============ KPT ================= TIME: Tue Jul 15 11:23:48 2008 USER: Todd Ansty ================================== Insert Spice File: /cas/ancillary/ops/NAIF/sp/080520AP_SE_08138_10182.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/070815AP_RE_90165_14363.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/070416BP_IRRE_00256_14363.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/080520AP_PE_08138_10182.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/080520AP_SK_08138_10182.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0008.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck15May2008.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_01Oct2007_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00114.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/07_274_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/080520AP_SE_08138_10182.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/070815AP_RE_90165_14363.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/070416BP_IRRE_00256_14363.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/080520AP_PE_08138_10182.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/080520AP_SK_08138_10182.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0008.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck15May2008.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_01Oct2007_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00114.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/07_274_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 ------------------------------ **** 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: 2008-355T23:29:56.000 Adding/Replacing Vector SKY_RA_DEC_139 to the IVT at UTC Time: 2008-355T23:29:57.000 Adding/Replacing Vector TITAN_FRAME_1 to the IVT at UTC Time: 2008-355T23:54:55.000 Adding/Replacing Vector TITAN_LAT_LON_133 to the IVT at UTC Time: 2008-355T23:54:57.000 Adding/Replacing Vector SKY_RA_DEC_140 to the IVT at UTC Time: 2008-355T23:54:58.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2008-355T23:59:46.000 ) This is Command #1 from the Event List NOTE: Primary Inertial Vector TITAN_LAT_LON_133 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): 2008-355T23:59:47.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_LON_133; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: SKY_RA_DEC_140; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2092.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2008-355T23:59:54.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 0.000 0.000 25.023 mrad Profiled Maneuver time (seconds): 295.4761 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2008-355T23:59:52.000 ) This is Command #4 from the Event List Simulated Maneuver End Time (UTC): 2008-356T00:04:49.620 Turn Magnitude for 7OFFSET (milliradians): 262.3916 PROCESSING Starting on OFFSET Command at 3622.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2008-356T00:25:24.000 ) This is Command #5 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 69.0382 Simulated Maneuver End Time (UTC): 2008-356T00:26:33.250 Turn Magnitude for 7OFFSET (milliradians): 24.9939 PROCESSING Starting on OFFSET Command at 15262.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2008-356T03:39:24.000 ) This is Command #6 from the Event List QUANTIZED ANGLES: 0.000 0.000 25.023 mrad Profiled Maneuver time (seconds): 69.0384 Simulated Maneuver End Time (UTC): 2008-356T03:40:33.250 Turn Magnitude for 7OFFSET (milliradians): 25.0731 PROCESSING Starting on PROFILE Command at 16154.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2008-356T03:54:16.000 ) This is Command #7 from the Event List PROCESSING Starting on TARGET Command at 16155.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2008-356T03:54:17.000 ) This is Command #8 from the Event List PRIMARY BODY: NEG_Y; PRIMARY INERTIAL: TITAN; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: SKY_RA_DEC_140; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 16162.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2008-356T03:54:24.000 ) This is Command #9 from the Event List QUANTIZED ANGLES: 0.000 -261.831 0.000 mrad Profiled Maneuver time (seconds): 295.4275 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2008-356T03:55:02.000 PROCESSING Starting on 89EXE_CMD_SEQ Command at 16430.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2008-356T03:58:52.000 ) This is Command #10 from the Event List Simulated Maneuver End Time (UTC): 2008-356T03:59:19.620 Turn Magnitude for 7OFFSET (milliradians): 262.3534 EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_4/kpt_eo.plt -----------------------------------