********** KPT Logfile For Engine Only Run ********** *** Date: Mon Mar 8 22:53:07 2004 *** User: cnixon : Conor Andrew Nixon, 301-286-6757 ***************************************************************** Insert Spice File: /cas/ancillary/ops/NAIF/sp/sat128.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/020514_SE_SAT105.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/981005_PLTEPH-DE405S.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/030201AP_SK_SM546_T45.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0007.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck01Oct2002.tpc SPICE Successfully Opened Successfully Read BVH File: /home/users/cnixon/PDT/Titan/s02/SOPU/pdt_Run_7/input.bvh Successfully Read IVT File: /home/users/cnixon/PDT/Titan/s02/SOPU/pdt_Run_7/input.ivt Successfully Read TLF File: /cas/msspath/MSS.D10.2/base/mss_sw/pdt/Input/KPT/kpt_default.tlf Successfully Read Momentum Models File: /cas/msspath/MSS.D10.2/base/mss_sw/pdt/Input/KPT/kpt_default.mmf Successfully Read Mass Properties File: /cas/msspath/MSS.D10.2/base/mss_sw/pdt/Input/KPT/kpt_default.mpf Successfully Read Grnd System Op Modes File: /cas/msspath/MSS.D10.2/base/mss_sw/pdt/Input/KPT/kpt_default.gso Successfully Read Input PEF File: /home/users/cnixon/PDT/Titan/s02/SOPU/pdt_Run_7/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/Cruise-Probe_Release-IOM020602.cmt Insert Spice File: /cas/ancillary/ops/NAIF/sp/sat128.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/020514_SE_SAT105.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/981005_PLTEPH-DE405S.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/030201AP_SK_SM546_T45.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0007.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck01Oct2002.tpc SPICE Successfully Opened Successfully Read BVH File: /home/users/cnixon/PDT/Titan/s02/SOPU/pdt_Run_7/input.bvh Successfully Read IVT File: /home/users/cnixon/PDT/Titan/s02/SOPU/pdt_Run_7/input.ivt Successfully Read TLF File: /cas/msspath/MSS.D10.2/base/mss_sw/pdt/Input/KPT/kpt_default.tlf Successfully Read Momentum Models File: /cas/msspath/MSS.D10.2/base/mss_sw/pdt/Input/KPT/kpt_default.mmf Successfully Read Mass Properties File: /cas/msspath/MSS.D10.2/base/mss_sw/pdt/Input/KPT/kpt_default.mpf Successfully Read Grnd System Op Modes File: /cas/msspath/MSS.D10.2/base/mss_sw/pdt/Input/KPT/kpt_default.gso Successfully Read Input PEF File: /home/users/cnixon/PDT/Titan/s02/SOPU/pdt_Run_7/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/Cruise-Probe_Release-IOM020602.cmt ---------------------------- CSAS-KPT Version: V10.1.1 August 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): 1.22800000e-04 1.01200000e-04 2.51000000e-04 RWA Max Rates(rad/s): 2.06520000e-03 2.23100000e-03 3.85150000e-03 RWA Max Accel(rad/s/s): 1.14000000e-05 1.23000000e-05 2.12000000e-05 ************************************************************ ************************************************************ * * * NOTE: ALL ERRORS, REJECTED COMMANDS, WARNINGS, * * CMT VIOLATIONS, etc, MUST BE FIXED PRIOR * * TO FINAL SEQUENCE GENERATION and UPLINK * ************************************************************ Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2004-184T09:55:41.000 Adding/Replacing Vector TITAN to the IVT at UTC Time: 2004-184T10:00:36.000 PROCESSING Starting on PROFILE Command at 2075.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-184T10:30:15.000 ) This is Command #1 from the Event List PROCESSING Starting on TARGET Command at 2076.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-184T10:30:16.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN; SECONDARY BODY: NEG_X; SECONDARY INERTIAL: SUN; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2083.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-184T10:30:23.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 0.766 0.000 -9.779 mrad Profiled Maneuver time (seconds): 51.0736 PROCESSING Starting on PROFILE Command at 2152.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-184T10:31:32.000 ) This is Command #4 from the Event List PROCESSING Starting on DELTA_BASE Command at 2156.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-184T10:31:36.000 ) This is Command #5 from the Event List QUANTIZED ANGLES: 0.000 0.000 19.462 mrad Profiled Maneuver time (seconds): 4865.4175 PROCESSING Starting on PROFILE Command at 7024.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-184T11:52:44.000 ) This is Command #6 from the Event List PROCESSING Starting on OFFSET Command at 7028.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-184T11:52:48.000 ) This is Command #7 from the Event List QUANTIZED ANGLES: -1.533 0.000 8.532 mrad Profiled Maneuver time (seconds): 32.5009 PROCESSING Starting on PROFILE Command at 7067.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-184T11:53:27.000 ) This is Command #8 from the Event List PROCESSING Starting on DELTA_BASE Command at 7071.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-184T11:53:31.000 ) This is Command #9 from the Event List QUANTIZED ANGLES: 0.000 0.000 -16.969 mrad Profiled Maneuver time (seconds): 4243.2107 PROCESSING Starting on PROFILE Command at 11318.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-184T13:04:18.000 ) This is Command #10 from the Event List PROCESSING Starting on OFFSET Command at 11322.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-184T13:04:22.000 ) This is Command #11 from the Event List QUANTIZED ANGLES: -3.739 0.000 -7.957 mrad Profiled Maneuver time (seconds): 31.4018 PROCESSING Starting on PROFILE Command at 11361.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-184T13:05:01.000 ) This is Command #12 from the Event List PROCESSING Starting on DELTA_BASE Command at 11365.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-184T13:05:05.000 ) This is Command #13 from the Event List QUANTIZED ANGLES: 0.000 0.000 16.010 mrad Profiled Maneuver time (seconds): 4002.4126 PROCESSING Starting on PROFILE Command at 15371.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-184T14:11:51.000 ) This is Command #14 from the Event List PROCESSING Starting on DELTA_BODY Command at 15375.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-184T14:11:55.000 ) This is Command #15 from the Event List QUANTIZED ANGLES: 0.000 0.000 7.957 mrad Profiled Maneuver time (seconds): 46.0582 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2004-184T14:25:41.000 PROCESSING Starting on PROFILE Command at 16395.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-184T14:28:55.000 ) This is Command #16 from the Event List PROCESSING Starting on TARGET Command at 16396.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-184T14:28:56.000 ) This is Command #17 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 16403.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-184T14:29:03.000 ) This is Command #18 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 62.0719 EVENT SEQUENCE COMPLETED SUCCESSFULLY. Created KPT Plot File: pdt_Run_7/kpt_eo.plt -----------------------------------