********** KPT Logfile For Engine Only Run ********** *** Date: Tue Nov 8 20:22:59 2005 *** User: Conor Andrew Nixon, 301-286-6757 ***************************************************************** Insert Spice File: /cas/ancillary/ops/NAIF/sp/050720AP_SE_05119_08222.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/050923AP_RE_04002_09011.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/050720AP_PE_05119_08222.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/050720AP_SK_05119_08222.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0008.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck29Apr2005.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_08Apr2005_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00093.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_6/input.bvh Successfully Read IVT File: pdt_Run_6/input.ivt Successfully Read TLF File: /cas/msspath/MSS.D11.0/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.tlf Successfully Read Momentum Models File: /cas/msspath/MSS.D11.0/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.mmf Successfully Read Mass Properties File: /cas/msspath/MSS.D11.0/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.mpf Successfully Read Grnd System Op Modes File: /cas/msspath/MSS.D11.0/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.gso Successfully Read KPT Spice Identification File: /cas/ancillary/ops/SCO/ssid/05_098_param.ssid Successfully Read Input PEF File: pdt_Run_6/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_V10.cmt Insert Spice File: /cas/ancillary/ops/NAIF/sp/050720AP_SE_05119_08222.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/050923AP_RE_04002_09011.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/050720AP_PE_05119_08222.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/050720AP_SK_05119_08222.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0008.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck29Apr2005.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_08Apr2005_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00093.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_6/input.bvh Successfully Read IVT File: pdt_Run_6/input.ivt Successfully Read TLF File: /cas/msspath/MSS.D11.0/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.tlf Successfully Read Momentum Models File: /cas/msspath/MSS.D11.0/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.mmf Successfully Read Mass Properties File: /cas/msspath/MSS.D11.0/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.mpf Successfully Read Grnd System Op Modes File: /cas/msspath/MSS.D11.0/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.gso Successfully Read KPT Spice Identification File: /cas/ancillary/ops/SCO/ssid/05_098_param.ssid Successfully Read Input PEF File: pdt_Run_6/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_V10.cmt ------------------------------ CSAS-KPT Version: V11.00 2004 ------------------------------ **** 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): 1.54400000e-04 1.25500000e-04 3.29100000e-04 RWA Max Rates(rad/s): 2.45900000e-03 2.95000000e-03 4.88000000e-03 RWA Max Accel(rad/s/s): 1.34800000e-05 1.61700000e-05 2.67400000e-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: 2006-078T11:56:02.000 Adding/Replacing Vector TITAN_FRAME_1 to the IVT at UTC Time: 2006-078T12:21:00.000 Adding/Replacing Vector TITAN_LAT_LON_122 to the IVT at UTC Time: 2006-078T12:21:02.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-078T12:25:51.000 ) This is Command #1 from the Event List NOTE: Primary Inertial Vector TITAN_LAT_LON_122 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): 2006-078T12:25:52.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_LON_122; SECONDARY BODY: NEG_X; 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): 2006-078T12:25:59.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 0.000 0.000 20.037 mrad Profiled Maneuver time (seconds): 65.8233 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-078T12:25:57.000 ) This is Command #4 from the Event List PROCESSING Starting on OFFSET Command at 2992.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-078T12:40:59.000 ) This is Command #5 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 61.7783 PROCESSING Starting on OFFSET Command at 7252.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-078T13:51:59.000 ) This is Command #6 from the Event List QUANTIZED ANGLES: 0.000 0.000 20.037 mrad Profiled Maneuver time (seconds): 61.7785 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2006-078T14:02:07.000 PROCESSING Starting on PROFILE Command at 7934.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-078T14:03:21.000 ) This is Command #7 from the Event List PROCESSING Starting on TARGET Command at 7935.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-078T14:03:22.000 ) This is Command #8 from the Event List PRIMARY BODY: ISS_NAC; PRIMARY INERTIAL: TITAN; SECONDARY BODY: NEG_X; SECONDARY INERTIAL: SUN; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 7942.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-078T14:03:29.000 ) This is Command #9 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 64.6049 PROCESSING Starting on 89EXE_CMD_SEQ Command at 8140.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2006-078T14:06:47.000 ) 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_6/kpt_eo.plt -----------------------------------