urn:nasa:pds:cassini-caps-raw:data-anc:anc_201007506 1.0 1.20.0.0 Product_Observational Waite, J. Hunter; Furman, Judith D.; Young, David T.; Crary, Frank A.; Wilson, Robert J. 2023 This file contains Cassini CAPS ancillary data and some spacececraft pointing information acquired at SATURN between 2010-075T06:00:31.000 and 2010-075T11:59:59.000 (orbit 128). 2023-08-18 1.0 This product, ANC_201007506_U3.DAT, was originally released as part of the PDS3 CO-E/J/S/SW-CAPS-2-UNCALIBRATED-V1.1 data set. The metadata have been migrated to PDS4. The data themselves are unchanged. 2010-03-16T06:00:31.000Z 2010-03-16T11:59:59.000Z Observation Geometry Engineering Raw Cassini-Huygens Mission urn:nasa:pds:context:investigation:mission.cassini-huygens data_to_investigation Cassini Orbiter Host urn:nasa:pds:context:instrument_host:spacecraft.co is_instrument_host Cassini Plasma Spectrometer Instrument urn:nasa:pds:context:instrument:caps.co is_instrument Saturn Planet urn:nasa:pds:context:target:planet.saturn data_to_target Equinox Mission 1/1647413093.000 1/1647434661.000 1 urn:nasa:pds:cassini-caps-raw:document:data-desc-raw::1.0 data_to_document CO-E/J/S/SW-CAPS-2-UNCALIBRATED-V1.1:ANC_201007506_U3:ANC_201007506_U3.DAT data_to_raw_source_product 10.17189/1519592 PDS Planetary Plasma Interactions Node This is the first version of this product converted to PDS4. The DOI provided references the PDS3 source data set. ANC_201007506_U3.DAT 2010-10-02T12:10:00.000Z 132300 6cedcd8c2166448d2f5a63456efb16c5 This data file is unmodified from the PDS3 version. 0 675 61 2 196 B_CYCLE_NUMBER 1 1 UnsignedMSB2 2 B cycle number from the start of the day, a value of 65535 indicates no B-cycle data is available 65535 65535 1 A_CYCLE_NUMBER 2 3 UnsignedMSB2 2 A cycle number from the start of day 65535 2732 1 TIME 3 5 IEEE754MSBDouble 8 SECOND Start time of the A cycle, seconds from J2000 (barycentric dynamic time). An A-cycle is the 32 second instrument collection cycle. 10e+09 1.5e+09 -7.1e+07 TIME_SCLK 4 13 UnsignedMSB4 4 SECOND Start time of the A cycle, spacecraft clock 10e+09 3.0e+09 0 SC_SATURN_POS_X 5 17 IEEE754MSBSingle 4 KILOMETER J2000[km]: Saturn-centered Spacecraft X Position 10e+12 9.46e+12 -9.46e+12 SC_SATURN_POS_Y 6 21 IEEE754MSBSingle 4 KILOMETER J2000[km]: Saturn-centered Spacecraft Y Position 10e+12 9.46e+12 -9.46e+12 SC_SATURN_POS_Z 7 25 IEEE754MSBSingle 4 KILOMETER J2000[km]: Saturn-centered Spacecraft Z Position 10e+12 9.46e+12 -9.46e+12 SC_SATURN_VELOCITY_VX 8 29 IEEE754MSBSingle 4 J2000 [km/s]: Relative to Saturn 5e+05 3e+05 -3e+05 SC_SATURN_VELOCITY_VY 9 33 IEEE754MSBSingle 4 J2000 [km/s]: Relative to Saturn 5e+05 3e+05 -3e+05 SC_SATURN_VELOCITY_VZ 10 37 IEEE754MSBSingle 4 J2000 [km/s]: Relative to Saturn 5e+05 3e+05 -3e+05 SC_SUN_POS_X 11 41 IEEE754MSBSingle 4 KILOMETER J2000[km]: Sun-centered Spacecraft X Position. 10e+12 9.46e+12 -9.46e+12 SC_SUN_POS_Y 12 45 IEEE754MSBSingle 4 KILOMETER J2000[km]: Sun-centered Spacecraft Y Position. 10e+12 9.46e+12 -9.46e+12 SC_SUN_POS_Z 13 49 IEEE754MSBSingle 4 KILOMETER J2000[km]: Sun-centered Spacecraft Z Position. 10e+12 9.46e+12 -9.46e+12 SC_SUN_VELOCITY_VX 14 53 IEEE754MSBSingle 4 J2000 [km/s]: Relative to the Sun 5e+05 3e+05 -3e+05 SC_SUN_VELOCITY_VY 15 57 IEEE754MSBSingle 4 J2000 [km/s]: Relative to the Sun 5e+05 3e+05 -3e+05 SC_SUN_VELOCITY_VZ 16 61 IEEE754MSBSingle 4 J2000 [km/s]: Relative to the Sun 5e+05 3e+05 -3e+05 SC_ORIENT_XX 17 65 IEEE754MSBSingle 4 XX component of rotation matrix to J2000 2 1 -1 SC_ORIENT_XY 18 69 IEEE754MSBSingle 4 XY component of rotation matrix to J2000 2 1 -1 SC_ORIENT_XZ 19 73 IEEE754MSBSingle 4 XZ component of rotation matrix to J2000 2 1 -1 SC_ORIENT_YX 20 77 IEEE754MSBSingle 4 YX component of rotation matrix to J2000 2 1 -1 SC_ORIENT_YY 21 81 IEEE754MSBSingle 4 YY component of rotation matrix to J2000 2 1 -1 SC_ORIENT_YZ 22 85 IEEE754MSBSingle 4 YZ component of rotation matrix to J2000 2 1 -1 SC_ORIENT_ZX 23 89 IEEE754MSBSingle 4 ZX component of rotation matrix to J2000 2 1 -1 SC_ORIENT_ZY 24 93 IEEE754MSBSingle 4 ZY component of rotation matrix to J2000 2 1 -1 SC_ORIENT_ZZ 25 97 IEEE754MSBSingle 4 ZZ component of rotation matrix to J2000 2 1 -1 ELS_QUALITY_FLAG 26 101 UnsignedByte 1 Missing data and good/bad checksum 0 = Everything is OK 1 = Missing Data 2 = Bad Checksum 3 = Both Missing Data & Bad Checksum 4,5,6 = Not used 7 = No Data 8 8 0 IBS_QUALITY_FLAG 27 102 UnsignedByte 1 Missing data and good/bad checksum 0 = Everything is OK 1 = Missing Data 2 = Bad Checksum 3 = Both Missing Data & Bad Checksum 4,5,6 = Not used 7 = No Data 8 8 0 ION_QUALITY_FLAG 28 103 UnsignedByte 1 Missing data and good/bad checksum 0 = Everything is OK 1 = Missing Data 2 = Bad Checksum 3 = Both Missing Data & Bad Checksum 4,5,6 = Not used 7 = No Data 8 8 0 TOF_LEF_QUALITY_FLAG 29 104 UnsignedByte 1 Missing data and good/bad checksum 0 = Everything is OK 1 = Missing Data 2 = Bad Checksum 3 = Both Missing Data & Bad Checksum 4,5,6 = Not used 7 = No Data 8 7 0 TOF_ST_QUALITY_FLAG 30 105 UnsignedByte 1 Missing data and good/bad checksum 0 = Everything is OK 1 = Missing Data 2 = Bad Checksum 3 = Both Missing Data & Bad Checksum 4,5,6 = Not used 7 = No Data 8 7 0 LOG_QUALITY_FLAG 31 106 UnsignedByte 1 Missing data and good/bad checksum 0 = Everything is OK 1 = Missing Data 2 = Bad Checksum 3 = Both Missing Data & Bad Checksum 4,5,6 = Not used 7 = No Data 8 7 0 SNG_QUALITY_FLAG 32 107 UnsignedByte 1 Missing data and good/bad checksum 0 = Everything is OK 1 = Missing Data 2 = Bad Checksum 3 = Both Missing Data & Bad Checksum 4,5,6 = Not used 7 = No Data 8 7 0 ACT_QUALITY_FLAG 33 108 UnsignedByte 1 Missing data and good/bad checksum 0 = Everything is OK 1 = Missing Data 2 = Bad Checksum 3 = Both Missing Data & Bad Checksum 4,5,6 = Not used 7 = No Data 8 7 0 32 1 0 109 32 ACT_STATUS_BITS 1 UnsignedByte 1 Actuator Status Bits: 0 = Everything is OK 4 = Hit the Limit Switch at +108 8 = Hit the Limit Switch at -108 16 = Data Not Available TLM_VERSION 35 141 UnsignedByte 1 Telemetry mode version number 255 255 0 FSW_MAJOR_VERSION 36 142 UnsignedByte 1 Flight software major version number. To build the full flight software version: Major.SubMajor.Minor.SubMinor For example: 3.1.0.2 255 255 0 FSW_SUBMAJOR_VERSION 37 143 UnsignedByte 1 Flight software sub-major version number. To build the full flight software version: Major.SubMajor.Minor.SubMinor For example: 3.1.0.2 255 255 0 FSW_MINOR_VERSION 38 144 UnsignedByte 1 Flight software minor version number. To build the full flight software version: Major.SubMajor.Minor.SubMinor For example: 3.1.0.2 255 255 0 FSW_SUBMINOR_VERSION 39 145 UnsignedByte 1 Flight software sub-minor version number. To build the full flight software version: Major.SubMajor.Minor.SubMinor For example: 3.1.0.2 255 255 0 POINTING_TYPE 40 146 UnsignedByte 1 Describes the type of pointing we have: 0 = no pointing available 1 = pointing based on predicts 2 = pointing based on reconstructs. 0 2 0 TELEMETRY_MODE 41 147 UnsignedByte 1 Logical telemetry rate and mode: 1 = 250 bps 2 = 500 bps 4 = 1 kbps 8 = 2 kbps 16 = 4 kbps 32 = 8 kbps 64 = 16 kbps 130 = 500 bps solar wind 132 = 1 kbps solar wind 136 = 2 kbps solar wind 255 255 1 IBS_SWEEP_TABLE_NUMBER 42 148 UnsignedByte 1 IBS sweep table and index table numbers: Upper 4 bits are the IBS index table Lower 4 bits are the IBS sweep table number Fill: 0xFF 255 255 0 3 1 0 149 6 DATA_IBS_BKGD 1 UnsignedMSB2 2 COUNTS IBS background counts in fans 1 through 3. Fill is 0xFFFF IBS_STARTING_ENERGY 44 155 UnsignedMSB2 2 IBS starting energy step number. Fill is 0xFFFF 65535 65535 1 IBS_SUBCYCLE 45 157 UnsignedByte 1 IBS subcycle counter. Fill is 0xFF 255 7 0 IBS_COMPRESSION_RATIO 46 158 UnsignedByte 1 ratio: (uncompressed length/compressed length). Calculated on ground from info in the IBS header and rounded down to the nearest integer. Fill is 0 0 255 1 IBS_PEAK_FAN 47 159 UnsignedByte 1 Fan containing the IBS peak. Fill is 4 4 4 1 IBS_PEAK_ACYCLE 48 160 UnsignedByte 1 A cycle number containing the IBS peak Fill is 9 160 160 1 IBS_PEAK_SWEEP 49 161 UnsignedByte 1 IBS peak energy sweep. Fill is 0 0 16 1 IBS_PEAK_STEP 50 162 UnsignedByte 1 IBS peak energy step. Fill is 0 0 255 1 IBS_THRESHOLD_RL 51 163 UnsignedMSB2 2 IBS Run length compression threshold. Fill is 0xFFFF 65535 65535 0 IMS_SWEEP_TABLE_NUMBER 52 165 UnsignedByte 1 IMS sweep table number. Number 240 will be reserved as a fill value 240 255 0 TDC_SINGLE_SELECT 53 166 UnsignedByte 1 TDC Singles Selection: Value: Single 13 Single 14 0 Start CFD Stop CFD 1 Acquisition Error Deadtimes 2 Single TOF's Double TOF's 3 Data Strobes Resets 255 3 0 IMS_LOGICALS_SELECTION 54 167 UnsignedMSB2 2 TDC logicals selection: Bits 15-13: IMS Logical 1 Bits 12-10: IMS Logical 2 Bits 9-7: IMS Logical 3 Bits 6-4: IMS Logical 4 Bits 3-0: Unused Logical selection decoder: 0 = Unused 1 = LEF Stop 2 = ST Stop 3 = Timeouts 4 = Total Events (As used in SAM deadtime correction) 5 = Logical 13 6 = Logical 14 7 = Unused NOTE: Logical 13 and 14 are set with 82TDC_ENG_SING. See OBJECT name TDC_SINGLE_SELECT. 65535 65535 4096 SAM_CPU2_STATUS_FLAGS 55 169 UnsignedByte 1 Bit 7 = CPU2/SAM mode change 6 = Background data 5 = Ion deadtime compensation 4 = SAM LEF enable 3 = SAM molecule enable 2 = SW/HW binning 1-0 = HW binning LUT index SAM_ION_SELECTION_INDEX 56 170 UnsignedByte 1 SAM Ion selection index number SAM_ION_GROUP_TABLE 57 171 UnsignedMSB2 2 SAM group table ID number 65535 65535 0 ELS_MCP_ADJ 58 173 IEEE754MSBSingle 4 VOLTS ELS High Voltage Adjust. converted using: V = DAC * 58.73. Where DAC is the digital to analog value transmitted by the instrument in housekeeping. -1.0 3700.0 0.0 IBS_CEM_DAC 59 177 IEEE754MSBSingle 4 VOLTS IBS CEM (channel-electron multiplier) High Voltage. Converted using: V = DAC * (-15.68627451). DAC is the digital to analog value transmitted by the instrument in housekeeping. 1.0 1.0 -4000.0 HVU1_RET_DAC 60 181 IEEE754MSBSingle 4 KILOVOLTS HVU1 (high voltage unit 1) Retarding High Voltage, converted using: kV = DAC * 0.0627451 Where DAC is the digital to analog value transmitted by the instrument in housekeeping. -1.0 16.0 0.0 HVU1_ACC_DAC 61 185 IEEE754MSBSingle 4 KILOVOLTS HVU1 (high voltage unit 1) Accelerating High Voltage, converted using: kV = DAC * -0.0627451 Where DAC is the digital to analog value transmitted by the instrument in housekeeping. 1.0 1.0 -16.0 HVU2_ST_DAC 62 189 IEEE754MSBSingle 4 VOLTS HVU2 (high voltage unit 2) Straight Through MCP (multichannel plate), converted using: V = DAC * -14.1176 Where DAC is the digital to analog value transmitted by the instrument in housekeeping. 1.0 1.0 -3600.0 HVU2_LEF_DAC 63 193 IEEE754MSBSingle 4 VOLTS HVU2 (high voltage unit 2) Linear Electric Field MCP (multichannel plate), converted using: V = DAC * -9.4118 Where DAC is the digital to analog value transmitted by the instrument in housekeeping. 1.0 1.0 -2400.0