============ KPT ================= TIME: Fri Aug 26 13:58:02 2011 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/cas00148.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_13/input.bvh Successfully Read IVT File: pdt_Run_13/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_13/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/cas00148.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_13/input.bvh Successfully Read IVT File: pdt_Run_13/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_13/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_192 to the IVT at UTC Time: 2012-050T08:13:22.000 Adding/Replacing Vector TITAN_LAT_VIEW_186 to the IVT at UTC Time: 2012-050T08:37:47.000 Adding/Replacing Vector TITAN_FOV_LIMB_186 to the IVT at UTC Time: 2012-050T08:38:02.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-050T08:43:11.000 ) This is Command #1 from the Event List TARGET / Command #2: Primary Inertial Vector: TITAN_LAT_VIEW_186 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #2: 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 2085.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-050T08:43:12.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_186; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_186; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2092.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-050T08:43:19.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 638.8934 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-050T08:43:17.000 ) This is Command #4 from the Event List Adding/Replacing Vector TITAN_FOV_LIMB_186 to the IVT at UTC Time: 2012-050T08:43:42.000 Simulated Maneuver End Time (UTC): 2012-050T08:53:58.120 Turn Magnitude for 7OFFSET (milliradians): 788.0522 PROCESSING Starting on PROFILE Command at 2772.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-050T08:54:39.000 ) This is Command #5 from the Event List PROCESSING Starting on DELTA_BASE Command at 2776.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-050T08:54:43.000 ) This is Command #6 from the Event List QUANTIZED ANGLES: 27.995 0.000 0.000 mrad Profiled Maneuver time (seconds): 744.3380 Adding/Replacing Vector TITAN_LAT_VIEW_186 to the IVT at UTC Time: 2012-050T08:57:27.000 Adding/Replacing Vector TITAN_LAT_VIEW_188 to the IVT at UTC Time: 2012-050T09:01:53.000 Adding/Replacing Vector TITAN_FOV_LIMB_188 to the IVT at UTC Time: 2012-050T09:02:08.000 Simulated Maneuver End Time (UTC): 2012-050T09:07:07.500 Turn Magnitude for 7DELTA_BASE (milliradians): 364.0151 PROCESSING Starting on PROFILE Command at 3530.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-050T09:07:17.000 ) This is Command #7 from the Event List TARGET / Command #8: Primary Inertial Vector: TITAN_LAT_VIEW_188 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #8: Secondary Inertial Vector: TITAN_FOV_LIMB_188 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 3531.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-050T09:07:18.000 ) This is Command #8 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_188; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_188; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 3538.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-050T09:07:25.000 ) This is Command #9 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 201.6608 Simulated Maneuver End Time (UTC): 2012-050T09:10:46.870 Turn Magnitude for 7OFFSET (milliradians): 133.1159 PROCESSING Starting on PROFILE Command at 3778.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-050T09:11:25.000 ) This is Command #10 from the Event List PROCESSING Starting on DELTA_BASE Command at 3782.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-050T09:11:29.000 ) This is Command #11 from the Event List QUANTIZED ANGLES: 27.995 0.000 0.000 mrad Profiled Maneuver time (seconds): 744.4128 Adding/Replacing Vector TITAN_LAT_VIEW_187 to the IVT at UTC Time: 2012-050T09:18:47.000 Adding/Replacing Vector TITAN_FOV_LIMB_187 to the IVT at UTC Time: 2012-050T09:19:02.000 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2012-050T09:23:27.000 Simulated Maneuver End Time (UTC): 2012-050T09:23:53.620 Turn Magnitude for 7DELTA_BASE (milliradians): 149.0874 PROCESSING Starting on PROFILE Command at 4544.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-050T09:24:11.000 ) This is Command #12 from the Event List TARGET / Command #13: Primary Inertial Vector: TITAN_LAT_VIEW_187 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #13: Secondary Inertial Vector: TITAN_FOV_LIMB_187 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 4545.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-050T09:24:12.000 ) This is Command #13 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_187; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_187; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 4552.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-050T09:24:19.000 ) This is Command #14 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 195.0719 PROCESSING Starting on 89EXE_CMD_SEQ Command at 4730.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2012-050T09:27:17.000 ) This is Command #15 from the Event List Simulated Maneuver End Time (UTC): 2012-050T09:27:34.250 Turn Magnitude for 7OFFSET (milliradians): 100.3464 EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_13/kpt_eo.plt -----------------------------------