============ KPT ================= TIME: Thu Aug 11 12:39:50 2011 USER: Todd Ansty ================================== Insert Spice File: /cas/ancillary/ops/NAIF/sp/091005AP_SE_09248_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/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_21Jan2011_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00148.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_4/input.bvh Successfully Read IVT File: pdt_Run_4/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_4/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/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/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_21Jan2011_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00148.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_4/input.bvh Successfully Read IVT File: pdt_Run_4/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_4/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: 2011-347T17:26:28.000 Adding/Replacing Vector TITAN_N_POLE_DIR to the IVT at UTC Time: 2011-347T17:26:29.000 Adding/Replacing Vector TITAN_LAT_VIEW_194 to the IVT at UTC Time: 2011-347T17:51:04.000 Adding/Replacing Vector TITAN_FOV_LIMB_194 to the IVT at UTC Time: 2011-347T17:51:09.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-347T17:56:18.000 ) This is Command #1 from the Event List TARGET / Command #2: Primary Inertial Vector: TITAN_LAT_VIEW_194 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #2: Secondary Inertial Vector: TITAN_FOV_LIMB_194 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): 2011-347T17:56:19.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_194; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_194; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2092.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-347T17:56:26.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 646.5391 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-347T17:56:24.000 ) This is Command #4 from the Event List Simulated Maneuver End Time (UTC): 2011-347T18:07:12.750 Turn Magnitude for 7OFFSET (milliradians): 1004.3119 Adding/Replacing Vector TITAN_FOV_LIMB_195 to the IVT at UTC Time: 2011-347T18:13:21.000 Adding/Replacing Vector TITAN_LAT_VIEW_195 to the IVT at UTC Time: 2011-347T18:13:23.000 PROCESSING Starting on PROFILE Command at 3419.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-347T18:18:33.000 ) This is Command #5 from the Event List TARGET / Command #6: Primary Inertial Vector: TITAN_LAT_VIEW_195 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #6: Secondary Inertial Vector: TITAN_FOV_LIMB_195 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 3420.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-347T18:18:34.000 ) This is Command #6 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_195; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_195; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 3427.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-347T18:18:41.000 ) This is Command #7 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 34.1973 Simulated Maneuver End Time (UTC): 2011-347T18:19:15.370 Turn Magnitude for 7OFFSET (milliradians): 3.5849 Adding/Replacing Vector TITAN_FOV_LIMB_196 to the IVT at UTC Time: 2011-347T18:25:21.000 Adding/Replacing Vector TITAN_LAT_VIEW_196 to the IVT at UTC Time: 2011-347T18:25:23.000 PROCESSING Starting on PROFILE Command at 4139.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-347T18:30:33.000 ) This is Command #8 from the Event List TARGET / Command #9: Primary Inertial Vector: TITAN_LAT_VIEW_196 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #9: Secondary Inertial Vector: TITAN_FOV_LIMB_196 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 4140.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-347T18:30:34.000 ) This is Command #9 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_196; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_196; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 4147.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-347T18:30:41.000 ) This is Command #10 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 36.0619 Simulated Maneuver End Time (UTC): 2011-347T18:31:17.250 Turn Magnitude for 7OFFSET (milliradians): 1.9826 Adding/Replacing Vector TITAN_FOV_LIMB_197 to the IVT at UTC Time: 2011-347T18:37:21.000 Adding/Replacing Vector TITAN_LAT_VIEW_197 to the IVT at UTC Time: 2011-347T18:37:23.000 PROCESSING Starting on PROFILE Command at 4859.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-347T18:42:33.000 ) This is Command #11 from the Event List TARGET / Command #12: Primary Inertial Vector: TITAN_LAT_VIEW_197 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #12: Secondary Inertial Vector: TITAN_FOV_LIMB_197 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 4860.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-347T18:42:34.000 ) This is Command #12 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_197; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_197; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 4867.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-347T18:42:41.000 ) This is Command #13 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 38.4129 Simulated Maneuver End Time (UTC): 2011-347T18:43:19.620 Turn Magnitude for 7OFFSET (milliradians): 5.0417 Adding/Replacing Vector TITAN_LAT_VIEW_198 to the IVT at UTC Time: 2011-347T18:49:14.000 Adding/Replacing Vector TITAN_FOV_LIMB_198 to the IVT at UTC Time: 2011-347T18:49:19.000 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2011-347T18:51:34.000 PROCESSING Starting on PROFILE Command at 5574.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-347T18:54:28.000 ) This is Command #14 from the Event List TARGET / Command #15: Primary Inertial Vector: TITAN_LAT_VIEW_198 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #15: Secondary Inertial Vector: TITAN_FOV_LIMB_198 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 5575.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-347T18:54:29.000 ) This is Command #15 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_198; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_198; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 5582.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-347T18:54:36.000 ) This is Command #16 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 76.6322 PROCESSING Starting on 89EXE_CMD_SEQ Command at 5630.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2011-347T18:55:24.000 ) This is Command #17 from the Event List Simulated Maneuver End Time (UTC): 2011-347T18:55:52.870 Turn Magnitude for 7OFFSET (milliradians): 9.7348 EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_4/kpt_eo.plt -----------------------------------