============ KPT ================= TIME: Fri Apr 5 16:12:46 2013 USER: Todd Ansty ================================== Insert Spice File: /cas/ancillary/ops/NAIF/sp/110818AP_SE_11175_17265.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/120308AP_RE_90165_18018.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/120711BP_IRRE_00256_25017.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/110818AP_PE_11175_17265.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/110818AP_SK_11175_17265.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0010.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck25Aug2011.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_21Jan2011_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00156.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/D14.2d_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_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/110818AP_SE_11175_17265.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/120308AP_RE_90165_18018.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/120711BP_IRRE_00256_25017.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/110818AP_PE_11175_17265.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/110818AP_SK_11175_17265.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0010.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck25Aug2011.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_21Jan2011_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00156.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/D14.2d_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_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: V14.1 ------------------------------ 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 **** 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: 2013-254T17:14:00.000 Adding/Replacing Vector TITAN_N_POLE_DIR to the IVT at UTC Time: 2013-254T17:14:01.000 Adding/Replacing Vector TITAN_FRAME_1 to the IVT at UTC Time: 2013-254T17:38:59.000 Adding/Replacing Vector TITAN_LAT_LON_175 to the IVT at UTC Time: 2013-254T17:39:01.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-254T17:43:50.000 ) This is Command #1 from the Event List NOTE: Primary Inertial Vector TITAN_LAT_LON_175 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): 2013-254T17:43:51.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_LON_175; SECONDARY BODY: NEG_X; 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): 2013-254T17:43:58.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 0.000 0.000 23.968 mrad Profiled Maneuver time (seconds): 70.1895 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-254T17:43:56.000 ) This is Command #4 from the Event List Simulated Maneuver End Time (UTC): 2013-254T17:45:08.250 Turn Magnitude for 7OFFSET (milliradians): 19.8158 PROCESSING Starting on OFFSET Command at 3412.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-254T18:05:58.000 ) This is Command #5 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 67.5672 Simulated Maneuver End Time (UTC): 2013-254T18:07:05.620 Turn Magnitude for 7OFFSET (milliradians): 23.9427 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2013-254T22:39:06.000 PROCESSING Starting on PROFILE Command at 19964.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-254T22:41:50.000 ) This is Command #6 from the Event List PROCESSING Starting on TARGET Command at 19965.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-254T22:41:51.000 ) 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 19972.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-254T22:41:58.000 ) This is Command #8 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 76.3337 PROCESSING Starting on 89EXE_CMD_SEQ Command at 20030.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-254T22:42:56.000 ) This is Command #9 from the Event List Simulated Maneuver End Time (UTC): 2013-254T22:43:14.370 Turn Magnitude for 7OFFSET (milliradians): 17.7420 EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_2/kpt_eo.plt -----------------------------------