********** KPT Logfile For Engine Only Run ********** *** Date: Tue Jun 29 12:55:49 2004 *** User: Amy Simon ***************************************************************** Insert Spice File: /cas/ancillary/ops/NAIF/sp/040506AP_SE_04002_09011.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/sat128.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_1/input.bvh Successfully Read IVT File: pdt_Run_1/input.ivt Successfully Read TLF File: /cas/msspath/MSS.D10.3.1/base/mss_sw/pdt/Input/KPT/kpt_default.tlf Successfully Read Input PEF File: pdt_Run_1/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/sat128.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_1/input.bvh Successfully Read IVT File: pdt_Run_1/input.ivt Successfully Read TLF File: /cas/msspath/MSS.D10.3.1/base/mss_sw/pdt/Input/KPT/kpt_default.tlf Successfully Read Input PEF File: pdt_Run_1/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 ------------------------------ ************************************************************ 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 SATURN_LAT_SSCLON_101 to the IVT at UTC Time: 2004-313T09:12:45.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-313T09:17:54.000 ) This is Command #1 from the Event List TARGET / Command #2: Primary Inertial Vector: SATURN_LAT_SSCLON_101 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): 2004-313T09:17:55.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: SATURN_LAT_SSCLON_101; 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): 2004-313T09:18:02.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 60.016 0.000 0.000 mrad Profiled Maneuver time (seconds): 185.9253 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-313T09:18:00.000 ) This is Command #4 from the Event List PROCESSING Starting on OFFSET Command at 3292.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-313T09:38:02.000 ) This is Command #5 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 173.2281 PROCESSING Starting on OFFSET Command at 40492.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-313T19:58:02.000 ) This is Command #6 from the Event List QUANTIZED ANGLES: 60.016 0.000 0.000 mrad Profiled Maneuver time (seconds): 173.2282 PROCESSING Starting on OFFSET Command at 41392.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-313T20:13:02.000 ) This is Command #7 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 173.2281 PROCESSING Starting on OFFSET Command at 74692.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-314T05:28:02.000 ) This is Command #8 from the Event List QUANTIZED ANGLES: 60.016 0.000 0.000 mrad Profiled Maneuver time (seconds): 173.2282 PROCESSING Starting on PROFILE Command at 75584.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-314T05:42:54.000 ) This is Command #9 from the Event List PROCESSING Starting on TARGET Command at 75585.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-314T05:42:55.000 ) This is Command #10 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: SATURN; SECONDARY BODY: NEG_X; SECONDARY INERTIAL: SUN; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 75592.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-314T05:43:02.000 ) This is Command #11 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 185.5465 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2004-314T05:43:10.000 PROCESSING Starting on 89EXE_CMD_SEQ Command at 75830.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2004-314T05:47:00.000 ) This is Command #12 from the Event List EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_1/kpt_eo.plt -----------------------------------