============ KPT ================= TIME: Thu Aug 15 15:16:40 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/130412AP_RE_90165_18018.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/130528BP_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/cas00157.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/130412AP_RE_90165_18018.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/130528BP_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/cas00157.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 ************************************************************ 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_190 to the IVT at UTC Time: 2014-001T21:59:46.000 Adding/Replacing Vector SKY_RA_DEC_191 to the IVT at UTC Time: 2014-001T21:59:47.000 Adding/Replacing Vector TITAN_LAT_VIEW_176 to the IVT at UTC Time: 2014-001T22:24:11.000 Adding/Replacing Vector TITAN_FOV_LIMB_176 to the IVT at UTC Time: 2014-001T22:24:26.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-001T22:29:35.000 ) This is Command #1 from the Event List TARGET / Command #2: Primary Inertial Vector: TITAN_LAT_VIEW_176 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #2: Secondary Inertial Vector: TITAN_FOV_LIMB_176 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): 2014-001T22:29:36.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_176; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_176; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2092.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-001T22:29:43.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 82.0824 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-001T22:29:41.000 ) This is Command #4 from the Event List Simulated Maneuver End Time (UTC): 2014-001T22:31:05.250 Turn Magnitude for 7OFFSET (milliradians): 13.2675 PROCESSING Starting on PROFILE Command at 2212.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-001T22:31:43.000 ) This is Command #5 from the Event List PROCESSING Starting on DELTA_BASE Command at 2216.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-001T22:31:47.000 ) This is Command #6 from the Event List QUANTIZED ANGLES: 32.980 0.000 0.000 mrad Profiled Maneuver time (seconds): 2358.6550 Adding/Replacing Vector TITAN_LAT_VIEW_175 to the IVT at UTC Time: 2014-001T23:06:51.000 Adding/Replacing Vector TITAN_FOV_LIMB_175 to the IVT at UTC Time: 2014-001T23:06:56.000 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2014-001T23:09:51.000 Simulated Maneuver End Time (UTC): 2014-001T23:11:05.870 Turn Magnitude for 7DELTA_BASE (milliradians): 205.0974 PROCESSING Starting on PROFILE Command at 4634.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-001T23:12:05.000 ) This is Command #7 from the Event List TARGET / Command #8: Primary Inertial Vector: TITAN_LAT_VIEW_175 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #8: Secondary Inertial Vector: TITAN_FOV_LIMB_175 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 4635.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-001T23:12:06.000 ) This is Command #8 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_175; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_175; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 4642.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-001T23:12:13.000 ) This is Command #9 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 100.2952 PROCESSING Starting on 89EXE_CMD_SEQ Command at 4730.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2014-001T23:13:41.000 ) This is Command #10 from the Event List Simulated Maneuver End Time (UTC): 2014-001T23:13:53.500 Turn Magnitude for 7OFFSET (milliradians): 25.3261 EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_2/kpt_eo.plt -----------------------------------