY: NEG_Y; PRIMARY INERTIAL: TITAN; SECONDARY BODY: NEG_X; SECONDARY INERTIAL: TITAN_N_POLE_DIR; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 12482.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-086T17:36:48.000 ) This is Command #8 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 368.5477 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2009-086T17:38:46.000 PROCESSING Starting on 89EXE_CMD_SEQ Command at 12830.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-086T17:42:36.000 ) This is Command #9 from the Event List Simulated Maneuver End Time (UTC): 2009-086T17:42:56.750 Turn Magnitude for 7OFFSET (milliradians): 407.5604 EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_2/kpt_eo.plt -----------------------------------