============ KPT ================= TIME: Tue May 19 12:30:40 2009 USER: Todd Ansty ================================== Insert Spice File: /cas/ancillary/ops/NAIF/sp/080806AP_SE_08138_10182.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/081125AP_RE_90165_18018.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/090202BP_IRRE_00256_50017.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/080806AP_PE_08138_10182.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/080806AP_SK_08138_10182.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0009.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck15May2008.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_11Mar2009_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00130.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: /export/home/eros/PDT13.2.1d/Input/KPT/kpt_defaultForXM.tlf Successfully Read KPT Spice Identification File: /cas/ancillary/ops/SCO/ssid/09_070_param.ssid 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/POST_PROBE_V11.cmt Insert Spice File: /cas/ancillary/ops/NAIF/sp/080806AP_SE_08138_10182.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/081125AP_RE_90165_18018.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/090202BP_IRRE_00256_50017.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/080806AP_PE_08138_10182.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/080806AP_SK_08138_10182.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0009.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck15May2008.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_11Mar2009_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00130.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: /export/home/eros/PDT13.2.1d/Input/KPT/kpt_defaultForXM.tlf Successfully Read KPT Spice Identification File: /cas/ancillary/ops/SCO/ssid/09_070_param.ssid 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/POST_PROBE_V11.cmt ------------------------------ CSAS-KPT Version: V12.1 ------------------------------ ************************************************************ 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): 1.52700000e-04 1.24200000e-04 3.24700000e-04 RWA Max Rates(rad/s): 2.46800000e-03 2.96200000e-03 4.88600000e-03 RWA Max Accel(rad/s/s): 1.35300000e-05 1.62300000e-05 2.67800000e-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: 2009-285T07:10:35.000 Adding/Replacing Vector SKY_RA_DEC_131 to the IVT at UTC Time: 2009-285T07:15:30.000 Adding/Replacing Vector TITAN_LAT_VIEW_130 to the IVT at UTC Time: 2009-285T07:39:59.000 Adding/Replacing Vector TITAN_FOV_LIMB_130 to the IVT at UTC Time: 2009-285T07:40:10.000 PROCESSING Starting on PROFILE Command at 2086.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-285T07:45:19.000 ) This is Command #1 from the Event List TARGET / Command #2: Primary Inertial Vector: TITAN_LAT_VIEW_130 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #2: Secondary Inertial Vector: TITAN_FOV_LIMB_130 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 2087.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-285T07:45:20.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_130; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_130; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2094.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-285T07:45:27.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 111.5823 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2092.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-285T07:45:25.000 ) This is Command #4 from the Event List WARNING: Detected an Artificially Padded Geometrical Constraint Violation: KPT_NEG_Y_SUN starting at 2009-285T07:46:17.250. WARNING: Detected a Pending or Actual Geometrical Constraint Violation: NEG_Y_SUN starting at 2009-285T07:46:19.250. Simulated Maneuver End Time (UTC): 2009-285T07:47:18.750 Turn Magnitude for 7OFFSET (milliradians): 289.7448 PROCESSING Starting on PROFILE Command at 2238.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-285T07:47:51.000 ) This is Command #5 from the Event List PROCESSING Starting on DELTA_BASE Command at 2242.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-285T07:47:55.000 ) This is Command #6 from the Event List QUANTIZED ANGLES: -27.995 0.000 0.000 mrad Profiled Maneuver time (seconds): 559.0524 Simulated Maneuver End Time (UTC): 2009-285T07:57:14.250 Turn Magnitude for 7DELTA_BASE (milliradians): 15.5097 PROCESSING Starting on PROFILE Command at 2802.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-285T07:57:15.000 ) This is Command #7 from the Event List PROCESSING Starting on DELTA_BODY Command at 2806.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-285T07:57:19.000 ) This is Command #8 from the Event List QUANTIZED ANGLES: 27.995 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.9802 PROCESSING Starting on PROFILE Command at 2840.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-285T07:57:53.000 ) This is Command #9 from the Event List Simulated Maneuver End Time (UTC): 2009-285T07:57:53.120 Turn Magnitude for 7DELTA_BODY (milliradians): 29.4840 PROCESSING Starting on DELTA_BASE Command at 2844.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-285T07:57:57.000 ) This is Command #10 from the Event List QUANTIZED ANGLES: -27.995 0.000 0.000 mrad Profiled Maneuver time (seconds): 559.0139 Adding/Replacing Vector SKY_RA_DEC_132 to the IVT at UTC Time: 2009-285T08:02:42.000 Simulated Maneuver End Time (UTC): 2009-285T08:07:16.250 Turn Magnitude for 7DELTA_BASE (milliradians): 20.9010 PROCESSING Starting on PROFILE Command at 3418.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-285T08:07:31.000 ) This is Command #11 from the Event List PROCESSING Starting on TARGET Command at 3419.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-285T08:07:32.000 ) This is Command #12 from the Event List PRIMARY BODY: ISS_NAC; PRIMARY INERTIAL: SUN; SECONDARY BODY: NEG_X; SECONDARY INERTIAL: SKY_RA_DEC_132; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 3426.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-285T08:07:39.000 ) This is Command #13 from the Event List QUANTIZED ANGLES: -349.076 0.000 -1.917 mrad Profiled Maneuver time (seconds): 434.4189 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2009-285T08:10:35.000 NOTE: Detected END of Geometrical Constraint Violation: NEG_Y_SUN at 2009-285T08:11:29.120. NOTE: Detected END of Geometrical Constraint Violation: KPT_NEG_Y_SUN at 2009-285T08:11:35.120. PROCESSING Starting on 89EXE_CMD_SEQ Command at 3832.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-285T08:14:25.000 ) This is Command #14 from the Event List Simulated Maneuver End Time (UTC): 2009-285T08:14:53.620 Turn Magnitude for 7OFFSET (milliradians): 1718.9456 EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_4/kpt_eo.plt -----------------------------------