============ KPT ================= TIME: Mon Sep 14 11:12:46 2009 USER: Todd Ansty ================================== Insert Spice File: /cas/ancillary/ops/NAIF/sp/080806AP_SE_08138_10182.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/090507AP_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/080806AP_PE_08138_10182.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/080806AP_SK_08138_10182.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0009.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck15May2008.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_11May2009_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00133.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_3/input.bvh Successfully Read IVT File: pdt_Run_3/input.ivt Successfully Read TLF File: /export/home/eros/PDT13.4d/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_3/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/080806AP_SE_08138_10182.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/090507AP_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/080806AP_PE_08138_10182.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/080806AP_SK_08138_10182.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0009.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck15May2008.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_11May2009_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00133.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_3/input.bvh Successfully Read IVT File: pdt_Run_3/input.ivt Successfully Read TLF File: /export/home/eros/PDT13.4d/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_3/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: V13.2 ------------------------------ 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: 2009-362T08:47:04.000 Adding/Replacing Vector TITAN_FRAME_1 to the IVT at UTC Time: 2009-362T09:12:02.000 Adding/Replacing Vector TITAN_LAT_LON_130 to the IVT at UTC Time: 2009-362T09:12:04.000 Adding/Replacing Vector SKY_RA_DEC_132 to the IVT at UTC Time: 2009-362T09:12:05.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-362T09:16:53.000 ) This is Command #1 from the Event List NOTE: Primary Inertial Vector TITAN_LAT_LON_130 WILL be propagated by a ROTATE_VEC from the IVT. PROCESSING Starting on TARGET Command at 2085.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-362T09:16:54.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_LON_130; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: SKY_RA_DEC_132; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2092.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-362T09:17:01.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 980.2622 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-362T09:16:59.000 ) This is Command #4 from the Event List Simulated Maneuver End Time (UTC): 2009-362T09:33:21.500 Turn Magnitude for 7OFFSET (milliradians): 1304.7334 PROCESSING Starting on PROFILE Command at 11864.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-362T11:59:53.000 ) This is Command #5 from the Event List PROCESSING Starting on TARGET Command at 11865.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-362T11:59:54.000 ) This is Command #6 from the Event List PRIMARY BODY: NEG_Y; PRIMARY INERTIAL: TITAN; SECONDARY BODY: NEG_X; SECONDARY INERTIAL: SUN; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 11872.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-362T12:00:01.000 ) This is Command #7 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 977.9372 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2009-362T12:12:09.000 PROCESSING Starting on 89EXE_CMD_SEQ Command at 12830.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-362T12:15:59.000 ) This is Command #8 from the Event List Simulated Maneuver End Time (UTC): 2009-362T12:16:19.120 Turn Magnitude for 7OFFSET (milliradians): 1300.9539 EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_3/kpt_eo.plt -----------------------------------