============ KPT ================= TIME: Wed Dec 1 16:06:51 2010 USER: Todd Ansty ================================== Insert Spice File: /cas/ancillary/ops/NAIF/sp/091005AP_SE_09248_17265.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/100209AP_RE_90165_18018.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/090202BP_IRRE_00256_50017.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/091005AP_PE_09248_17265.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/091005AP_SK_09248_17265.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0009.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck02Sep2010.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_11May2009_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00146.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_12/input.bvh Successfully Read IVT File: pdt_Run_12/input.ivt Successfully Read TLF File: /export/home/eros/D14.0d_PDT-SWDepot/Input/KPT/kpt_default.tlf Successfully Read KPT Spice Identification File: /cas/ancillary/ops/SCO/ssid/09_131_param.ssid Successfully Read Input PEF File: pdt_Run_12/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/091005AP_SE_09248_17265.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/100209AP_RE_90165_18018.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/090202BP_IRRE_00256_50017.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/091005AP_PE_09248_17265.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/091005AP_SK_09248_17265.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0009.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck02Sep2010.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_11May2009_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00146.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_12/input.bvh Successfully Read IVT File: pdt_Run_12/input.ivt Successfully Read TLF File: /export/home/eros/D14.0d_PDT-SWDepot/Input/KPT/kpt_default.tlf Successfully Read KPT Spice Identification File: /cas/ancillary/ops/SCO/ssid/09_131_param.ssid Successfully Read Input PEF File: pdt_Run_12/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: V14.0 ------------------------------ SID Suspend Values Theta_1: 0.20 degrees Theta_2: 0.50 degrees Theta_3: 1.50 degrees T_1: 60.00 seconds T_2: 240.00 seconds T_3: 1800.00 seconds T_4: 2400.00 seconds ************************************************************ 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_134 to the IVT at UTC Time: 2011-174T05:12:05.000 Adding/Replacing Vector TITAN to the IVT at UTC Time: 2011-174T05:37:04.000 Adding/Replacing Vector TITAN_N_POLE_DIR to the IVT at UTC Time: 2011-174T05:37:05.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-174T05:41:54.000 ) This is Command #1 from the Event List PROCESSING Starting on TARGET Command at 2085.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-174T05:41:55.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_N_POLE_DIR; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2092.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-174T05:42:02.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 0.000 0.000 6.998 mrad Profiled Maneuver time (seconds): 1524.5431 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-174T05:42:00.000 ) This is Command #4 from the Event List Simulated Maneuver End Time (UTC): 2011-174T06:07:26.620 Turn Magnitude for 7OFFSET (milliradians): 2202.0239 PROCESSING Starting on OFFSET Command at 5632.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-174T06:41:02.000 ) This is Command #5 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 36.5092 Simulated Maneuver End Time (UTC): 2011-174T06:41:38.620 Turn Magnitude for 7OFFSET (milliradians): 6.9547 PROCESSING Starting on OFFSET Command at 74332.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-175T01:46:02.000 ) This is Command #6 from the Event List QUANTIZED ANGLES: 0.000 0.000 6.998 mrad Profiled Maneuver time (seconds): 36.5101 Simulated Maneuver End Time (UTC): 2011-175T01:46:38.620 Turn Magnitude for 7OFFSET (milliradians): 7.0472 Adding/Replacing Vector SKY_RA_DEC_135 to the IVT at UTC Time: 2011-175T02:08:05.000 PROCESSING Starting on PROFILE Command at 75944.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-175T02:12:54.000 ) This is Command #7 from the Event List PROCESSING Starting on TARGET Command at 75945.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-175T02:12:55.000 ) This is Command #8 from the Event List PRIMARY BODY: XBAND; PRIMARY INERTIAL: EARTH; SECONDARY BODY: NEG_X; SECONDARY INERTIAL: SKY_RA_DEC_135; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 75952.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-175T02:13:02.000 ) This is Command #9 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 1557.0765 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2011-175T02:37:10.000 Simulated Maneuver End Time (UTC): 2011-175T02:38:59.120 Turn Magnitude for 7OFFSET (milliradians): 2251.6217 PROCESSING Starting on 89EXE_CMD_SEQ Command at 77630.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-175T02:41:00.000 ) This is Command #10 from the Event List EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_12/kpt_eo.plt -----------------------------------