The KPLO dictionary contains classes that describe aspects of the Korea Pathfinder Lunar Orbiter mission and related instruments. The KPLO_Parameters class is the container for mission-specific metadata elements. The LUTI_Parameters class is the container for Lunar Terrain Imager A and B specific observation parameters. The SHADOWCAM_Parameters class is the container for ShadowCam-specific observation parameters. This section contains the simpleTypes that provide more constraints than those at the base data type level. The simpleTypes defined here build on the base data types. This is another component of the common dictionary and therefore falls within the common namespace. Difference between the max and min bias 12-bit DN value for the whole image. Difference between the max and min bias 12-bit DN value for channel 0. Difference between the max and min bias 12-bit DN value for channel 1. Difference between the max and min bias 12-bit DN value for channel 2. Difference between the max and min bias 12-bit DN value for channel 3. Difference between the max and min bias 12-bit DN value for channel 4. Difference between the max and min bias 12-bit DN value for channel 5. The ADC bit selection is for the used bit range flag. The value 0 is for bit range 11 ~ 0 and detectable range 0~4095, the value 1 is for bit range 12 ~ 1 and detectable range 0~8190, and the value 2 is for bit range 13 ~ 2 and detectable range 0~16380. ShadowCam companding bterm 1 (See appendix in the ShadowCam archive SIS for detailed companding information) ShadowCam companding bterm 2 (See appendix in the ShadowCam archive SIS for detailed companding information) ShadowCam companding bterm 3 (See appendix in the ShadowCam archive SIS for detailed companding information) ShadowCam companding bterm 4 (See appendix in the ShadowCam archive SIS for detailed companding information) ShadowCam companding bterm 5 (See appendix in the ShadowCam archive SIS for detailed companding information) The CCD direction parameter defines the direction of CCD reading. The value 0 is for the reading direction from 1st pixel to 2048th pixel (default) and the value 1 is from the reading direction from 2048th pixel to 1st pixel. Describes how to interpret the data_quality_id field. LROC-style data quality ID bitmask with minimal differences between ShadowCam and LROC definitions. See data_quality_desc for details. The individual boolean fields (dqi_*) are likely easier to use for new software. The corruption detection algorithm found a strong likelihood of image corruption somewhere in the observation. This is often localized to a small area, leaving most of the image usable. The focal plane temperature was outside of the nominal operational limits. The calibration of the image is likely to not be as good in this case. One or more 1 MiB data blocks are missing from the image. Due to interleaving, this typically results in a pattern of 4 pixels present 4 pixels missing. SPICE was unavailable for this observation. This observation could not be calibrated. One or more 0 DN values are present in the companded 8-bit DN. The spacecraft time of when the image command was executed. Use this time with the SCLK kernel and add the start_time_offset value for the most accurate image start. The UTC time and date at the execution of the image acquisition command. Add the start time offset to this time to get the start of the image data. Use the spacecraft clock version of the time with an SCLK kernel for the most accurate timing. Records if the image was LUTI A or B The analog front end gain for channel 0. See ShadowCam calibration paper for details on the gain correction. The analog front end gain for channel 1. See ShadowCam calibration paper for details on the gain correction. The analog front end gain for channel 2. See ShadowCam calibration paper for details on the gain correction. The analog front end gain for channel 3. See ShadowCam calibration paper for details on the gain correction. The analog front end gain for channel 4. See ShadowCam calibration paper for details on the gain correction. The analog front end gain for channel 4. See ShadowCam calibration paper for details on the gain correction. The number of 1024-line image chunks commanded (includes preroll). The line integration time in milliseconds. The TDI line rate code commanded. The line time in seconds can be computed from the commanded line rate using the expression 50e-9*(12*524+(lr*(38+1)+46)), where lr is thecommanded line rate (0-4095). The TDI line rate in milliseconds, the effective exposure time is multiplied by 32 for the number of TDI stages. Constant time offset for LUTI A or B in seconds. For LUTI, the quality ID represents the error status of the image. 0: No error, 1: CRC error, 2: CRC error + compression/decompression error. The luti target name indicates the name of target areas if it is available. If it is not, it will show NA. The luti target type is for LUTI target type such as MLND (Lunar surface, moon landing candidates), MMMO (man made objects), MCRT (lunar craters), MPIT (lunar pits), CGEO (calibration target for geocal), CDRK (dark), CLIM(lunar limb), LSLT (side slither), CSTA (star image), SERT (special targets for the earth), SPLT (planets), and SMS1 and SMS2 (special lunar surface image). The mission_phase_name attribute provides the mission-defined name of a time period within the mission. The instrument was commanded in test mode, resulting in a gradient rather than image data. The analog front end offset for channel 0. The analog front end offset for channel 1. The analog front end offset for channel 2. The analog front end offset for channel 3. The analog front end offset for channel 4. The analog front end offset for channel 5. The orbit_number attribute identifies the number of the orbital revolution of the spacecraft around the Moon. The pre scan mode selection flag is set by ground command. Default value is 1. The value 0 is for disable of use of pre-scan pixel and the value 1 is to use averaged value of pre-scan pixel and the value 2 is to use constant offset value predefined. The number of image lines dropped to initialize the TDI sensor. Typically, this is a minimum of 256. The UTC time and date at the start of the image acquisition, corresponding to the acquisition of preroll_lines at the given exposure prior to the actual image acquisition. The producer_institution_name attribute identifies a university, research center, NASA center, or other institution associated with the production of a data product. A version specifier to differentiate how the data was processed. Any available commentary on the goal of the observation. This is created at planning time, and specific instrument and spacecraft performance may impact if the resulting image meets the original goal or not. The spacecraft_clock_start_count attribute provides the value of the spacecraft clock at the beginning of a time period of interest. The spacecraft_clock_stop_count attribute provides the value of the spacecraft clock at the beginning of a time period of interest. The time in seconds after the execution time that the first image row started. Use this with execution_spacecraft_time and the KPLO SCLK kernel to get the best available start of the image data. The TDI direction of the sensor (A or B). This must match the flight direction of the spacecraft except for calibration images. The temperature of the ‘A’ sensor adjacent to the focal plane. This sensor is located on the heat strap going to the radiator and is the primary temperature used for calibration. The temperature of the ‘B’ sensor adjacent to the focal plane. This sensor is on the opposite side of the TDI sensor from ‘A’, but is not on the copper strap. The temperature reported on the electronics board adjacent to the FPGA. The temperature reported from the metering structure of the telescope. ShadowCam companding xterm 0 (See appendix in the ShadowCam archive SIS for detailed companding information) ShadowCam companding xterm 1 (See appendix in the ShadowCam archive SIS for detailed companding information) ShadowCam companding xterm 2 (See appendix in the ShadowCam archive SIS for detailed companding information) ShadowCam companding xterm 3 (See appendix in the ShadowCam archive SIS for detailed companding information) ShadowCam companding xterm 4 (See appendix in the ShadowCam archive SIS for detailed companding information)