********** KPT Logfile For Engine Only Run ********** *** Date: Thu Apr 14 15:16:23 2005 *** User: Conor Andrew Nixon, 301-286-6757 ***************************************************************** Insert Spice File: /cas/ancillary/ops/NAIF/sp/041210AP_SE_04308_08197.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/050120AP_RE_04002_09011.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/041210AP_PE_04324_08207.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/041210AP_SK_04329_08189.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0007.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck09Dec2004.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00089.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_9/input.bvh Successfully Read IVT File: pdt_Run_9/input.ivt Successfully Read TLF File: /cas/mss/MSS.D10.5/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.tlf Successfully Read Momentum Models File: /cas/mss/MSS.D10.5/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.mmf Successfully Read Mass Properties File: /cas/mss/MSS.D10.5/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.mpf Successfully Read Grnd System Op Modes File: /cas/mss/MSS.D10.5/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.gso Successfully Read KPT Spice Identification File: /cas/ancillary/ops/SCO/ssid/04_335_param.ssid Successfully Read Input PEF File: pdt_Run_9/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/041210AP_SE_04308_08197.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/050120AP_RE_04002_09011.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/041210AP_PE_04324_08207.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/041210AP_SK_04329_08189.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0007.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck09Dec2004.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00089.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_9/input.bvh Successfully Read IVT File: pdt_Run_9/input.ivt Successfully Read TLF File: /cas/mss/MSS.D10.5/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.tlf Successfully Read Momentum Models File: /cas/mss/MSS.D10.5/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.mmf Successfully Read Mass Properties File: /cas/mss/MSS.D10.5/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.mpf Successfully Read Grnd System Op Modes File: /cas/mss/MSS.D10.5/sci_tools/mss_sw/pdt/Input/KPT/kpt_default.gso Successfully Read KPT Spice Identification File: /cas/ancillary/ops/SCO/ssid/04_335_param.ssid Successfully Read Input PEF File: pdt_Run_9/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 ------------------------------ NOTE: Primary Inertial Vector TITAN_LAT_VIEW_179 WILL be propagated by a Chebyshev Polynomial from the IVT. (INITIAL CONDITIONS) ************************************************************ 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_LAT_VIEW_179 to the IVT at UTC Time: 2005-234T09:38:22.000 Adding/Replacing Vector TITAN_LAT_VIEW_188 to the IVT at UTC Time: 2005-234T10:03:22.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-234T10:08:31.000 ) This is Command #1 from the Event List TARGET / Command #2: Primary Inertial Vector: TITAN_LAT_VIEW_188 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): 2005-234T10:08:32.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_188; SECONDARY BODY: NEG_Z; 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): 2005-234T10:08:39.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 35.3821 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-234T10:08:37.000 ) This is Command #4 from the Event List PROCESSING Starting on DELTA_BODY Command at 3292.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-234T10:28:39.000 ) This is Command #5 from the Event List QUANTIZED ANGLES: 0.000 0.000 39.979 mrad Profiled Maneuver time (seconds): 89.4194 Adding/Replacing Vector TITAN_LAT_VIEW_189 to the IVT at UTC Time: 2005-234T10:30:52.000 Adding/Replacing Vector TITAN_LAT_VIEW_190 to the IVT at UTC Time: 2005-234T10:32:52.000 PROCESSING Starting on PROFILE Command at 3734.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-234T10:36:01.000 ) This is Command #6 from the Event List TARGET / Command #7: Primary Inertial Vector: TITAN_LAT_VIEW_189 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): 2005-234T10:36:02.000 ) This is Command #7 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_189; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: SUN; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 3742.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-234T10:36:09.000 ) This is Command #8 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 86.3251 PROCESSING Starting on PROFILE Command at 3854.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-234T10:38:01.000 ) This is Command #9 from the Event List TARGET / Command #10: Primary Inertial Vector: TITAN_LAT_VIEW_190 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 3855.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-234T10:38:02.000 ) This is Command #10 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_190; SECONDARY BODY: NEG_X; SECONDARY INERTIAL: SUN; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 3862.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-234T10:38:09.000 ) This is Command #11 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 896.2239 PROCESSING Starting on 89EXE_CMD_SEQ Command at 3860.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-234T10:38:07.000 ) This is Command #12 from the Event List Adding/Replacing Vector TITAN to the IVT at UTC Time: 2005-234T10:59:42.000 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2005-234T11:03:47.000 PROCESSING Starting on PROFILE Command at 5444.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-234T11:04:31.000 ) This is Command #13 from the Event List PROCESSING Starting on TARGET Command at 5445.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-234T11:04:32.000 ) This is Command #14 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 5452.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2005-234T11:04:39.000 ) This is Command #15 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 176.1473 EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_9/kpt_eo.plt -----------------------------------