============ KPT ================= TIME: Fri Aug 10 15:57:30 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/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/cas00155.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_11/input.bvh Successfully Read IVT File: pdt_Run_11/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_11/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/cas00155.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_11/input.bvh Successfully Read IVT File: pdt_Run_11/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_11/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_176 to the IVT at UTC Time: 2013-049T09:16:05.000 Adding/Replacing Vector TITAN to the IVT at UTC Time: 2013-049T09:41:04.000 Adding/Replacing Vector SKY_RA_DEC_178 to the IVT at UTC Time: 2013-049T09:41:05.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-049T09:45:54.000 ) This is Command #1 from the Event List PROCESSING Starting on TARGET Command at 2085.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-049T09:45:55.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN; SECONDARY BODY: NEG_X; SECONDARY INERTIAL: SKY_RA_DEC_178; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2092.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-049T09:46:02.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 1.342 0.000 2.972 mrad Profiled Maneuver time (seconds): 1788.7845 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-049T09:46:00.000 ) This is Command #4 from the Event List Simulated Maneuver End Time (UTC): 2013-049T10:15:51.000 Turn Magnitude for 7OFFSET (milliradians): 2534.5491 PROCESSING Starting on OFFSET Command at 4342.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-049T10:23:32.000 ) This is Command #5 from the Event List QUANTIZED ANGLES: -1.629 0.000 2.972 mrad Profiled Maneuver time (seconds): 36.3380 Simulated Maneuver End Time (UTC): 2013-049T10:24:08.500 Turn Magnitude for 7OFFSET (milliradians): 2.9746 PROCESSING Starting on OFFSET Command at 4672.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-049T10:29:02.000 ) This is Command #6 from the Event List QUANTIZED ANGLES: -1.629 0.000 -0.862 mrad Profiled Maneuver time (seconds): 27.0235 Simulated Maneuver End Time (UTC): 2013-049T10:29:29.250 Turn Magnitude for 7OFFSET (milliradians): 3.8175 PROCESSING Starting on OFFSET Command at 5002.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-049T10:34:32.000 ) This is Command #7 from the Event List QUANTIZED ANGLES: 1.342 0.000 -0.862 mrad Profiled Maneuver time (seconds): 36.3378 Adding/Replacing Vector TITAN_LAT_SSCLON_175 to the IVT at UTC Time: 2013-049T10:34:45.000 Adding/Replacing Vector SKY_RA_DEC_179 to the IVT at UTC Time: 2013-049T10:35:05.000 Simulated Maneuver End Time (UTC): 2013-049T10:35:08.500 Turn Magnitude for 7OFFSET (milliradians): 2.9675 PROCESSING Starting on PROFILE Command at 5324.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-049T10:39:54.000 ) This is Command #8 from the Event List TARGET / Command #9: Primary Inertial Vector: TITAN_LAT_SSCLON_175 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 5325.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-049T10:39:55.000 ) This is Command #9 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_SSCLON_175; SECONDARY BODY: NEG_X; SECONDARY INERTIAL: SKY_RA_DEC_179; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 5332.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-049T10:40:02.000 ) This is Command #10 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 26.1899 Simulated Maneuver End Time (UTC): 2013-049T10:40:28.370 Turn Magnitude for 7OFFSET (milliradians): 2.2392 Adding/Replacing Vector TITAN_LAT_SSCLON_176 to the IVT at UTC Time: 2013-049T16:30:15.000 Adding/Replacing Vector SKY_RA_DEC_180 to the IVT at UTC Time: 2013-049T16:30:35.000 PROCESSING Starting on PROFILE Command at 26654.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-049T16:35:24.000 ) This is Command #11 from the Event List TARGET / Command #12: Primary Inertial Vector: TITAN_LAT_SSCLON_176 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 26655.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-049T16:35:25.000 ) This is Command #12 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_SSCLON_176; SECONDARY BODY: NEG_X; SECONDARY INERTIAL: SKY_RA_DEC_180; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 26662.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-049T16:35:32.000 ) This is Command #13 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 9.9500 Simulated Maneuver End Time (UTC): 2013-049T16:35:42.120 Turn Magnitude for 7OFFSET (milliradians): 0.2337 Adding/Replacing Vector TITAN to the IVT at UTC Time: 2013-049T22:26:04.000 Adding/Replacing Vector SKY_RA_DEC_181 to the IVT at UTC Time: 2013-049T22:26:05.000 PROCESSING Starting on PROFILE Command at 47984.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-049T22:30:54.000 ) This is Command #14 from the Event List PROCESSING Starting on TARGET Command at 47985.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-049T22:30:55.000 ) This is Command #15 from the Event List PRIMARY BODY: ISS_NAC; PRIMARY INERTIAL: TITAN; SECONDARY BODY: NEG_X; SECONDARY INERTIAL: SKY_RA_DEC_181; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 47992.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-049T22:31:02.000 ) This is Command #16 from the Event List QUANTIZED ANGLES: 0.958 0.000 0.958 mrad Profiled Maneuver time (seconds): 22.6781 Simulated Maneuver End Time (UTC): 2013-049T22:31:24.870 Turn Magnitude for 7OFFSET (milliradians): 1.7352 PROCESSING Starting on OFFSET Command at 48382.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-049T22:37:32.000 ) This is Command #17 from the Event List QUANTIZED ANGLES: -0.958 0.000 0.958 mrad Profiled Maneuver time (seconds): 29.1816 Simulated Maneuver End Time (UTC): 2013-049T22:38:01.370 Turn Magnitude for 7OFFSET (milliradians): 1.9217 PROCESSING Starting on OFFSET Command at 48712.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-049T22:43:02.000 ) This is Command #18 from the Event List QUANTIZED ANGLES: -0.958 0.000 -0.958 mrad Profiled Maneuver time (seconds): 19.1032 Simulated Maneuver End Time (UTC): 2013-049T22:43:21.250 Turn Magnitude for 7OFFSET (milliradians): 1.9011 PROCESSING Starting on OFFSET Command at 49042.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-049T22:48:32.000 ) This is Command #19 from the Event List QUANTIZED ANGLES: 0.958 0.000 -0.958 mrad Profiled Maneuver time (seconds): 29.1812 Adding/Replacing Vector TITAN_LAT_SSCLON_177 to the IVT at UTC Time: 2013-049T22:48:45.000 Simulated Maneuver End Time (UTC): 2013-049T22:49:01.370 Turn Magnitude for 7OFFSET (milliradians): 1.9105 Adding/Replacing Vector SKY_RA_DEC_184 to the IVT at UTC Time: 2013-049T22:49:05.000 PROCESSING Starting on PROFILE Command at 49364.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-049T22:53:54.000 ) This is Command #20 from the Event List TARGET / Command #21: Primary Inertial Vector: TITAN_LAT_SSCLON_177 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 49365.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-049T22:53:55.000 ) This is Command #21 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_SSCLON_177; SECONDARY BODY: NEG_X; SECONDARY INERTIAL: SKY_RA_DEC_184; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 49372.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-049T22:54:02.000 ) This is Command #22 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 18.7595 Simulated Maneuver End Time (UTC): 2013-049T22:54:21.000 Turn Magnitude for 7OFFSET (milliradians): 0.8862 Adding/Replacing Vector TITAN_LAT_SSCLON_178 to the IVT at UTC Time: 2013-050T04:44:15.000 Adding/Replacing Vector SKY_RA_DEC_182 to the IVT at UTC Time: 2013-050T04:44:35.000 PROCESSING Starting on PROFILE Command at 70694.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-050T04:49:24.000 ) This is Command #23 from the Event List TARGET / Command #24: Primary Inertial Vector: TITAN_LAT_SSCLON_178 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 70695.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-050T04:49:25.000 ) This is Command #24 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_SSCLON_178; SECONDARY BODY: NEG_X; SECONDARY INERTIAL: SKY_RA_DEC_182; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 70702.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-050T04:49:32.000 ) This is Command #25 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 9.3032 Simulated Maneuver End Time (UTC): 2013-050T04:49:41.500 Turn Magnitude for 7OFFSET (milliradians): 0.2062 Adding/Replacing Vector TITAN to the IVT at UTC Time: 2013-050T10:40:04.000 Adding/Replacing Vector SKY_RA_DEC_183 to the IVT at UTC Time: 2013-050T10:40:05.000 PROCESSING Starting on PROFILE Command at 92024.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-050T10:44:54.000 ) This is Command #26 from the Event List PROCESSING Starting on TARGET Command at 92025.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-050T10:44:55.000 ) This is Command #27 from the Event List PRIMARY BODY: ISS_NAC; PRIMARY INERTIAL: TITAN; SECONDARY BODY: NEG_X; SECONDARY INERTIAL: SKY_RA_DEC_183; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 92032.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-050T10:45:02.000 ) This is Command #28 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 23.8790 Simulated Maneuver End Time (UTC): 2013-050T10:45:26.120 Turn Magnitude for 7OFFSET (milliradians): 1.4332 Adding/Replacing Vector SKY_RA_DEC_177 to the IVT at UTC Time: 2013-050T10:49:05.000 PROCESSING Starting on PROFILE Command at 92564.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-050T10:53:54.000 ) This is Command #29 from the Event List PROCESSING Starting on TARGET Command at 92565.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-050T10:53:55.000 ) This is Command #30 from the Event List PRIMARY BODY: XBAND; PRIMARY INERTIAL: EARTH; SECONDARY BODY: NEG_Y; SECONDARY INERTIAL: SKY_RA_DEC_177; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 92572.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-050T10:54:02.000 ) This is Command #31 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 1787.9126 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2013-050T11:22:10.000 Simulated Maneuver End Time (UTC): 2013-050T11:23:50.120 Turn Magnitude for 7OFFSET (milliradians): 2553.5220 PROCESSING Starting on 89EXE_CMD_SEQ Command at 94490.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-050T11:26:00.000 ) This is Command #32 from the Event List EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_11/kpt_eo.plt -----------------------------------