============ KPT ================= TIME: Thu Feb 9 16:26:54 2012 USER: Todd Ansty ================================== Insert Spice File: /cas/ancillary/ops/NAIF/sp/110818AP_SE_11175_17265.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/110317AP_RE_90165_18018.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/110120BP_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/naif0009.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/cas00150.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_5/input.bvh Successfully Read IVT File: pdt_Run_5/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_5/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/110317AP_RE_90165_18018.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/110120BP_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/naif0009.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/cas00150.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_5/input.bvh Successfully Read IVT File: pdt_Run_5/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_5/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: Primary Inertial Vector TITAN_LAT_VIEW_184 WILL be propagated by a Chebyshev Polynomial from the IVT. (INITIAL CONDITIONS) NOTE: Secondary Inertial Vector TITAN_FOV_LIMB_184 WILL be propagated by a Chebyshev Polynomial from the IVT. (INITIAL CONDITIONS) ************************************************************ 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_LAT_VIEW_184 to the IVT at UTC Time: 2012-206T18:48:38.000 Adding/Replacing Vector TITAN_FOV_LIMB_184 to the IVT at UTC Time: 2012-206T18:48:53.000 Adding/Replacing Vector TITAN_LAT_VIEW_185 to the IVT at UTC Time: 2012-206T19:13:38.000 Adding/Replacing Vector TITAN_FOV_LIMB_185 to the IVT at UTC Time: 2012-206T19:13:53.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-206T19:19:02.000 ) This is Command #1 from the Event List TARGET / Command #2: Primary Inertial Vector: TITAN_LAT_VIEW_185 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #2: Secondary Inertial Vector: TITAN_FOV_LIMB_185 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): 2012-206T19:19:03.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_185; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_185; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2092.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-206T19:19:10.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 0.3226 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-206T19:19:08.000 ) This is Command #4 from the Event List Simulated Maneuver End Time (UTC): 2012-206T19:19:10.370 Turn Magnitude for 7OFFSET (milliradians): 0.0200 PROCESSING Starting on PROFILE Command at 2112.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-206T19:19:30.000 ) This is Command #5 from the Event List PROCESSING Starting on DELTA_BASE Command at 2116.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-206T19:19:34.000 ) This is Command #6 from the Event List QUANTIZED ANGLES: -27.995 0.000 0.000 mrad Profiled Maneuver time (seconds): 806.7895 Adding/Replacing Vector TITAN_LAT_VIEW_186 to the IVT at UTC Time: 2012-206T19:27:58.000 Adding/Replacing Vector TITAN_FOV_LIMB_186 to the IVT at UTC Time: 2012-206T19:28:03.000 Simulated Maneuver End Time (UTC): 2012-206T19:33:00.870 Turn Magnitude for 7DELTA_BASE (milliradians): 52.3773 PROCESSING Starting on PROFILE Command at 2934.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-206T19:33:12.000 ) This is Command #7 from the Event List TARGET / Command #8: Primary Inertial Vector: TITAN_LAT_VIEW_186 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #8: Secondary Inertial Vector: TITAN_FOV_LIMB_186 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 2935.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-206T19:33:13.000 ) This is Command #8 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_186; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_186; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2942.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-206T19:33:20.000 ) This is Command #9 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 72.5193 Simulated Maneuver End Time (UTC): 2012-206T19:34:32.620 Turn Magnitude for 7OFFSET (milliradians): 110.8990 PROCESSING Starting on PROFILE Command at 3052.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-206T19:35:10.000 ) This is Command #10 from the Event List PROCESSING Starting on DELTA_BASE Command at 3056.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-206T19:35:14.000 ) This is Command #11 from the Event List QUANTIZED ANGLES: -27.995 0.000 0.000 mrad Profiled Maneuver time (seconds): 806.7421 Adding/Replacing Vector TITAN_SC_RAM to the IVT at UTC Time: 2012-206T19:43:50.000 Adding/Replacing Vector TITAN to the IVT at UTC Time: 2012-206T19:43:52.000 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2012-206T19:48:18.000 Simulated Maneuver End Time (UTC): 2012-206T19:48:40.750 Turn Magnitude for 7DELTA_BASE (milliradians): 168.2600 PROCESSING Starting on PROFILE Command at 3864.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-206T19:48:42.000 ) This is Command #12 from the Event List TARGET / Command #13: Secondary Inertial Vector: TITAN_SC_RAM determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 3865.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-206T19:48:43.000 ) This is Command #13 from the Event List PRIMARY BODY: NEG_Y; PRIMARY INERTIAL: TITAN; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_SC_RAM; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 3872.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-206T19:48:50.000 ) This is Command #14 from the Event List QUANTIZED ANGLES: -357.801 0.000 -279.280 mrad Profiled Maneuver time (seconds): 216.9196 PROCESSING Starting on 89EXE_CMD_SEQ Command at 4070.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-206T19:52:08.000 ) This is Command #15 from the Event List Simulated Maneuver End Time (UTC): 2012-206T19:52:27.000 Turn Magnitude for 7OFFSET (milliradians): 784.4499 EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_5/kpt_eo.plt -----------------------------------