============ KPT ================= TIME: Tue Jun 3 19:27:41 2008 USER: Conor Andrew Nixon, 301-286-6757 ================================== Insert Spice File: /cas/ancillary/ops/NAIF/sp/070918AP_SE_07261_10191.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/070815AP_RE_90165_14363.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/070416BP_IRRE_00256_14363.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/070918AP_PE_07261_10191.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/070918AP_SK_07261_10191.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0008.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck16Apr2008.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_01Oct2007_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00113.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_1/input.bvh Successfully Read IVT File: pdt_Run_1/input.ivt Successfully Read TLF File: /cas/msspath/MSS.D13.1/sci_tools/mss_sw/pdt/Input/KPT/kpt_defaultForXM.tlf Successfully Read Momentum Models File: /cas/msspath/MSS.D13.1/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.mmf Successfully Read Mass Properties File: /cas/msspath/MSS.D13.1/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.mpf Successfully Read Grnd System Op Modes File: /cas/msspath/MSS.D13.1/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.gso Successfully Read KPT Spice Identification File: /cas/ancillary/ops/SCO/ssid/07_274_param.ssid Successfully Read Input PEF File: pdt_Run_1/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/070918AP_SE_07261_10191.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/070815AP_RE_90165_14363.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/070416BP_IRRE_00256_14363.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/070918AP_PE_07261_10191.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/070918AP_SK_07261_10191.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0008.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck16Apr2008.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_01Oct2007_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00113.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_1/input.bvh Successfully Read IVT File: pdt_Run_1/input.ivt Successfully Read TLF File: /cas/msspath/MSS.D13.1/sci_tools/mss_sw/pdt/Input/KPT/kpt_defaultForXM.tlf Successfully Read Momentum Models File: /cas/msspath/MSS.D13.1/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.mmf Successfully Read Mass Properties File: /cas/msspath/MSS.D13.1/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.mpf Successfully Read Grnd System Op Modes File: /cas/msspath/MSS.D13.1/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.gso Successfully Read KPT Spice Identification File: /cas/ancillary/ops/SCO/ssid/07_274_param.ssid Successfully Read Input PEF File: pdt_Run_1/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: V12.1 ------------------------------ NOTE: Primary Inertial Vector TITAN_LAT_VIEW_104 WILL be propagated by a Chebyshev Polynomial from the IVT. (INITIAL CONDITIONS) NOTE: Secondary Inertial Vector TITAN_FOV_LIMB_104 WILL be propagated by a Chebyshev Polynomial from the IVT. (INITIAL CONDITIONS) ************************************************************ 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_LAT_VIEW_104 to the IVT at UTC Time: 2008-324T17:40:58.000 Adding/Replacing Vector TITAN_FOV_LIMB_104 to the IVT at UTC Time: 2008-324T17:41:13.000 Adding/Replacing Vector TITAN to the IVT at UTC Time: 2008-324T18:06:33.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2008-324T18:11:22.000 ) 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): 2008-324T18:11:23.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: SUN; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2092.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2008-324T18:11:30.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 0.000 0.000 55.031 mrad Profiled Maneuver time (seconds): 678.8208 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2008-324T18:11:28.000 ) This is Command #4 from the Event List Simulated Maneuver End Time (UTC): 2008-324T18:22:49.000 Turn Magnitude for 7OFFSET (milliradians): 1115.7571 PROCESSING Starting on PROFILE Command at 2992.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2008-324T18:26:30.000 ) This is Command #5 from the Event List PROCESSING Starting on DELTA_BODY Command at 2996.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2008-324T18:26:34.000 ) This is Command #6 from the Event List QUANTIZED ANGLES: 0.000 0.000 -85.998 mrad Profiled Maneuver time (seconds): 8600.2314 Simulated Maneuver End Time (UTC): 2008-324T20:49:54.370 Turn Magnitude for 7DELTA_BODY (milliradians): 76.5233 PROCESSING Starting on PROFILE Command at 11684.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2008-324T20:51:22.000 ) This is Command #7 from the Event List PROCESSING Starting on TARGET Command at 11685.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2008-324T20:51:23.000 ) This is Command #8 from the Event List PRIMARY BODY: NEG_Y; PRIMARY INERTIAL: TITAN; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: SUN; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 11692.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2008-324T20:51:30.000 ) This is Command #9 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 83.5489 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2008-324T20:51:38.000 Simulated Maneuver End Time (UTC): 2008-324T20:52:53.750 Turn Magnitude for 7OFFSET (milliradians): 36.7250 PROCESSING Starting on 89EXE_CMD_SEQ Command at 11930.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2008-324T20:55:28.000 ) This is Command #10 from the Event List EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_1/kpt_eo.plt -----------------------------------