********** KPT Logfile For Engine Only Run ********** *** Date: Wed Oct 20 19:37:26 2004 *** User: Conor Andrew Nixon, 301-286-6757 ***************************************************************** Insert Spice File: /cas/ancillary/ops/NAIF/sp/041001AP_SE_04002_09011.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/040701AP_RE_04001_09001.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/sat164.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/041001AP_PE_04002_09011.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/041001AP_SK_04275_08222.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0007.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck29Sep2004.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00085.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_13/input.bvh Successfully Read IVT File: pdt_Run_13/input.ivt Successfully Read TLF File: /cas/mss/MSS.D10.3.3/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.tlf Successfully Read Momentum Models File: /cas/mss/MSS.D10.3.3/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.mmf Successfully Read Mass Properties File: /cas/mss/MSS.D10.3.3/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.mpf Successfully Read Grnd System Op Modes File: /cas/mss/MSS.D10.3.3/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.gso Successfully Read KPT Spice Identification File: /cas/mss/MSS.D10.3.3/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.sid Successfully Read Input PEF File: pdt_Run_13/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/041001AP_SE_04002_09011.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/040701AP_RE_04001_09001.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/sat164.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/041001AP_PE_04002_09011.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/041001AP_SK_04275_08222.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0007.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck29Sep2004.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00085.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_13/input.bvh Successfully Read IVT File: pdt_Run_13/input.ivt Successfully Read TLF File: /cas/mss/MSS.D10.3.3/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.tlf Successfully Read Momentum Models File: /cas/mss/MSS.D10.3.3/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.mmf Successfully Read Mass Properties File: /cas/mss/MSS.D10.3.3/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.mpf Successfully Read Grnd System Op Modes File: /cas/mss/MSS.D10.3.3/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.gso Successfully Read KPT Spice Identification File: /cas/mss/MSS.D10.3.3/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.sid Successfully Read Input PEF File: pdt_Run_13/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: V10.3 2003 ------------------------------ **** 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_FOV_LIMB_112 to the IVT at UTC Time: 2005-090T19:54:41.000 Adding/Replacing Vector TITAN to the IVT at UTC Time: 2005-090T19:55:21.000 Adding/Replacing Vector TITAN_LAT_VIEW_112 to the IVT at UTC Time: 2005-090T20:00:01.000 PROCESSING Starting on PROFILE Command at 884.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-090T20:00:10.000 ) This is Command #1 from the Event List PROCESSING Starting on TARGET Command at 885.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-090T20:00:11.000 ) This is Command #2 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 892.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-090T20:00:18.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 10.4012 PROCESSING Starting on PROFILE Command at 1184.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-090T20:05:10.000 ) This is Command #4 from the Event List TARGET / Command #5: Primary Inertial Vector: TITAN_LAT_VIEW_112 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #5: Secondary Inertial Vector: TITAN_FOV_LIMB_112 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 1185.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-090T20:05:11.000 ) This is Command #5 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_112; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_112; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 1192.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-090T20:05:18.000 ) This is Command #6 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 711.8720 PROCESSING Starting on 89EXE_CMD_SEQ Command at 1190.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-090T20:05:16.000 ) This is Command #7 from the Event List PROCESSING Starting on PROFILE Command at 2120.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-090T20:20:46.000 ) This is Command #8 from the Event List PROCESSING Starting on DELTA_BODY Command at 2124.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-090T20:20:50.000 ) This is Command #9 from the Event List QUANTIZED ANGLES: -20.037 0.000 0.000 mrad Profiled Maneuver time (seconds): 614.5036 **** WARNING: Exceeded Overall CMT Attitude or Rate Discontinuity Check *** WARNING: Commencing CMT AVOIDANCE Maneuver at 2005-090T20:20:50.120 . NOTE: Any Currently executing Profiled Maneuver will now NOT be completed in the Maneuver Time reported above. Adding/Replacing Vector TITAN_FOV_LIMB_114 to the IVT at UTC Time: 2005-090T20:21:11.000 Adding/Replacing Vector TITAN_FOV_LIMB_112 to the IVT at UTC Time: 2005-090T20:22:21.000 Adding/Replacing Vector TITAN_LAT_VIEW_114 to the IVT at UTC Time: 2005-090T20:26:31.000 PROCESSING Starting on PROFILE Command at 2774.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-090T20:31:40.000 ) This is Command #10 from the Event List TARGET / Command #11: Primary Inertial Vector: TITAN_LAT_VIEW_114 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #11: Secondary Inertial Vector: TITAN_FOV_LIMB_114 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 2775.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-090T20:31:41.000 ) This is Command #11 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_114; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_114; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2782.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-090T20:31:48.000 ) This is Command #12 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 330.3970 *** NOTE: Detected END of CMT AVOIDANCE Maneuver at 2005-090T20:31:48.120 Adding/Replacing Vector TITAN_FOV_LIMB_113 to the IVT at UTC Time: 2005-090T20:37:11.000 PROCESSING Starting on PROFILE Command at 3170.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-090T20:38:16.000 ) This is Command #13 from the Event List PROCESSING Starting on DELTA_BODY Command at 3174.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-090T20:38:20.000 ) This is Command #14 from the Event List QUANTIZED ANGLES: -16.010 0.000 0.000 mrad Profiled Maneuver time (seconds): 539.7574 Adding/Replacing Vector TITAN_LAT_VIEW_113 to the IVT at UTC Time: 2005-090T20:42:31.000 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2005-090T20:45:26.000 PROCESSING Starting on PROFILE Command at 3734.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-090T20:47:40.000 ) This is Command #15 from the Event List TARGET / Command #16: Primary Inertial Vector: TITAN_LAT_VIEW_113 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #16: Secondary Inertial Vector: TITAN_FOV_LIMB_113 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 3735.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-090T20:47:41.000 ) This is Command #16 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_113; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_113; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 3742.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-090T20:47:48.000 ) This is Command #17 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 103.3121 PROCESSING Starting on 89EXE_CMD_SEQ Command at 3830.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-090T20:49:16.000 ) This is Command #18 from the Event List EVENT SEQUENCE COMPLETED with 1 Entrances into CMT Avoidance (Save Checklist and Violations Summary Reports for more details) *************************************************************************** * EVENT SEQUENCE COMPLETED WITH INSTANCES OF Constraint AVOIDANCE ** * Maneuvers. YOU MUST CORRECT THIS PROBLEM BEFORE BUILDING THE ** * FINAL Command Sequence for Uplink. Constraint Avoidance Maneuvers ** * MAY BE, but MAY NOT ALWAYS BE, MODELLED CORRECTLY for Analysis in KPT. ** *************************************************************************** Created KPT Plot File: pdt_Run_13/kpt_eo.plt -----------------------------------