#! /mnt/svejk0/ras/ras/cfg/master_cfg #----------------------------------------------------------------------------- # Flyby Setup & IO Pass Information # spacecraft - specifies the name of a SPICE recognized observer body # target - specifies the name of a SPICE recognized target body # data_take_number - Cruise IEB's < 30, Tour IEB's > 30 # if larger than 255, it will roll back to 0 # target_name - use target # IO_PDT_configfile - PDT config specifies SPICE files for that sequence # IO_smtfile_1 - path and file name of SMT file received from IO # (Science Planning Web Site) # IO_smtfile_2 - path and file name of SMT file # (often: PEF are 2 Sequences, SMT are 1 seqence) # IO_peffile - path and file name of PEF file received from IO # (Science Planning Web Site) # IEB_number_in_PEF - PEF file can contain multiple IEBs. # If 0 config_merge will prompt user #----------------------------------------------------------------------------- spacecraft Cassini target Phoebe data_take_number 32 IO_PDT_configfile /afs/jpl/group/casops/dom/data/main/pdt_config/S01_ssup_psiv1_040324_a_pdt.cfg IO_smtfile_1 /afs/jpl.nasa.gov/group/casradar/tour/s01/S01_040407b_newsmt.rpt IO_peffile /afs/jpl/group/casops/dom/data/seq/S01/pef/z0010d_full.pef IEB_number_in_PEF 2 #----------------------------------------------------------------------------- # RMSS IO Parameters (populated by the config_merge process) # IEB_Trigger - SCLK value of trigger given in PEF file # This is second trigger (not IDAPT trigger) # IEB_delta_trigger - Delta trigger time update due to live ivp update # IDAPT_delta - time prior to IEB_Trigger. Value always second prior to Trigger # IEB_duration - time from IEB_Trigger to Halt # DataVolumeAllocation - time from IEB_Trigger to Halt # DataRateTime_1 - Time of Data Rate Mode Change # DataRateTime_2 - Time of Data Rate Mode Change # DataRateTime_3 - Time of Data Rate Mode Change # DataRateTime_4 - Time of Data Rate Mode Change # DataRateTime_5 - Time of Data Rate Mode Change # DataRateTime_6 - Time of Data Rate Mode Change # DataRateTime_7 - Time of Data Rate Mode Change # DataRateTime_8 - Time of Data Rate Mode Change # DataRateTime_9 - Time of Data Rate Mode Change # DataRate_1 - The S/C Date Rate starting at correlated DateRateTime # DataRate_2 - The S/C Date Rate starting at correlated DateRateTime # DataRate_3 - The S/C Date Rate starting at correlated DateRateTime # DataRate_4 - The S/C Date Rate starting at correlated DateRateTime # DataRate_5 - The S/C Date Rate starting at correlated DateRateTime # DataRate_6 - The S/C Date Rate starting at correlated DateRateTime # DataRate_7 - The S/C Date Rate starting at correlated DateRateTime # DataRate_8 - The S/C Date Rate starting at correlated DateRateTime # DataRate_9 - The S/C Date Rate starting at correlated DateRateTime # PowerTransitionTime_1 - Time of Power Transition Allocation # PowerTransitionTime_2 - Time of Power Transition Allocation # PowerTransitionTime_3 - Time of Power Transition Allocation # PowerTransitionTime_4 - Time of Power Transition Allocation # PowerTransitionTime_5 - Time of Power Transition Allocation # PowerTransitionTime_6 - Time of Power Transition Allocation # PowerTransitionTime_7 - Time of Power Transition Allocation # PowerTransitionTime_8 - Time of Power Transition Allocation # PowerTransitionTime_9 - Time of Power Transition Allocation # PowerAllocation_1 - Power Level Allocation (ie: 0,55,86) # PowerAllocation_2 - Power Level Allocation (ie: 0,55,86) # PowerAllocation_3 - Power Level Allocation (ie: 0,55,86) # PowerAllocation_4 - Power Level Allocation (ie: 0,55,86) # PowerAllocation_5 - Power Level Allocation (ie: 0,55,86) # PowerAllocation_6 - Power Level Allocation (ie: 0,55,86) # PowerAllocation_7 - Power Level Allocation (ie: 0,55,86) # PowerAllocation_8 - Power Level Allocation (ie: 0,55,86) # PowerAllocation_9 - Power Level Allocation (ie: 0,55,86) #----------------------------------------------------------------------------- IEB_Trigger 1465655576 IEB_delta_trigger 2 s IDAPT_delta -30 s IEB_duration 41685 s DataVolumeAllocation 0 DataRateTime_1 1465655261 DataRateTime_2 1465660721 DataRateTime_3 1465682261 DataRateTime_4 1465698769 DataRate_1 364800 DataRate_2 0 DataRate_3 364800 DataRate_4 0 PowerTransitionTime_1 1465655394 PowerTransitionTime_2 1465660721 PowerTransitionTime_3 1465682303 PowerTransitionTime_4 1465697524 PowerAllocation_1 86 W PowerAllocation_2 55 W PowerAllocation_3 86 W PowerAllocation_4 55 W #----------------------------------------------------------------------------- # Epoch Setup # epoch_selection - specifies how the epoch time for this config file is set # Valid values for: epoch_selection # absolute - The value specified by epoch_time is used directly # closest_flyby - The closest approach time nearest to epoch_time is used # epoch_accuracy - The precision of the search for the closest flyby time # epoch_time - The epoch time to use, or the starting point in the search for # the epoch time to use. #----------------------------------------------------------------------------- epoch_selection closest_flyby epoch_accuracy 1 ms epoch_time 2004-163T19:33:37.000 #----------------------------------------------------------------------------- # SAR Pointing and IVD Setup # look_direction - Specifies which side to tilt the 5 beams towards # Valid values for: look_direction # right - Look to the right when you look along the velocity direction from # behind the spacecraft. # left - Look to the left when you look along the velocity direction from # behind the spacecraft. # sc_orientation - Specifies whether plus or minus X should be closest to the # velocity direction during the IVD interval. # ie., resolve the 180 degree ambiguitiy in SAR pointing. # Valid values for: sc_orientation # -x_direction_to_velocity - Hold -X towards the velocity direction # +x_direction_to_velocity - Hold +X towards the velocity direction # ivd_file - the name of the output IVD file to create # start_time_ivd - Start time of SAR profile - used to create ivd files # time_step_ivd - used to create ivd files # end_time_ivd - End time of SAR profile - used to create ivd files # ivd_time_pad - amount of time to add to the IVD time interval on each side. # This creates an IVD file valid for a longer time interval. #----------------------------------------------------------------------------- look_direction right sc_orientation -x_direction_to_velocity ivd_file UserEdit RADAR_S01_PORT1_TX_yymmdd.ivd start_time_ivd -16 min time_step_ivd 1 s end_time_ivd 16 min ivd_time_pad 6 min #----------------------------------------------------------------------------- # Default Spice Directories # hasekSPICEdir - Default path to SPICE files on hasek (except ckernels) # Note: Also default for unknown workstation # (according to config_merge) # casradar2SPICEdir - Default path to SPICE files on casradar2 (except ckernels) #----------------------------------------------------------------------------- hasekSPICEdir /home/ras/dat/naif/ casradar2SPICEdir /cas/ancillary/ops/NAIF/ #----------------------------------------------------------------------------- # Spice File Setup # spice_directory - Directory where Spice files reside (except ckernels) # If not present, fully qualified names must be used # tour_ephemeris - SPICE file: the spacecraft ephemeris file # sclk_kernel - SPICE file: sclk to UTC translation data # time_kernel - SPICE file: leapseconds data # instrument_kernel - SPICE file: field of view data for an instrument # frame_kernel - SPICE file: instrument frame definitions # planetary_constants_kernel - SPICE file: GM, radii etc for planets # solarsystem_ephemeris_kernel - SPICE file: ephemeris data for planet # barycenters # planet_ephemeris_kernel - SPICE file: ephemeris data for specific planet #----------------------------------------------------------------------------- spice_directory /home/ras/dat/naif/ tour_ephemeris sp/041014R_SCPSE_01066_04199.bsp sclk_kernel sclk/cas00090.tsc time_kernel lsk/naif0007.tls instrument_kernel ik/cas_radar_v11.ti frame_kernel fk/cas_v39.tf planetary_constants_kernel pck/cpck14Oct2004.tpc solarsystem_ephemeris_kernel sp/041014R_SCPSE_01066_04199.bsp planet_ephemeris_kernel sp/041014R_SCPSE_01066_04199.bsp #----------------------------------------------------------------------------- # Ckernel Names # ckernel_directory - Directory where C-kernel files reside # If not present, fully qualified names must be used # ckernel - name of first ckernel file to load # ckernel_* - optional additional ckernel files to load # * is replaced by 1,2,3.. #----------------------------------------------------------------------------- ckernel /home/ras/dat/naif/ck/04161_04164ra.bc #----------------------------------------------------------------------------- # Time Interval Specifications # Interval specificiations are epoch relative and consist of three associated # keywords (time_step_xx, start_time_xx, end_time_xx where xx is a string # identifying a particular interval). # time_step - The default time step to use # start_time - Default epoch relative starting time # end_time - Default epoch relative ending time #----------------------------------------------------------------------------- time_step 10 s start_time 150 min end_time 156 min #----------------------------------------------------------------------------- # RMSS Constants and semi-fixed parameters # InstDensityNavErrors - Switch the usage of Navigation Errors # in InstructionDensity Routine # Valid values for: InstDensityNavErrors # on - Use nav errors, this is the normal setting # off - Don't use nav errors # Some small distant targets may need the off setting # CDS_Cmd_Delay - Time delay between time command in the PEF going to CDS # vs the RADAR execution of that command. # (Expected to be +1 second) # SoftPowerCycle - Default = enable to allow RMSS to power down if there # is a radiometer division between two Active modes # (If Disabled, RMSS will not power down until last active mode) # AutoGainCycles - When AutoGain is enabled or a FLTSW autogain # Feature boundary is encountered # RMSS should insert rapid copies of the instruction # to give AutoGain ability to step at the start # AutoRadCycles - When AutoRad is enabled # RMSS should insert rapid copies of the instruction # to give AutoRAD ability to step at the start # Calibration_Instruction_Method - RMSS insert calibraion mode # (rerouted,chirp, leakage, ant only) # These can be inserted in 1 of 4 different locations in the IEB timeline # 0 - Normal Calibration Insert: Between each mode change. # 1 - Lumped.Beginning: Gather all calibrations to be done and insert # block at first location only # 2 - Lumped.Ending: Gather all calibrations to be done and insert # block at last location # 3 - Lumped.both ends: Gather all calibrations to be done and insert # at beginning and a copy at the end # Max_Scat_Incidence_Used - (default 60) During Scatterometry RMSS will update instruction based on validtime upto normally 60 degress. # However if PDT designs go to higher incidence or to reduce FINs the user can adjust this value. # Calibration_SARH_ANT_Cycles - Allows user to state the number of Ant calibration cycles to be inserted for the calibrartion routines. # SlowCFSCompression - Percentage (integer: between 0-100) of the Slow_Cfs parameter that RMSS is allowed to compress in order to # reduce the number of Slow Field Instructions (SIN). # BpdGapAdjustPercentage - Percentage (integer: between 0-100) of the amount of the Burst Period that RMSS is allowed to # increase the BPD in order to reduce the gap between ILXes. (goes with Bpd_Adjust below) # Scat_Validtime_Adjust_For_Gaps - (enable or disable) If enabled, RMSS may decrease the VALIDTIME time value (Up to a limit) to # reduce gaps between instruction boundaries (This can be enabled/disabled based on mode) # Alth_Validtime_Adjust_For_Gaps - (enable or disable) see note above. # Sarh_Validtime_Adjust_For_Gaps - (enable or disable) see note above. # Sarl_Validtime_Adjust_For_Gaps - (enable or disable) see note above. # Scat_Bpd_Adjust_For_Gaps - (enable or disable) If enabled, RMSS may increase Burst Period (BPD) (Up to a limit) to reduce gaps # between instruction boundaries (This can be enabled/disabled based on mode) # Alth_Bpd_Adjust_For_Gaps - (enable or disable) see note above. # Sarh_Bpd_Adjust_For_Gaps - (enable or disable) see note above. # Sarl_Bpd_Adjust_For_Gaps - (enable or disable) see note above. # RMSS_UserInputFile_1 - Provide a wtk formatted file to overwrite any # RMSS create section of the IEB. # The User Input File will NOT overwrite Power or TNC instructions. # The first file must have the '1' extention, # if there are more this extenstion should be incremented #----------------------------------------------------------------------------- InstDensityNavErrors off CDS_Cmd_Delay 1 s AutoGainCycles 5 AutoRadCycles 3 #----------------------------------------------------------------------------- # Radar Commanding Parameters # radar mode options: # sarh, sarl, altimeter, scatterometer, scatterometer_compressed, radiometer # Calibration source: # 0(normal), 1(antenna cal source), 2(noise diode), 3(resitive load) # 4(rerouted chirp),5(leakage),6(radiometer only),7(transmit only) # 8(auto gain) # baq: # 0(8-2 baq),1(8-1 baq), 2(8-0,no science data),3(ALTL compressed) # 4(8-4MSB), 5(8-8 straight), 6(ALTL),7(ALTH) # beam mask # 00000 : all beams disabled # 00001: beam 1 only # .. # 00100: beam 3 only # 11111: all beams only # Division keywords are identified by suffix letter _a, _b etc. # div_mode_* # div_start_time_* # div_end_time_* # div_time_step_* # div_bem_* # div_baq_* # div_csr_* # div_noise_bit_setting_* # div_bpd_* # div_dutycycle_* # div_prf* # div_number_of_pulses_* # div_n_bursts_in_flight_* # div_percent_of_BW_* # div_auto_rad_* # div_rip_* # div_max_data_rate_* # div_interleave_flag_* # div_interleave_duration_* #----------------------------------------------------------------------------- %-------------------------------- div_mode_a radiometer %note IEB#1 div_start_time_a -510 min div_end_time_a -326 min div_time_step_a 30 min div_bem_a 00100 div_baq_a 5 div_csr_a 6 div_noise_bit_setting_a 4 div_bpd_a 1 s div_dutycycle_a 0.38 div_prf_a 1 KHz div_number_of_pulses_a 8 div_n_bursts_in_flight_a 1 div_percent_of_BW_a 100 div_auto_rad_a on div_rip_a 34 ms div_max_data_rate_a 0.25 div_interleave_flag_a off div_interleave_duration_a 10 min %-------------------------------- div_mode_b radiometer %note IEB#2 div_start_time_b -326 min div_end_time_b -248 min div_time_step_b 5 min div_bem_b 00100 div_baq_b 5 div_csr_b 6 div_noise_bit_setting_b 4 div_bpd_b 1 s div_dutycycle_b 0.38 div_prf_b 1 KHz div_number_of_pulses_b 8 div_n_bursts_in_flight_b 1 div_percent_of_BW_b 100 div_auto_rad_b on div_rip_b 34 ms div_max_data_rate_b 1 div_interleave_flag_b off div_interleave_duration_b 10 min %-------------------------------- div_mode_c scatterometer div_start_time_c -248 min div_end_time_c -246 min div_time_step_c 10 s div_bem_c 00100 div_baq_c 5 div_csr_c 8 div_noise_bit_setting_c 4 div_bpd_c 1 s div_dutycycle_c 0.70 div_prf_c 1200 Hz div_number_of_pulses_c 80 div_n_bursts_in_flight_c 1 div_percent_of_BW_c 0 div_auto_rad_c on div_rip_c 34 ms div_max_data_rate_c 90 div_interleave_flag_c off div_interleave_duration_c 90 s %-------------------------------- div_mode_d scatterometer div_start_time_d -246 min div_end_time_d -240 min div_time_step_d 16 s div_bem_d 00100 div_baq_d 5 div_csr_d 0 div_noise_bit_setting_d 4 div_bpd_d 1 s div_dutycycle_d 0.70 div_prf_d 4000 Hz div_number_of_pulses_d 200 div_n_bursts_in_flight_d 2 div_percent_of_BW_d 0 div_auto_rad_d on div_rip_d 34 ms div_max_data_rate_d 200 div_interleave_flag_d off div_interleave_duration_d 10 min %-------------------------------- div_mode_e radiometer div_start_time_e -240 min div_end_time_e 140 min div_time_step_e 30 min div_bem_e 00100 div_baq_e 5 div_csr_e 6 div_noise_bit_setting_e 4 div_bpd_e 4 s div_dutycycle_e 0.38 div_prf_e 1 KHz div_number_of_pulses_e 8 div_n_bursts_in_flight_e 1 div_percent_of_BW_e 100 div_auto_rad_e on div_rip_e 34 ms div_max_data_rate_e 0.25 div_interleave_flag_e off div_interleave_duration_e 10 min %-------------------------------- div_mode_f scatterometer div_start_time_f 140 min div_end_time_f 144.0 min div_time_step_f 16 s div_bem_f 00100 div_baq_f 5 div_csr_f 0 div_noise_bit_setting_f 4 div_bpd_f 1 s div_dutycycle_f 0.70 div_prf_f 4000 Hz div_number_of_pulses_f 120 div_n_bursts_in_flight_f 2 div_percent_of_BW_f 100 div_auto_rad_f on div_rip_f 34 ms div_max_data_rate_f 200 div_interleave_flag_f off div_interleave_duration_f 3 min %-------------------------------- div_mode_g scatterometer div_start_time_g 144 min div_end_time_g 150.5 min div_time_step_g 16 s div_bem_g 00100 div_baq_g 5 div_csr_g 0 div_noise_bit_setting_g 4 div_bpd_g 1 s div_dutycycle_g 0.70 div_prf_g 4500 Hz div_number_of_pulses_g 120 div_n_bursts_in_flight_g 2 div_percent_of_BW_g 100 div_auto_rad_g on div_rip_g 34 ms div_max_data_rate_g 200 div_interleave_flag_g off div_interleave_duration_g 10 min %-------------------------------- div_mode_h scatterometer div_start_time_h 150.5 min div_end_time_h 155.5 min div_time_step_h 16 s div_bem_h 00100 div_baq_h 5 div_csr_h 0 div_noise_bit_setting_h 4 div_bpd_h 1 s div_dutycycle_h 0.70 div_prf_h 4000 Hz div_number_of_pulses_h 120 div_n_bursts_in_flight_h 2 div_percent_of_BW_h 0 div_auto_rad_h on div_rip_h 34 ms div_max_data_rate_h 200 div_interleave_flag_h off div_interleave_duration_h 10 min %-------------------------------- div_mode_i radiometer div_start_time_i 155.5 min div_end_time_i 265 min div_time_step_i 15 min div_bem_i 00100 div_baq_i 5 div_csr_i 6 div_noise_bit_setting_i 4 div_bpd_i 4 s div_dutycycle_i 0.38 div_prf_i 1 KHz div_number_of_pulses_i 8 div_n_bursts_in_flight_i 1 div_percent_of_BW_i 100 div_auto_rad_i on div_rip_i 34 ms div_max_data_rate_i 1 div_interleave_flag_i off div_interleave_duration_i 10 min %-------------------------------- div_mode_j radiometer div_start_time_j 265 min div_end_time_j 317 min div_time_step_j 60 min div_bem_j 00100 div_baq_j 5 div_csr_j 6 div_noise_bit_setting_j 4 div_bpd_j 4 s div_dutycycle_j 0.38 div_prf_j 1 KHz div_number_of_pulses_j 8 div_n_bursts_in_flight_j 1 div_percent_of_BW_j 100 div_auto_rad_j on div_rip_j 34 ms div_max_data_rate_j 1 div_interleave_flag_j off div_interleave_duration_j 10 min div_mode_k radiometer div_start_time_k 317 min div_end_time_k 400 min div_time_step_k 30 min div_bem_k 00100 div_baq_k 5 div_csr_k 6 div_noise_bit_setting_k 4 div_bpd_k 4 s div_dutycycle_k 0.38 div_prf_k 1 KHz div_number_of_pulses_k 8 div_n_bursts_in_flight_k 1 div_percent_of_BW_k 100 div_auto_rad_k on div_rip_k 34 ms div_max_data_rate_k 0.5 div_interleave_flag_k off div_interleave_duration_k 10 min #----------------------------------------------------------------------------- # Special Chirp Start Frequency Selection # Make_csf_integer_multiple_of_prf -(this choice is used only for CW wave) If Yes(yes), chirp start frequency will be adjusted to be an integer multiple of prf if possible or minimize fractional part of csf/prf # Min_frequency_of_returned_CW_echo - when Make_csf_integer_multiple_of_prf is enabled, chirp start frequency will be scanned in such a way that echo location in the base band is larger than this value : suggested value -100 KHz # Max_frequency_of_returned_CW_echo - - when Make_csf_integer_multiple_of_prf is enabled, chirp start frequency will be scanned in such a way that echo location in the base band is smaller than this value: suggested value -20 KHz #----------------------------------------------------------------------------- Make_csf_integer_multiple_of_prf no #----------------------------------------------------------------------------- # Parameters needed by dlap_generate # tracking_option - Specifies the general behavior of the spacecraft rotation # about the Y axis during SAR pointing. # Valid values for: tracking_option # target_center - Point -Z at the target spin axis. # If the incidence angle is zero, then this # simply means to point -Z at the target center. # target_isodoppler - Point -Z so as to minimize doppler variation in the # cross-track direction. # target_pitch_bias - Apply a rotation about spacecraft y-axis away from # isodoppler pointing. This option is used to increase # alongtrack coverage during Titan tour # target_contiguous_coverage - Point -Z so as to fan the 5 beams # perpendicular to the projected # motion of the 5 beams. # incidence_angle_offset - Change incidence angle profile from an ideal one # by adding a constant offset angle # set_azimuth_rotation - Used when tracking_option is set to target_center. # This keyword specifies the azimuth offset to use. # set_sc_z_rotation - Used when tracking_option is set to target_isodoppler # This keyword specifies an additional rotation w.r.t # sc z_axis after isodoppler location is set. # angle_profile_option - Specifies the form of the incidence angle # profile to use # Valid values for: angle_profile_option # constant_incidence_angle - Use same incidence angle # throughout IVD interval # polynomial_fit - Use a polynomial profile fitted in the # least squares sense to points listed in # this config file. # sech_function - Use a hyperbolic secant function to model the incidence # angle variation. This function will fit the c/a incidence # angle, the residual incidence angle at high altitude, # and one mid point value. Special keywords below control # this model. #----------------------------------------------------------------------------- %-------------------------------- tracking_option target_isodoppler set_azimuth_rotation 0 deg set_sc_z_rotation 0 deg angle_profile_option polynomial_fit #----------------------------------------------------------------------------- # When incidence angle profile is constant_incidence_angle # constant_incidence_angle - the constant incidence angle to use when # angle_profile_option is set to # constant_incidence_angle #----------------------------------------------------------------------------- constant_incidence_angle 10 deg #----------------------------------------------------------------------------- # When angle profile option is polynomial_fit, # this incidence angle profile will be used # polynomial_power - the order of polynomial used to fit the incidence angle # profile points # number_of_altitude_incidenceAngle_variations - number of points to fit to a # polynomial profile # altitude* - altitude point to fit to a polynomial profile # incidenceAngle* - incidence angle point to fit to a polynomial profile #----------------------------------------------------------------------------- altitude1 950.001 km altitude11 2398.3 km altitude21 5245.61 km incidenceAngle1 35.1583 deg incidenceAngle11 16.7275 deg incidenceAngle21 12.4807 deg altitude10 2158.04 km incidenceAngle10 17.8359 deg altitude12 2650.72 km incidenceAngle12 16.1645 deg altitude13 2913.55 km incidenceAngle13 16.0165 deg altitude14 3185.33 km incidenceAngle14 16.0312 deg altitude15 3464.79 km incidenceAngle15 15.8233 deg altitude16 3750.88 km incidenceAngle16 14.8667 deg altitude17 4036.83 km incidenceAngle17 14.5654 deg altitude18 4333.05 km incidenceAngle18 13.548 deg altitude19 4633.61 km incidenceAngle19 13.5835 deg altitude2 967.326 km incidenceAngle2 34.7643 deg altitude20 4937.95 km incidenceAngle20 13.5603 deg altitude3 1019.17 km incidenceAngle3 33.6087 deg altitude4 1104.03 km incidenceAngle4 31.7946 deg altitude5 1219.65 km incidenceAngle5 29.4827 deg altitude6 1363.24 km incidenceAngle6 26.8769 deg altitude7 1531.81 km incidenceAngle7 24.2019 deg altitude8 1722.33 km incidenceAngle8 21.6812 deg altitude9 1931.94 km incidenceAngle9 19.511 deg altitude_error 10 km polynomial_power 8 number_of_altitude_incidenceAngle_variations 21 #----------------------------------------------------------------------------- # When incidence angle Incidence angle sech profile parameters # when angle_profile_option is sech_function # angle = angle1 + 2*(angle2-angle1)/{exp( (x-x0)/a) + exp(-(x-x0)/a)} # angle1: residual incidence angle at high altitude # angle2: desired incidence angel at closest approach # a: this parameter will be calculated inside dlap_generate programs # and is used to obtain a desired incidence angle # at a mid altitude between closest approach (about 950 km) and # high altitude (> 4000 km) # this function will try to fit incidence angle at CA, residual incidence angle # at high altitude,and one mid point value between CA and high altitude # incidence_angle_at_lowest_altitude - for sech_function model # mid_altitude - for sech_function model # incidence_angle_at_mid_altitude - for sech_function_model # residual_incidence_angle_at_high_altitude - for sech_function model #----------------------------------------------------------------------------- incidence_angle_at_lowest_altitude 35 deg mid_altitude 2000 km incidence_angle_at_mid_altitude 20 deg residual_incidence_angle_at_high_altitude 0 deg #----------------------------------------------------------------------------- # Parameters needed to image a special targeting area specified by (lat, lon) # target_lat_lon_option - On or Off # target_isodoppler_pointing - On or Off # time_at_closest_range_to_target - Time w.r.t. epoch when sc makes a closest approach to the target (lat lon) # angle_at_closest_range_to_target - Incidence angle at time_at_closed_range_to_target for Isodoppler # start_target_lat_lon_tracking - Start time for tracking target_lat_lon before sc approaches targeted positin # end_target_lat_lon_tracking - End time for tracking target_lat_lon after sc passes targeted position # target_latitude - Used when tracking_option is set to target_isodopper_lat_lon # target_longitude - Used when tracking_option is se to target_isodoppler_lat_lon # off_centered_beam_time_lag - Time lag between beam3 and off-centered beam #----------------------------------------------------------------------------- target_lat_lon_option Off time_at_closest_range_to_target -157.763 s angle_at_closest_range_to_target 0.645888 rad start_target_lat_lon_tracking -1 min end_target_lat_lon_tracking 1 min target_latitude -70 deg target_longitude 0 deg #----------------------------------------------------------------------------- # Parameters needed by ieb_param_generate # Time parameter will use start_time_ieb and end_time_ieb defined in # Time Specification # Some fixed parameters: long term duty cycle < 0.07 # ieb_file - Specifies ieb file containing time tagged slow/fast fields # start_time_ieb - If present, used to create ieb file # end_time_ieb - If present, used to create ieb file # time_step_ieb - If present, used to create ieb file # min_bpd # prf_profile_option - Specifies the form of the prf profile to use # Valid values for: prf_profile_option # constant_prf - Use same prf through IEB interval # polynomial_fit - Use a polynomial profile fitted in the least squares # senses to points listed in this config file # lookup_table - Not implemented yet #----------------------------------------------------------------------------- ieb_file /home/ras/dat/tour/s01/ph_000_2/comm/ph2_psiv_rmss_040413.ieb start_time_ieb -400 min end_time_ieb 400 min time_step_ieb 1 s prf_profile_option polynomial_fit #----------------------------------------------------------------------------- # When prf_profile_option is constant_prf, this value will be used # constant_prf_value - the constant prf value to use when prf profile # option is set to constant_prf #----------------------------------------------------------------------------- constant_prf_value 5000 Hz #----------------------------------------------------------------------------- # PRF profile to be used when prf_profile_option is polynomial_fit # time_prf_polynomial_power - the order of polynomial used to fit the the # prf profile points # number_of_time_prf_variations - number of points to fit to a polynomial # profile # time_prf* - time for prf # prf* - prf point to fit to a polynomial profile #----------------------------------------------------------------------------- time_prf1 -0 min time_prf11 -10 min time_prf21 -20 min prf1 5478.26 Hz prf11 4282.93 Hz prf21 2589.74 Hz time_prf10 -9 min prf10 4465.27 Hz time_prf12 -11 min prf12 4082.35 Hz time_prf13 -12 min prf13 3836.42 Hz time_prf14 -13 min prf14 3535.71 Hz time_prf15 -14 min prf15 3295.45 Hz time_prf16 -15 min prf16 3159.26 Hz time_prf17 -16 min prf17 2911.95 Hz time_prf18 -17 min prf18 2862.82 Hz time_prf19 -18 min prf19 2718.17 Hz time_prf2 -1 min prf2 5414.63 Hz time_prf20 -19 min prf20 2606.87 Hz time_prf3 -2 min prf3 5290.62 Hz time_prf4 -3 min prf4 5186.57 Hz time_prf5 -4 min prf5 5135.25 Hz time_prf6 -5 min prf6 5047.75 Hz time_prf7 -6 min prf7 4869.19 Hz time_prf8 -7 min prf8 4734.58 Hz time_prf9 -8 min prf9 4740 Hz time_prf_polynomial_power 4 number_of_time_prf_variations 21 #----------------------------------------------------------------------------- # dutycyle and altitude values # dutycycle_profile_option - Specifies the form of the dutycycle profile # to be used # Valid values for: dutycycle_profile_option # constant_dutycycle - Use constant dutycycle value in radar parameter block # polynomial_fit - Use a polymonial profile in the least squares sense # to points listed in this config file # It is very unlikely that we are going to use this option #----------------------------------------------------------------------------- dutycycle_profile_option constant_dutycycle #----------------------------------------------------------------------------- # Altitude-dependent dutycycle setup # when dutycycle profile option is polynomial_fit # alt_dutycycle_polynomial_power - the order of polynomial used to fit the # dutycycle profile points # number_of_altitude_dutycycle_variations - number of points to fit to # to a polynomial profile # alt_dutycycle1 - altitude point to fit a polynomial profile # dutycycle1 - dutycycle point to fit a polynomial profile # alt_dutycycle2 - altitude point to fit a polynomial profile # dutycycle2 - dutycycle point to fit a polynomial profile # alt_dutycycle3 - altitude point to fit a polynomial profile # dutycycle3 - dutycycle point to fit a polynomial profile # alt_dutycycle4 - altitude point to fit a polynomial profile # dutycycle4 - dutycycle point to fit a polynomial profile # alt_dutycycle5 - altitude point to fit a polynomial profile # dutycycle5 - dutycycle point to fit a polynomial profile #----------------------------------------------------------------------------- alt_dutycycle_polynomial_power 2 number_of_altitude_dutycycle_variations 3 alt_dutycycle1 1000 km dutycycle1 0.6 alt_dutycycle2 2000 km dutycycle2 0.65 alt_dutycycle3 4000 km dutycycle3 0.70 #----------------------------------------------------------------------------- # Parameters needed to set attenuator for scatterometer(ALTL) mode # cal_gaindB_altl - gain setting when calibration was performed # cal_radar_buffer_std_deviation_altl - standard deviation of radar buffer output (8-8 bits) # squared_deviation_of_system_noise_input_at_ALTL - measured squared deviation of 8-8 straight radar buffer data with the system noise and ALTL bandwidth # squared_deviation_of_system_noise_input_at_ALTH - measured squared deviation of 8-8 straight radar buffer data with the system noise and ALTH bandwidth # squared_deviation_of_system_noise_input_at_SARL - measured squared deviation of 8-8 straight radar buffer data with the system noise and SARL bandwidth # squared_deviation_of_system_noise_input_at_SARH - measured squared deviation of 8-8 straight radar buffer data with the system noise and SARH bandwidth #----------------------------------------------------------------------------- cal_gaindB_altl 8 cal_radar_buffer_std_deviation_altl 20.3 squared_deviation_of_system_noise_input_at_ALTL 1.70e18 s/J squared_deviation_of_system_noise_input_at_ALTH 1.70e18 s/J squared_deviation_of_system_noise_input_at_SARL 1.70e18 s/J squared_deviation_of_system_noise_input_at_SARH 1.70e18 s/J #----------------------------------------------------------------------------- # Antenna pattern configuration # beam_pattern_source - specifies how the beam pattern will be determined # Valid values for: beam_pattern_source # file - Read beam patterns from files specifed by subsequent keywords # sinc_model - Compute beam patterns from a sinc model using parameters # specified in subsequent keywords. # beam_azi_1 - Beam 1 azimuth beamwidth # beam_azi_2 - Beam 2 azimuth beamwidth # beam_azi_3 - Beam 3 azimuth beamwidth # beam_azi_4 - Beam 4 azimuth beamwidth # beam_azi_5 - Beam 5 azimuth beamwidth # beam_elev_1 - Beam 1 elevation beamwidth # beam_elev_2 - Beam 2 elevation beamwidth # beam_elev_3 - Beam 3 elevation beamwidth # beam_elev_4 - Beam 4 elevation beamwidth # beam_elev_5 - Beam 5 elevation beamwidth # beam_maxdB_gain1 - Beam 1 maximum gain (dB) # beam_maxdB_gain2 - Beam 2 maximum gain (dB) # beam_maxdB_gain3 - Beam 3 maximum gain (dB) # beam_maxdB_gain4 - Beam 4 maximum gain (dB) # beam_maxdB_gain5 - Beam 5 maximum gain (dB) # beam_mindB_gain - Beam gain value reported for out of range angles # beam_pattern_directory - full path to the directory containing beam patterns # beam_1_pattern_file - name of file containing pattern data for beam 1 # beam_2_pattern_file - name of file containing pattern data for beam 2 # beam_3_pattern_file - name of file containing pattern data for beam 3 # beam_4_pattern_file - name of file containing pattern data for beam 4 # beam_5_pattern_file - name of file containing pattern data for beam 5 #----------------------------------------------------------------------------- beam_pattern_source file beam_azi_1 0.35 deg beam_azi_2 0.35 deg beam_azi_3 0.35 deg beam_azi_4 0.35 deg beam_azi_5 0.35 deg beam_elev_1 1.35 deg beam_elev_2 1.35 deg beam_elev_3 0.35 deg beam_elev_4 1.35 deg beam_elev_5 1.35 deg beam_maxdB_gain1 44.2 beam_maxdB_gain2 44.2 beam_maxdB_gain3 50.7 beam_maxdB_gain4 44.2 beam_maxdB_gain5 44.2 beam_mindB_gain 20.0 beam_1_pattern_file /home/ras/beam_patterns/beam1.042402.dat beam_2_pattern_file /home/ras/beam_patterns/beam2.042402.dat beam_3_pattern_file /home/ras/beam_patterns/beam3.042402.dat beam_4_pattern_file /home/ras/beam_patterns/beam4.042402.dat beam_5_pattern_file /home/ras/beam_patterns/beam5.042402.dat #----------------------------------------------------------------------------- # Back scattering model specification # Muhleman_backscatt_model_k1 - Muhleman model back scattering coefficient # Muhleman_backscatt_model_k2 - Muhleman model back scattering coefficient #----------------------------------------------------------------------------- Muhleman_backscatt_model_k1 0.0188 Muhleman_backscatt_model_k2 0.111 #----------------------------------------------------------------------------- # Parameters to be used by amb_geom_cal # time_step_sar - If present, used to run SAR simulation # start_time_sar - If present, used to run SAR simulation # end_time_sar - If present, used to run SAR simulation #----------------------------------------------------------------------------- time_step_sar 1 min start_time_sar -14 min end_time_sar 14 min #----------------------------------------------------------------------------- # Parameters to set up 4 ambiguity patches near the imaged area # number_of_dop_bins - Used by performance_cal , set number of dop bins inside # the process window # number_of_range_bins - Used by performance_cal, set number of range bins # inside the process window # number_of_dop_patches - Used by performance_cal, set number of dop patches # separated by prf from the process window # number_of_range_patches - Used by performance_cal, set number of range patches # separated by c * pri/2 from the process window #----------------------------------------------------------------------------- number_of_dop_bins 20 number_of_range_bins 20 #----------------------------------------------------------------------------- # Parameters to set up a global range-doppler grid # To calculate radar geometry factors based on range and doppler grids, # we need to set ranges of range and doppler # delta_doppler = +-2 * max_prf # delta_range = +- 2* (c * max_pri(=1/min_prf))/2 # then, frequency and range resolutions are determined by grid size N # frequency resolution of grid cells: 2* 2 * max_prf/grid # range resolution of grid cells: 2* 2 * (c * max_pri(1/min_prf)/2)/grid # max_prf and min_prf # Number_of_range_doppler_grid - Used by amb_geom_cal to set up global grid # whose range/doppler extents are determined by # ambiguity_search_max_prf -Used by amb_geom_cal to set extent of doppler axis # + - max_prf w.r.t. boresight doppler shift # ambiguity_search_min_prf - Used by amb_geom_cal to set extent of range axis # + - c *max_prf(/min_prf)/2 w.r.t. boresight range # calculate_mirror_ambiguity - Used by amb_geom_cal to calculate radar echo # from mirror location that has the same range/doppler # as the target location # Valid values for: calculate_mirror_ambiguity # Yes - calculate radar return echo from mirror location # No - do not consider radar return echo from mirror location #----------------------------------------------------------------------------- Number_of_range_doppler_grid 200 ambiguity_search_max_prf 6.0 KHz ambiguity_search_min_prf 2.0 KHz calculate_mirror_ambiguity No #----------------------------------------------------------------------------- # Parameters to be used by amb_param_scan # pulse_bandwidth_ratio # usable_area_search_max_prf - Set maximum prf # usable_area_search_min_prf - Set minimum prf # usable_area_number_of_prf_steps - Used by amb_param_scan, search usable area # using prf values from min_prf to max_prf # at an interval of # (max_prf - min_prf)/number_of_prf_steps # usable_area_search_max_pulsegate - Set maximum pulsegate # usable_area_search_min_pulsegate - Set minimum pulsegate # usable_area_number_of_pulsegate_steps - Used by amb_param_scan, search usable # area using pulsegate values # from min_pulsegate to max_pulsegate # at an interval of # (max_pulsegate - min_pulsegate)/number_of_pulsegate_steps #----------------------------------------------------------------------------- pulse_bandwidth_ratio 0.8 usable_area_search_max_prf 6.0 KHz usable_area_search_min_prf 2.0 KHz usable_area_number_of_prf_steps 41 usable_area_search_max_pulsegate 50 km usable_area_search_min_pulsegate 20 km usable_area_number_of_pulsegate_steps 6 #----------------------------------------------------------------------------- # Requirements for a pixel to be "usable" # signal_to_amb_ratiodB - Usable area should have a signal to amb ratio > + 14 dB # noise_equivalent_sigma0dB - Usable area should have a sigma0 < - 10 dB # min_oneway_gaindB_wrt_peak - Usable area should have a gain > -5 dB #----------------------------------------------------------------------------- signal_to_amb_ratiodB 14 noise_equivalent_sigma0dB -10 min_oneway_gaindB_wrt_peak -5 #----------------------------------------------------------------------------- # Radar Parameters # Pt - Transmitted power (46.2 W) # Tsys - System noise temperature (1000 K) # dutycycle_per_burst - long term dutycycle (< 7 %) # constant_dutycycle_value - constant dutycycle value to be used # carrier_frequency - Ku band frequency (13.78 GHz) # stalo_frequency - stable local oscillator frequency (10 MHz) #----------------------------------------------------------------------------- Pt 46.2 W Tsys 886 K dutycycle_per_burst 0.069 constant_dutycycle_value 0.7 carrier_frequency 13.78 GHz #----------------------------------------------------------------------------- # Point Target Sim Radar Parameters for CONFIG parameter source mode # ADC_SAMPLE_RATE - ADC sampling rate for Point Target Simulator # ANTENNA_IMPEDANCE - No longer needed because SAR_CAL_COEFF should include this # ATTENUATOR_LOSS1 - Attenuator setting for beams 1,2 in dB # ATTENUATOR_LOSS3 - Attenuator setting for beam 3 in dB # ATTENUATOR_LOSS4 - Attenuator setting for beam 4 and 5 in dB # BAQ_MODE - Mode used in Baq simulation # BEAM_ORDER_1 - first beam to enable # BEAM_ORDER_2 - second beam to enable # BEAM_ORDER_3 - third beam to enable # BEAM_ORDER_4 - fourth beam to enable # BEAM_ORDER_5 - fifth beam to enable # CHIRP_RATE - Chirp rate used in simulation # INTRA_BURST_DUTY_CYCLE - Pulse Duty Cycle (i.e., 0.70) # PRF - Pulse Repetition Frequency # RECEIVER_BANDWIDTH - Bandwidth of anti-aliasing filter # RECEIVER_GAIN - No longer needed because SAR_CAL_COEFF should include this # RX_WINDOW_EXTRA_PRI - Receive window pad (TRO) used in simulation # in units of PRI # SYSTEM_LOSS - No longer needed because SAR_CAL_COEFF should include this # TOTAL_DUTY_CYCLE - Burst duty cycle (i.e., 0.07) #----------------------------------------------------------------------------- ADC_SAMPLE_RATE 2.0 MHz ATTENUATOR_LOSS1 0 ATTENUATOR_LOSS3 0 ATTENUATOR_LOSS4 0 BAQ_MODE 0 BEAM_ORDER_1 3 BEAM_ORDER_2 3 BEAM_ORDER_3 3 BEAM_ORDER_4 3 BEAM_ORDER_5 3 CHIRP_RATE 5000 MHz/s INTRA_BURST_DUTY_CYCLE 0.70 PRF 6493.5 Hz RECEIVER_BANDWIDTH 0.117 MHz RX_WINDOW_EXTRA_PRI 2 TOTAL_DUTY_CYCLE 0.07 #----------------------------------------------------------------------------- # PTS Radar Parameters needed by IEB and CONFIG mode # BURST_PERIOD - Burst period used in CONFIG mode or in IEB if USE_CONFIG_BPD=1 # FILTER_START_FREQ_OFFSET - Offset of start of anti-aliasing filter # w.r.t -ADC/2, Needed for old SAR processor ' # (l1b_l1i). # SAR_CAL_COEFF - Estimated conversion factor between receive power and sample # number 6.25e19 1/W. Also used by SAR processor. # TRANSMIT_POWER - 46.2 W (should use Pt instead) # UPDOWN_FREQUENCY_SHIFT - Shift of return echo from baseband # due to down convert -10.0 MHz #----------------------------------------------------------------------------- BURST_PERIOD 1 s #----------------------------------------------------------------------------- # PTS Options (Booleans) # COMPUTE_ECHO_AMPLITUDE - 1:= radar equation is employed, 0:= amplitude=1 # IDEAL_GAIN_SETTING - 1:= gain is set to fill ADC, 0:= IEB or CONFIG value used # IDEAL_TRACKING_ON - 1:= Boresight is centered in time and freq, 0: IEB or CONFIG params # SIMULATE_BAQ - 1/0 = ON/OFF # SIMULATE_QUANTIZATION - 1/0 = ON/OFF # SIMULATE_THERMAL_NOISE - 1/0 = ON/OFF # USE_CONFIG_BPD - 1:= Use BURST_PERIOD from config file # even if IEB mode enabled # ASSUME_FILTER_CENTERED - 1:= Do not use FILTER_START_FREQ_OFFSET, assume # anti-aliasing filter is centered in Nyquist usable # bandwidth for each mode # USE_RANDOM_PHASE_SHIFT - 1:= Applies a random phase shift (height on carrier # frequency scale) to point targets #----------------------------------------------------------------------------- COMPUTE_ECHO_AMPLITUDE 0 IDEAL_GAIN_SETTING 1 IDEAL_TRACKING_ON 0 SIMULATE_BAQ 0 SIMULATE_QUANTIZATION 0 SIMULATE_THERMAL_NOISE 0 USE_CONFIG_BPD 1 #----------------------------------------------------------------------------- # PTS Fidelity/Speed Trade-Off Parameters # MAX_TARGET_ANGLE - Maximum angle between a beam and a point target to # compute an echo # SAMPLE_SKIP - Number of samples to skip between evaluations of doppler, # delay, and echo amplitude. A value of 1 recomputes these # quantities for every sample. #----------------------------------------------------------------------------- MAX_TARGET_ANGLE 30 deg SAMPLE_SKIP 100 #----------------------------------------------------------------------------- # PTS point target specification # TARGET_TYPE - Method for specifying point target positions # Target Types 0 and 1 specify fixed positions on the ground which # are viewed by multiple beams and bursts. # 0:= Lat/Lon specification: target specified by its ground coordinates. # Latitude, longitude, and amplitude are specified for each target. # 1:= Altitude/Beam Position Specification: each target is specified by a # location in a particular beam frame, when the spacecraft is # at a given altitude. Inbound/Outbound is also needed to # complete the position specification. Amplitude is specified for each # target. # Types 2 and 3 specify locations within a beam pattern for # each burst and beam. The locations are fixed within the # duration of a burst but vary from burst to burst. Each beam # only sees those point targets meant for it. # 2:= Beam Position Specification: beam number, azimuth, elevation # and amplitude, are specified for each point target. # 3:= Beam Extrema Specification: A a two-way gain value G is specified. # 5 point targets are automatically determined for each of the 5 beams # for a total of 25 targets. Targets occur at the two-way boresights # and at the four 0 elevation and 0 azimuth locations on the G gain # contour in the two-way antenna pattern for each beam. # 4:= Grid of point targets in azimuth and elevation # 5:= Grid of point targets in latitude and longitude # TARGET - Target body name (i.e., TITAN) should use "target" instead (disabled) # NUM_TARGETS - Number of Point Targets, ignored for TARGET_TYPE=3,4,5 # POINT_TARGET_AMPLITUDE1 - Amplitude of First Point Target # (used by all targets for TARGET_TYPE=3,4,5) # POINT_TARGET_AMPLITUDE2 - Amplitude of Second Point Target # (units are area i.e, km km) # POINT_TARGET_AMPLITUDE3 - # POINT_TARGET_AMPLITUDE4 - # POINT_TARGET_AMPLITUDE5 - # POINT_TARGET_LAT1 - Latitude for first point target (TARGET_TYPE=0) # POINT_TARGET_LAT2 - Latitude for second point target # POINT_TARGET_LAT3 - # POINT_TARGET_LAT4 - # POINT_TARGET_LAT5 - # POINT_TARGET_LON1 - Longitude for first point target (TARGET_TYPE=0) # POINT_TARGET_LON2 - Longitude for second point target (TARGET_TYPE=0) # POINT_TARGET_LON3 - # POINT_TARGET_LON4 - # POINT_TARGET_LON5 - # POINT_TARGET_INBOUND1 - Inbound/Outbound (1/0) switch for first Point Target # (TARGET_TYPE=1) # POINT_TARGET_INBOUND2 - Inbound/Outbound (1/0) switch for second Point Target # POINT_TARGET_INBOUND3 - # POINT_TARGET_INBOUND4 - # POINT_TARGET_INBOUND5 - # POINT_TARGET_SC_ALT1 - S/C Altitude for first point target (TARGET_TYPE=1) # POINT_TARGET_SC_ALT2 - S/C Altitude for second point target (TARGET_TYPE=1) # POINT_TARGET_SC_ALT3 - # POINT_TARGET_SC_ALT4 - # POINT_TARGET_SC_ALT5 - # POINT_TARGET_AZIMUTH1 - Azimuth of First Point Target (TARGET_TYPE=1,2) # POINT_TARGET_AZIMUTH2 - Azimuth of Second Point Target # POINT_TARGET_AZIMUTH3 - # POINT_TARGET_AZIMUTH4 - # POINT_TARGET_AZIMUTH5 - # POINT_TARGET_BEAM1 - Beam of First Point Target (TARGET_TYPE=1,2) # POINT_TARGET_BEAM2 - Beam of Second Point Target # POINT_TARGET_BEAM3 - # POINT_TARGET_BEAM4 - # POINT_TARGET_BEAM5 - # POINT_TARGET_ELEVATION1 - Elevation of First Point Target (TARGET_TYPE=1,2) # POINT_TARGET_ELEVATION2 - Elevation of Second Point Target # POINT_TARGET_ELEVATION3 - # POINT_TARGET_ELEVATION4 - # POINT_TARGET_ELEVATION5 - # TARGET_TWO_WAY_GAIN_DB - Two way gain (actually loss is positive) of # antenna pattern contour for use with TARGET_TYPE=3. # (i.e., a value of 6 signifies the contour 6 dB down # from the peak (3 dB one-way). # POINT_TARGET_GRID_NUM_AZIM - # POINT_TARGET_GRID_NUM_ELEV - # POINT_TARGET_GRID_AZIM_RES - # POINT_TARGET_GRID_ELEV_RES - # POINT_TARGET_GRID_MIN_AZIMUTH - # POINT_TARGET_GRID_MIN_ELEVATION - # POINT_TARGET_GRID_NUM_LAT - # POINT_TARGET_GRID_NUM_LON - # POINT_TARGET_GRID_LAT_RES - # POINT_TARGET_GRID_LON_RES - # POINT_TARGET_GRID_MIN_LATITUDE - # POINT_TARGET_GRID_MIN_LONGITUDE - #----------------------------------------------------------------------------- TARGET_TYPE 3 NUM_TARGETS 5 POINT_TARGET_AMPLITUDE1 1.0 km km POINT_TARGET_AMPLITUDE2 1.0 km km POINT_TARGET_AMPLITUDE3 1.0 km km POINT_TARGET_AMPLITUDE4 1.0 km km POINT_TARGET_AMPLITUDE5 1.0 km km POINT_TARGET_LAT1 -67.6923 deg POINT_TARGET_LAT2 -67.7923 deg POINT_TARGET_LAT3 -67.5923 deg POINT_TARGET_LAT4 -67.7923 deg POINT_TARGET_LAT5 -67.5923 deg POINT_TARGET_LON1 -99.9116 deg POINT_TARGET_LON2 -100.0116 deg POINT_TARGET_LON3 -100.0116 deg POINT_TARGET_LON4 -99.8116 deg POINT_TARGET_LON5 -99.8116 deg POINT_TARGET_INBOUND1 1 POINT_TARGET_SC_ALT1 1200 km POINT_TARGET_AZIMUTH1 0.0 deg POINT_TARGET_AZIMUTH2 0.1 deg POINT_TARGET_AZIMUTH3 0.1 deg POINT_TARGET_AZIMUTH4 -0.1 deg POINT_TARGET_AZIMUTH5 -0.1 deg POINT_TARGET_BEAM1 3 POINT_TARGET_BEAM2 3 POINT_TARGET_BEAM3 3 POINT_TARGET_BEAM4 3 POINT_TARGET_BEAM5 3 POINT_TARGET_ELEVATION1 0.0 deg POINT_TARGET_ELEVATION2 0.1 deg POINT_TARGET_ELEVATION3 -0.1 deg POINT_TARGET_ELEVATION4 0.1 deg POINT_TARGET_ELEVATION5 -0.1 deg TARGET_TWO_WAY_GAIN_DB 10 #----------------------------------------------------------------------------- # PTS Timing parameters # SIM_TIME_CONFIG_METHOD - 0:= obsolete timing method using SIM_END_TIME and # SIM_START_TIME. # 1:= Use Flyby timing set-up # 2:= Use start and end times of IEB file # SIM_END_TIME - UTC YMD Time tag for simulation end time # SIM_START_TIME - UTC YMD Time tag for simulation start time #----------------------------------------------------------------------------- SIM_TIME_CONFIG_METHOD 1 #----------------------------------------------------------------------------- # Special PTS I/O filenames and modes # IEB_FILENAME - File used to input Radar Parameters in IEB mode # PTS_DIAG_FILENAME - Diagnostic MATLAB output .m file, Useful for testing # IEB generation # L1A_A_filename - Active mode preprocessed file name when used as source # of radar parameters. This keyword is distinct from # L1B_A_filename which is the simulator's output file. #----------------------------------------------------------------------------- PTS_DIAG_FILENAME pts_t7_diag.m #----------------------------------------------------------------------------- # DOWNLINK Processing File Setup # egse_filename - Downlinked binary file from spacecrfat # L1B_A_filename - Active mode file name(Scatterometry,Altimetry or SAR) # L1B_P_filename - Passive mode file name(Radiometer) # ras_filename - compressed BAQ threshold and RAW data # burst_ordered_ieblist - bursted ordered ieblist filename # L1I_filename - SAR Processor burst-by-burst output file # t_feed_filename - Filename for external temperature telemetry # E-2507.gph or NONE if not available # t_hga_filename - Filename for external temperature telemetry # E-2505.gph or NONE if not available # t_scwg_filename - Filename for external temperature telemetry # E-2503.gph or NONE if not available # Adjust_TFI_in_units_of_sclk - change TFI (active mode nominal value 1) # zero_range_time_delay - positive delay in generating pulse after # receiving command # Show_sclk_adjust_message - when want to see all sclk correction, set 1 #----------------------------------------------------------------------------- egse_filename /home/ras/dat/tour/s01/ph_000_2/raw/ph2_psiv_rmss_040413_003.12Jun04_2257 L1B_A_filename ph2_run3.lbdr L1B_P_filename ph2_run3.sbdr ras_filename ph2_run3.ras burst_ordered_ieblist ph2_run3_burst_order.ieb L1I_filename x t_feed_filename /home/ras/dat/tour/s01/ph_000_2/raw/anc3/E-2507.gph t_hga_filename /home/ras/dat/tour/s01/ph_000_2/raw/anc3/E-2505.gph t_scwg_filename /home/ras/dat/tour/s01/ph_000_2/raw/anc3/E-2503.gph Adjust_TFI_in_units_of_sclk 1 zero_range_time_delay 9.8e-6 s #----------------------------------------------------------------------------- # Preprocessor Archiving (PDS) Parameters # BODP_PRODUCT_VERSION_ID - Version number of LBDR/SBDR/ABDR product for # PDS archiving # BODP_SOFTWARE_VERSION_ID - Version number of LBDR/SBDR/ABDR product for # PDS archiving # FLYBY_ID - Flyby name used in DESCRIPTION field in PDS label # MISSION_PHASE_NAME - Value for same keyword in PDS label # PRODUCER_FULL_NAME - Value for same keyword in PDS label # CHECK_PDS_STRING_LENGTHS - 1: Check that string values that are being # written to PDS labels conform to maximum # lengths specified by PDS standard. # 0: Disable checking. # If keyword not present, processor will behave # as if it had been set to "1." #----------------------------------------------------------------------------- BODP_PRODUCT_VERSION_ID 01 BODP_SOFTWARE_VERSION_ID V1.0 FLYBY_ID Phoebe_S01 PRODUCER_FULL_NAME Inst_Lead_Charles_Elachi_contact_Bryan_Stiles #----------------------------------------------------------------------------- # SARProc I/O filenames and modes # CHECK_BURST_FILENAME - Filename for output MATLAB .m file if # CHECK_BURST_NO - Number of burst to output debug info from (starts with 1) # DATA_QUALITY_OVERRIDE_FILE - If this keyword is specified a file is used # to override the SAR processor nominal quality # checking for each burst. It can be used to force # the inclusion/exclusion of ranges of bursts. # SAR_PROC_SEGMENT_TYPE - Sets method of restricting sar processor including # FULL:= process all data # TIME_FROM_CLOSEST_APPROACH:= process time interval # SAB_COUNTER:= process sab_counter interval # LATLON:= process spatial region # SINGLE_BEAM_MODE - 1: Only one beam's data is processed # 0: All five beams are processed # SARPROC_BEAM_NUMBER - Beam to process if SINGLE_BEAM_MODE=1 # sar_annotation_file - Name of file to which burst by burst SAR processor # run-time output is directed. # SAR_PROC_AUTO_OVERWRITE_BIDR- 1: Automatically overwrite existing BIDR # output product files. # 0: If any of the BIDR output product files # exist, ask user whether to overwrite them. # Continue only if response is "y" or "Y." # If keyword not present, processor will behave # as if it had been set to "0." #----------------------------------------------------------------------------- CHECK_BURST_FILENAME debug_t7_bws.m CHECK_BURST_NO 1 #----------------------------------------------------------------------------- # SARProc Processing Parameters # DC_NULL_BINS - Size of filter for removing DC (in bins) # RANGE_REF_WINDOW_PARAM - Parameter for adjusting windowing performed # during range compression. Range is (0.0-1.0). # AZIMUTH_REF_WINDOW_PARAM - Parameter for adjusting windowing performed # during azimuth compression. Range is (0.0-1.0). # BIDR_LATLON_PAD_EACH_SIDE - Amount of pad applying to the four sides of # the BIDR image in order to avoid clipping of # data. # BIDR_PIXELS_PER_DEGREE - Resolution of BIDR image (nominally 256) # FULL_USABILITY_CALC_ENABLED - 1 set the processing window using a slow routine # which optimizes ambiguity isolation/window size # GAIN_CUTOFF_ENABLED - 1 enables nominal processing window selection method, # one-way antenna gain cut-off # GAIN_CUTOFF_POLYNOMIAL_ORDER - Order of polynominal in time used to compute # antenna gain cut-off threshold # GAIN_CUTOFF_BEAM_1_POLYNOMIAL_COEFF_* - Coefficients of gain cut-off # polynomial for beam 1. # GAIN_CUTOFF_BEAM_2_POLYNOMIAL_COEFF_* - # GAIN_CUTOFF_BEAM_3_POLYNOMIAL_COEFF_* - # GAIN_CUTOFF_BEAM_4_POLYNOMIAL_COEFF_* - # GAIN_CUTOFF_BEAM_5_POLYNOMIAL_COEFF_* - # INCIDENCE_ANGLE_CORRECTION_MODEL - Name of backscatter model used to produce # incidence angle corrected BIDR backplane # PULSE_SPREADING_IN_PRI - Coarse estimate of pulse spreading on the ground # used to determine size of overlapping window used # in range compression # SARPROC_NUM_LOOKS_REQUIRED - Minimum number of looks required to # produce a valid pixel in the BIDR image. #----------------------------------------------------------------------------- DC_NULL_BINS 0 RANGE_REF_WINDOW_PARAM 0.5 #----------------------------------------------------------------------------- # SARProc Options (Booleans) # PERFORM_SINGLE_BURST_CHECK - 1:= Output a Mfile for a selected burst # USE_HENSLEY_RANGE_COMPRESS - 1:= Use Scott Hensley' range compression method # 0:= Use an obsolete simplified method # USE_UPPER_BAND - 1: Range compress the upper half of the signal spectrum. # 0: Range compress the lower half of the signal spectrum. # So far as I know this should always be 0. # SARPROC_USE_LINEAR_CHIRP - 1: Use a linear chirp for range compression # 0: Use the more exact form of the stepped chirp # which was transmitted # PROC_SAR_MODE_ONLY - 1: Process only SARH or SARL data # 0: Process all data as if it were SAR # STRIP_PROC_ON - 1 turns on geolocation processing # AZIMUTH_RANGE_ORTHOGONALIZATION_ON - 1 turns on range dependent doppler shifting # for use in azimuth compression # AZIMUTH_DERAMP_PROCESSING_ON - 1 turns on deramp processing during azimuth # compression # SAR_CALIBRATION_ON - 1 turns on calibration of SAR data # REMOVE_DOPPLER_PHASE_RAMP - 1 turns on data dependent method for removing # phase ramps from compressed data # SARPROC_OUTPUT_SCATTEROMETER_INFO - 1 turns on an output of a simplified estimate # of the real aperture backscatter to the # LBDR file for debugging purposes. # USE_OBLIQUE_CYLINDRICAL - 1 turns on oblique clyndrical map projection. # USE_SINC_INTERPOLATION - 1:Sinc Interpolation 0:= Nearest neighbor #----------------------------------------------------------------------------- PERFORM_SINGLE_BURST_CHECK 1 USE_UPPER_BAND 0 #----------------------------------------------------------------------------- # GENERATE_GEOMETRY_FILE keywords # intermediate_geometry_file - File containing geometry arrays used to speedup # geometry calculations currently used by sar_proc, # point_target_sim, and l0_l1b. Created by # generate_geometry_file # geometry_time_step - Time step used to create geometry file. #----------------------------------------------------------------------------- intermediate_geometry_file tmp.gf #----------------------------------------------------------------------------- # DEBUGINFO debugging and warning keywords # debug_filename - Filename to write debugging info # debug_routine_name_1 - first routine to debug ... # debug_routine_name_2 - # debug_routine_name_3 - # debug_level_1 - debugging level for first routine # debug_level_2 - # debug_level_3 - # ENABLE_ALL_WARNINGS - turns on/off (1/0) verbose warning messages #----------------------------------------------------------------------------- debug_filename ph3.dbg debug_routine_name_1 main debug_level_1 1 ENABLE_ALL_WARNINGS 1 #----------------------------------------------------------------------------- # doppler_centroid_tracking_tool_yaw_bias - yaw bias angle # doppler_centroid_tracking_tool_pitch_bias - pitch bias angle # doppler_centroid_ckernel - name of ckernel generated by doppler_centroid program # range_doppler_file - range and doppler filename that is output of doppler centroid tracking program #----------------------------------------------------------------------------- doppler_centroid_ckernel /home/ras/dat/naif/ck/04162_04165pa_phoebe_lmb_kpt.bc #----------------------------------------------------------------------------- # Radiometer Processor Parameters # Number_of_targets - Number of targets for cruise or tour sequence # target_1 - Extra target in addition to main target set by target_keyword # cold_sky_Temperature - cold sky temperature # cold_sky_average_time - cold sky calibration time duration # radiometer_system_gain - system gain: N= gain * (Tsys+Tcold) # frontend_loss_dB - Antenna frontend loss (from cruise, 3dB) # min_beam_distance - Distance between limb direction and boresight in units of beam oneway 3dB # radiometer_delta_tau - Parameter for performed radiometer normalization 0 s # radiometer_offset - Parameter for performed radiometer normalization 3550 # noise_diode_delta_tau - noise diode integration time offset # resistive_load_delta_tau - resistive load integration time offset # ND_Rip - Noise Diode Radiometric integration time (used in RMSS) # Max_ND_Rip - Maximum Noise Diode Radiometric integration time when auto rad is on # RL_Rip - Resistive Load Radiometric integration time (used in RMSS) # Max_RL_Rip - Maximum Resistive Load Radiometric integration time when auto rad is on #----------------------------------------------------------------------------- radiometer_delta_tau -1.175 ms radiometer_offset 3550 noise_diode_delta_tau -0.12 ms resistive_load_delta_tau -0.0405 ms ND_Rip 7 ms Max_ND_Rip 12 ms RL_Rip 30 ms Max_RL_Rip 40 ms