********** KPT Logfile For Engine Only Run ********** *** Date: Wed Aug 11 19:23:13 2004 *** User: Conor Andrew Nixon, 301-286-6757 ***************************************************************** Insert Spice File: /cas/ancillary/ops/NAIF/sp/040622AP_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/040622AP_PE_04002_09011.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/040622AP_SK_04122_08222.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0007.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck21Jun2004.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00085.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_4/input.bvh Successfully Read IVT File: pdt_Run_4/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_4/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/040622AP_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/040622AP_PE_04002_09011.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/040622AP_SK_04122_08222.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0007.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck21Jun2004.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00085.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_4/input.bvh Successfully Read IVT File: pdt_Run_4/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_4/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: 2004-348T16:07:34.000 Adding/Replacing Vector TITAN_FOV_LIMB_199 to the IVT at UTC Time: 2004-348T16:26:54.000 Adding/Replacing Vector TITAN_LAT_VIEW_199 to the IVT at UTC Time: 2004-348T16:32:14.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-348T16:37:23.000 ) This is Command #1 from the Event List TARGET / Command #2: Primary Inertial Vector: TITAN_LAT_VIEW_199 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #2: Secondary Inertial Vector: TITAN_FOV_LIMB_199 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 2085.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-348T16:37:24.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_199; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_199; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2092.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-348T16:37:31.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: -39.979 0.000 0.000 mrad Profiled Maneuver time (seconds): 230.5165 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-348T16:37:29.000 ) This is Command #4 from the Event List PROCESSING Starting on OFFSET Command at 2812.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-348T16:49:31.000 ) This is Command #5 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 141.3849 PROCESSING Starting on OFFSET Command at 4252.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-348T17:13:31.000 ) This is Command #6 from the Event List QUANTIZED ANGLES: -2.205 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2013 PROCESSING Starting on OFFSET Command at 5692.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-348T17:37:31.000 ) This is Command #7 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2062 PROCESSING Starting on OFFSET Command at 7132.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-348T18:01:31.000 ) This is Command #8 from the Event List QUANTIZED ANGLES: -2.205 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2020 PROCESSING Starting on OFFSET Command at 8572.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-348T18:25:31.000 ) This is Command #9 from the Event List QUANTIZED ANGLES: -39.979 0.000 0.000 mrad Profiled Maneuver time (seconds): 137.4296 Adding/Replacing Vector TITAN to the IVT at UTC Time: 2004-348T18:27:34.000 PROCESSING Starting on PROFILE Command at 8984.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-348T18:32:23.000 ) This is Command #10 from the Event List PROCESSING Starting on TARGET Command at 8985.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-348T18:32:24.000 ) This is Command #11 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 8992.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-348T18:32:31.000 ) This is Command #12 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 188.7889 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2004-348T18:32:39.000 PROCESSING Starting on 89EXE_CMD_SEQ Command at 9230.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-348T18:36:29.000 ) This is Command #13 from the Event List EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_4/kpt_eo.plt -----------------------------------