********** KPT Logfile For Engine Only Run ********** *** Date: Fri Jul 2 20:00:11 2004 *** User: Conor Andrew Nixon, 301-286-6757 ***************************************************************** Insert Spice File: /cas/ancillary/ops/NAIF/sp/040506AP_SE_04002_09011.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/sat164.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/040506AP_PE_94328_16357.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/040513AP_SK_04122_08222.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0007.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck05May2004.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00085.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/mss/MSS.D10.3.1/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.tlf Successfully Read Momentum Models File: /cas/mss/MSS.D10.3.1/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.mmf Successfully Read Mass Properties File: /cas/mss/MSS.D10.3.1/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.mpf Successfully Read Grnd System Op Modes File: /cas/mss/MSS.D10.3.1/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.gso Successfully Read KPT Spice Identification File: /cas/mss/MSS.D10.3.1/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.sid 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/Cruise-Probe_Release-IOM020602.cmt Insert Spice File: /cas/ancillary/ops/NAIF/sp/040506AP_SE_04002_09011.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/sat164.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/040506AP_PE_94328_16357.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/040513AP_SK_04122_08222.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0007.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck05May2004.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00085.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/mss/MSS.D10.3.1/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.tlf Successfully Read Momentum Models File: /cas/mss/MSS.D10.3.1/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.mmf Successfully Read Mass Properties File: /cas/mss/MSS.D10.3.1/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.mpf Successfully Read Grnd System Op Modes File: /cas/mss/MSS.D10.3.1/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.gso Successfully Read KPT Spice Identification File: /cas/mss/MSS.D10.3.1/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.sid 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/Cruise-Probe_Release-IOM020602.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): 1.22800000e-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 TITAN to the IVT at UTC Time: 2004-299T17:00:28.000 Adding/Replacing Vector TITAN_N_POLE_DIR to the IVT at UTC Time: 2004-299T17:25:28.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T17:30:17.000 ) 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): 2004-299T17:30:18.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN; SECONDARY BODY: POS_X; SECONDARY INERTIAL: TITAN_N_POLE_DIR; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2092.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T17:30:25.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: -6.040 0.000 -9.970 mrad Profiled Maneuver time (seconds): 667.8925 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T17:30:23.000 ) This is Command #4 from the Event List PROCESSING Starting on PROFILE Command at 2931.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T17:44:24.000 ) This is Command #5 from the Event List PROCESSING Starting on DELTA_BASE Command at 2935.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T17:44:28.000 ) This is Command #6 from the Event List QUANTIZED ANGLES: 0.000 0.000 21.955 mrad Profiled Maneuver time (seconds): 2196.5731 PROCESSING Starting on PROFILE Command at 5132.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T18:21:05.000 ) This is Command #7 from the Event List PROCESSING Starting on DELTA_BODY Command at 5136.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T18:21:09.000 ) This is Command #8 from the Event List QUANTIZED ANGLES: 2.013 0.000 0.000 mrad Profiled Maneuver time (seconds): 40.1304 PROCESSING Starting on PROFILE Command at 5177.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T18:21:50.000 ) This is Command #9 from the Event List PROCESSING Starting on DELTA_BASE Command at 5181.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T18:21:54.000 ) This is Command #10 from the Event List QUANTIZED ANGLES: 0.000 0.000 -21.955 mrad Profiled Maneuver time (seconds): 2196.5917 PROCESSING Starting on PROFILE Command at 7378.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T18:58:31.000 ) This is Command #11 from the Event List PROCESSING Starting on DELTA_BODY Command at 7382.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T18:58:35.000 ) This is Command #12 from the Event List QUANTIZED ANGLES: 2.013 0.000 0.000 mrad Profiled Maneuver time (seconds): 40.1304 PROCESSING Starting on PROFILE Command at 7423.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T18:59:16.000 ) This is Command #13 from the Event List PROCESSING Starting on DELTA_BASE Command at 7427.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T18:59:20.000 ) This is Command #14 from the Event List QUANTIZED ANGLES: 0.000 0.000 21.955 mrad Profiled Maneuver time (seconds): 2196.6085 PROCESSING Starting on PROFILE Command at 9624.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T19:35:57.000 ) This is Command #15 from the Event List PROCESSING Starting on DELTA_BODY Command at 9628.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T19:36:01.000 ) This is Command #16 from the Event List QUANTIZED ANGLES: 2.013 0.000 0.000 mrad Profiled Maneuver time (seconds): 40.1304 PROCESSING Starting on PROFILE Command at 9669.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T19:36:42.000 ) This is Command #17 from the Event List PROCESSING Starting on DELTA_BASE Command at 9673.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T19:36:46.000 ) This is Command #18 from the Event List QUANTIZED ANGLES: 0.000 0.000 -21.955 mrad Profiled Maneuver time (seconds): 2196.6096 PROCESSING Starting on PROFILE Command at 11870.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T20:13:23.000 ) This is Command #19 from the Event List PROCESSING Starting on DELTA_BODY Command at 11874.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T20:13:27.000 ) This is Command #20 from the Event List QUANTIZED ANGLES: 2.013 0.000 0.000 mrad Profiled Maneuver time (seconds): 40.1304 PROCESSING Starting on PROFILE Command at 11915.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T20:14:08.000 ) This is Command #21 from the Event List PROCESSING Starting on DELTA_BASE Command at 11919.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T20:14:12.000 ) This is Command #22 from the Event List QUANTIZED ANGLES: 0.000 0.000 21.955 mrad Profiled Maneuver time (seconds): 2196.6083 PROCESSING Starting on PROFILE Command at 14116.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T20:50:49.000 ) This is Command #23 from the Event List PROCESSING Starting on DELTA_BODY Command at 14120.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T20:50:53.000 ) This is Command #24 from the Event List QUANTIZED ANGLES: 2.013 0.000 0.000 mrad Profiled Maneuver time (seconds): 40.1304 PROCESSING Starting on PROFILE Command at 14161.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T20:51:34.000 ) This is Command #25 from the Event List PROCESSING Starting on DELTA_BASE Command at 14165.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T20:51:38.000 ) This is Command #26 from the Event List QUANTIZED ANGLES: 0.000 0.000 -21.955 mrad Profiled Maneuver time (seconds): 2196.5921 PROCESSING Starting on PROFILE Command at 16362.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T21:28:15.000 ) This is Command #27 from the Event List PROCESSING Starting on DELTA_BODY Command at 16366.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T21:28:19.000 ) This is Command #28 from the Event List QUANTIZED ANGLES: 2.013 0.000 0.000 mrad Profiled Maneuver time (seconds): 40.1304 PROCESSING Starting on PROFILE Command at 16407.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T21:29:00.000 ) This is Command #29 from the Event List PROCESSING Starting on DELTA_BASE Command at 16411.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T21:29:04.000 ) This is Command #30 from the Event List QUANTIZED ANGLES: 0.000 0.000 21.955 mrad Profiled Maneuver time (seconds): 2196.5725 PROCESSING Starting on PROFILE Command at 20144.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T22:31:17.000 ) This is Command #31 from the Event List PROCESSING Starting on TARGET Command at 20145.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T22:31:18.000 ) This is Command #32 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 20152.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-299T22:31:25.000 ) This is Command #33 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 660.2857 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2004-299T22:40:33.000 EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_6/kpt_eo.plt -----------------------------------