============ KPT ================= TIME: Thu Jul 8 15:15:11 2010 USER: Todd Ansty ================================== Insert Spice File: /cas/ancillary/ops/NAIF/sp/091005AP_SE_09248_17265.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/100209AP_RE_90165_18018.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/090202BP_IRRE_00256_50017.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/cpck07Oct2009.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_11May2009_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00144.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/D14.0d_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/091005AP_SE_09248_17265.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/100209AP_RE_90165_18018.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/090202BP_IRRE_00256_50017.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/cpck07Oct2009.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_11May2009_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00144.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/D14.0d_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: V14.0 ------------------------------ 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: 2010-287T04:22:04.000 Adding/Replacing Vector SATURN_N_POLE_DIR to the IVT at UTC Time: 2010-287T04:22:05.000 Adding/Replacing Vector TITAN_LAT_SSCLON_130 to the IVT at UTC Time: 2010-287T04:46:45.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-287T04:51:54.000 ) This is Command #1 from the Event List TARGET / Command #2: Primary Inertial Vector: TITAN_LAT_SSCLON_130 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): 2010-287T04:51:55.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_SSCLON_130; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: SATURN_N_POLE_DIR; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2092.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-287T04:52:02.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: -32.021 0.000 0.000 mrad Profiled Maneuver time (seconds): 133.5082 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-287T04:52:00.000 ) This is Command #4 from the Event List Simulated Maneuver End Time (UTC): 2010-287T04:54:15.750 Turn Magnitude for 7OFFSET (milliradians): 39.6268 PROCESSING Starting on OFFSET Command at 4072.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-287T05:25:02.000 ) This is Command #5 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 119.2969 Simulated Maneuver End Time (UTC): 2010-287T05:27:01.500 Turn Magnitude for 7OFFSET (milliradians): 32.4940 PROCESSING Starting on OFFSET Command at 31792.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-287T13:07:02.000 ) This is Command #6 from the Event List QUANTIZED ANGLES: -32.021 0.000 0.000 mrad Profiled Maneuver time (seconds): 119.2954 Simulated Maneuver End Time (UTC): 2010-287T13:09:01.500 Turn Magnitude for 7OFFSET (milliradians): 31.8384 Adding/Replacing Vector TITAN_LAT_SSCLON_131 to the IVT at UTC Time: 2010-287T13:40:45.000 Adding/Replacing Vector SKY_RA_DEC_147 to the IVT at UTC Time: 2010-287T13:41:05.000 PROCESSING Starting on PROFILE Command at 34124.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-287T13:45:54.000 ) This is Command #7 from the Event List TARGET / Command #8: Primary Inertial Vector: TITAN_LAT_SSCLON_131 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 34125.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-287T13:45:55.000 ) This is Command #8 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_SSCLON_131; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: SKY_RA_DEC_147; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 34132.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-287T13:46:02.000 ) This is Command #9 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 782.8146 ***** ERROR: FR VIOLATION**************** FR07D145-1 (>60 Deg Turn Restriction) IS IN VIOLATION at 2010-287T13:55:16.500 The total Spacecraft body rates are: 0.021 2.289 0.051 (mrad/s) which exceeds the FR-specified body rate limits of: 1.250 1.540 2.600 (mrad/s) This is Violation #1 Simulated Maneuver End Time (UTC): 2010-287T13:59:05.000 Turn Magnitude for 7OFFSET (milliradians): 1353.4190 Adding/Replacing Vector TITAN to the IVT at UTC Time: 2010-287T18:01:35.000 PROCESSING Starting on PROFILE Command at 49754.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-287T18:06:24.000 ) This is Command #10 from the Event List PROCESSING Starting on TARGET Command at 49755.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-287T18:06:25.000 ) This is Command #11 from the Event List PRIMARY BODY: ISS_NAC; PRIMARY INERTIAL: TITAN; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: SATURN_N_POLE_DIR; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 49762.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-287T18:06:32.000 ) This is Command #12 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 872.7772 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2010-287T18:17:10.000 PROCESSING Starting on 89EXE_CMD_SEQ Command at 50630.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2010-287T18:21:00.000 ) This is Command #13 from the Event List Simulated Maneuver End Time (UTC): 2010-287T18:21:05.000 Turn Magnitude for 7OFFSET (milliradians): 1127.9622 EVENT SEQUENCE COMPLETED with Approximately 1 FR Violation(s) (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_2/kpt_eo.plt -----------------------------------