European Space Agency Research and Science Support Department Planetary Missions Division | | | | | | |SMART1-SPEDE | | | |To Planetary Science Archive Interface | |Control Document | | | | | |S1-SPE-ICD-3005 | | | |Version 2.4 | | | |5 June 2006 | | | ______________________________ Prepared by: Maria Genzer, FMI _______________________________ Approved by: Walter Schmidt, FMI _______________________________ Approved by: Anssi Mälkki, FMI Distribution List |Recipient |Organisation |Recipient | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | Change Log |Date |Sections Changed |Reasons for Change | |8.4.2004 / v.1.1 |All | | |22.4.2004 / v.1.2 |All |Moved to PSA EAICD | | | |template | |17.6.2004 / v2.0 |All |Added level 2 data | | | |descriptions | | | |Some changes in | | | |level 1 descriptions| | | | | |18.5.2005 / v2.1 |All |Wave measurement | | | |descriptions added. | | | |Some editorial | | | |changes. | |26.9.2005 / v2.2 |Chapters 2.4.9, 3.2.2, |S/C position and | | |4.n.n |attitude information| | | |added to Level 2 | | | |datasets. | | | |S/C clock format | | | |changed. | |26.1.2006 / v2.3 |Chapters 4.n.n |More attitude | | | |information in Level| | | |2 data products. | | | |More keywords in all| | | |data product labels.| |5.6.2006 / v2.4 |Chapters 3.1.1, 3.3, |Added dataset and | | |3.4.4.9,4.2 |release information,| | | |pvv version, typo | | | |correction, new | | | |dataset naming | | | | | | | | | | | | | TBD ITEMS |Section |Description | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | Table Of Contents 1 Introduction 4 1.1 Purpose and Scope 4 1.2 Archiving Authorities 4 1.3 Contents 4 1.4 Intended Readership 4 1.5 Applicable and Reference Documents 4 1.6 Relationships to Other Interfaces 4 1.7 Acronyms and Abbreviations 5 1.8 Contact Names and Addresses 5 2 Overview of Instrument Design, Data Handling Process and Product Generation 6 2.1 Science and Technology Objectives 6 2.2 Instrument description 7 2.3 Data Handling Process 10 2.3.1 Level 1b products (raw data) 10 2.3.2 Level 2 products (calibrated data) 11 2.4 Overview of Data Products 12 2.4.1 Pre-Flight Data Products 12 2.4.2 Sub-System Tests 12 2.4.3 Instrument Calibrations 12 2.4.4 Other Files written during Calibration 13 2.4.5 In-Flight Data Products 13 2.4.6 Software 13 2.4.6.1 Data processing software 13 2.4.6.2 Scientific analysis software 13 2.4.7 Documentation 13 2.4.8 Derived and other Data Products 13 2.4.9 Ancillary Data Usage 14 2.4.9.1 SPEDE ancillary data 14 2.4.9.2 Spacecraft auxiliary data 14 3 Archive Format and Content 15 3.1 Format and Conventions 15 3.1.1 Deliveries and Archive Volume Format 15 3.1.2 Data Set ID Formation 16 3.1.3 Data Directory Naming Convention 16 3.1.4 Filenaming Convention 17 3.1.4.1 Level 1b - raw data 17 3.1.4.2 Level 2 - calibrated data 17 3.2 Standards Used in Data Product Generation 18 3.2.1 PDS Standards 18 3.2.2 Time Standards 18 3.2.3 Reference Systems 18 3.2.4 Other Applicable Standards 18 3.3 Data Validation 18 3.4 Content 18 3.4.1 Volume Set 18 3.4.2 Data Set 18 3.4.3 Directories 19 3.4.3.1 Root Directory 19 3.4.3.2 Calibration Directory 19 3.4.3.3 Catalog Directory 19 3.4.3.4 Index Directory 19 3.4.3.5 Browse Directory and Browse Files 19 3.4.3.6 Geometry Directory 19 3.4.3.7 Software Directory 19 3.4.3.8 Gazetter Directory 19 3.4.3.9 Label Directory 19 3.4.3.10 Document Directory 20 3.4.3.11 Extras Directory 20 3.4.3.12 Data Directory 20 4 Detailed Interface Specifications 21 4.1 Structure and Organization Overview 21 4.2 Data Sets, Definition and Content 21 4.3 Data Product Design 21 4.3.1 Raw probe current (Langmuir) and probe voltage (S/C potential) data product 21 4.3.1.1 General description 21 4.3.1.2 Label example 22 4.3.2 Raw wave electric field data 26 4.3.2.1 General description 26 4.3.2.2 Label example 27 4.3.3 Raw configuration table dump (ancillary data) 29 4.3.3.1 General description 29 4.3.3.2 Label example 29 4.3.4 Raw operation parameters (software dumps) product (ancillary data) 35 4.3.4.1 General description 35 4.3.4.2 Label example 36 4.3.5 Calibrated electron/ion flux data product 40 4.3.5.1 General description 40 4.3.5.2 Label example 41 4.3.6 Calibrated plasma data product 46 4.3.6.1 General description 46 4.3.6.2 Label example 46 4.3.7 Calibrated electric field data product 51 4.3.8 Calibrated wave data 51 4.3.8.1 General description 51 4.3.8.2 Label example 52 4.3.9 Calibrated housekeeping data (ancillary product) 57 4.3.9.1 General description 57 4.3.9.2 Label example 58 4.4 Indices - summary tables of data products 61 4.4.1 Level 1b 61 4.4.2 Level 2 64 5 Appendix: Available Software to read PDS files 66 6 Appendix: Example of Directory Listing of Data Set: S1-X-SPEDE-4-REFDR-LEOP-CALIBRATION-V1.0 67 Introduction 1 Purpose and Scope The purpose of this EAICD (Experimenter to (Science) Archive Interface Control Document) is two fold. First it provides users of the SPEDE instrument with a detailed description of the product and a description of how it was generated, including data sources and destinations. Secondly, it is the official interface between the SPEDE instrument team and SMART-1 archiving authority. 2 Archiving Authorities ESA's Planetary Science Archive (PSA). 3 Contents This document describes the data flow of the SPEDE instrument on SMART-1 from the s/c until the insertion into the PSA for ESA. It includes information on how data were processed, formatted, labeled and uniquely identified. The document discusses general naming schemes for data volumes, data sets, data and label files. Standards used to generate the product are explained. Software that may be used to access the product is explained further on. The design of the data set structure and the data product is given. Examples of these are given in the appendix. 4 Intended Readership The staff of the archiving authority (Planetary Science Archive, ESA, RSSD, design team) and any potential user of the SPEDE data. 5 Applicable and Reference Documents [AD-01] Planetary Data System Data Preparation Workbook, February 17, 1995, Version 3.1, JPL, D-7669, Part 1 [AD-02] Planetary Data System Standards Reference, August 1, 2003, Version 3.6, JPL, D-7669, Part 2 [AD-03] SMART-1 Data Processing and Archive Plan, July 7, 2003, Issue 1, Rev. 5 [AD-04] Planetary Science Archieve Experiment Data Release Concept Technical Proposal, SOP-RSSD-TN-015 [RD-01] SPEDE User Manual, S1-SPE-MA-3001 6 Relationships to Other Interfaces TBD 7 Acronyms and Abbreviations APID Application Identification DDS Data Distribution System EP Electric Propulsion GSE Ground Support Equipment MJD2000 Modified Julian Date 2000 LEOP Low Earth Orbit Period PDS Planetary Data System PSA Planetary Science Data Archive SIS Software Interface Specification TBC To Be Confirmed TBD To Be Defined UTC Coordinated Universal Time 8 Contact Names and Addresses Finnish Meteorological Institute Anssi Malkki (PI), Walter Schmidt (Tech. Manager), Maria Genzer (Operations and PDS Archiving) E-mail: firstname.lastname@fmi.fi Tel: + 358 9 19291 Address: Finnish Meteorological Institute Space Research P.O. Box 503 00101 Helsinki, Finland Overview of Instrument Design, Data Handling Process and Product Generation 1 Science and Technology Objectives The SPEDE (Spacecraft Potential, Electron and Dust Experiment) experiment, consisting of two electric sensors and an electronics unit, will measure the electron flux and wave electric fields. The cylindrical sensors are mounted on the tips of two 60-cm booms, located at the +X and -X faces of the spacecraft (see Figure 1.). The sensors are connected to the electronics unit via a single triaxial cable each without any active electronics outside the board; the SPEDE electronics is housed on two electronics boards, located in a box inside the spacecraft body. [pic] Figure 1. Smart-1 and SPEDE booms. The mission of the SPEDE experiment is two-fold: it will monitor - The disturbances (electron flux, wave electric fields, and spacecraft potential variations) induced by the propulsion system, and - The variability of the electron density and wave electric fields during the Earth spiraling and cruise phases and during the Moon phase 1. Monitoring of disturbances produced by the SMART-1 propulsion system Gas releases, most commonly from thrusters used to control the spacecraft velocity and attitude, can disturb observations of some instruments as well as contaminate the spacecraft structure. Because of possible interference effects and spacecraft contamination can be detrimental to sensitive instruments, it is important that the disturbances produced by the thruster operations in the spacecraft environment are monitored. This is especially important for the SMART- 1 mission, for the first time using electrical propulsion on an ESA mission. Charged clouds expanding from the propulsion system may introduce a variety of phenomena when interacting with the ambient plasma and the spacecraft surface. These include - variations in the spacecraft potential and electron flux, - contamination of the spacecraft surfaces for an extended period of time, and - generation of wave electric fields. Especially, large effects in the spacecraft potential can be immediately observed if, for some reason, the exhaust ions are not properly neutralized by the cathode electron emitter. It is also important to gain knowledge of the reactions of the plasma environment to changes in EP engine parameters of operation. 2. Monitoring of electron density in the inner magnetosphere In the first part of the SMART-1 mission, the Earth spiralling phase, the spacecraft will be accelerated by the ion propulsion engine and remain in the inner magnetosphere. In addition to monitoring the effects of the propulsion as described above, the SPEDE observations are used for measuring the distribution of thermal plasma of the plasmasphere whenever the EP is not operating. Particularly the measurements aim at detecting the position of its outer boundary, the plasmapause, usually located at a distance of 3-7 Earth's radii at the equator. As long as the perigee of the orbit is less than 3-4 Re (20 000 km), the plasmapause is crossed twice per orbit. When the perigee is between 20 000 and 40 000 km, the plasmapause is not always encountered, particularly so during magnetic storms, when the plasmasphere becomes smaller in size. 3. Monitoring of plasma density and waves in the Earth's magnetosphere and in the Solar Wind After the perigee of the orbit is raised outside of the plasmasphere boundary (see above), SPEDE observations will concentrate on low-rate monitoring of the magnetospheric and solar wind plasma. These regions have been extensively investigated on earlier missions with plasma instrumentation optimised for tenuous plasmas, and no scientific break-throughs are expected. The measurements will consist of monitoring variations of plasma density by operating the instrument in a constant-bias low-sampling mode. 4. Monitoring of space weathering of the Moon The target of the SMART-1 mission is the Moon, which has no magnetic field and atmosphere. Therefore, it is continuously exposed to the interplanetary space environment. The fast solar wind stream hits the dayside lunar surface and is possibly capable of lifting up small dust grains from the surface. Behind the moon, the solar wind produces a wake that is more tenuous than the solar wind. On lunar orbit, SPEDE observations are used for studying solar wind - moon interaction processes. The uplifted dust particles can be detected as variations in the spacecraft potential, as the particles are ionised when hitting the spacecraft surface. A high sampling rate will be used at the region of the predicted wake boundary, to obtain the best data both for dust impact detection and studies of the plasma density and turbulence at the wake. Optimised modes initiated by time-tagged commands will be used. 2 Instrument description SPEDE is a double-probe plasma instrument, measuring plasma parameters with two cylindrical Langmuir probes. The objectives of SPEDE are to measure 1) variations in the spacecraft potential and electron flux, caused by the electric propulsion, and 2) the variability of the electron density and wave electric fields of the natural plasma during Earth spiraling, cruise, and Moon phases. In addition, SPEDE will provide dust impact detection based on ionisation effects on the spacecraft surface. SPEDE consists of two separate conical metallic sensor areas mounted each at the tip of a 60cm long carbon fiber sensor boom, and an electronics box on the inside of the -X face of the spacecraft. The booms are attached to the centers of the spacecraft's -X and +X face, respectively. Each is a 100 mm long metallic TiN foil glued around another slightly protruding150 mm long TiN foil, which is attached to the boom structure. The outer foil is the sensor area. The inner foil extends 25 mm outside of the probe area at both ends. The potential of the inner foil is kept actively at the sensor area's potential to compensate for capacitive coupling losses (guard). The booms are slightly conical, but the conical shape can be neglected in analysis, and the sensors can be considered cylindrical, with a radius of 12 mm and a length of 100 mm. Due to the short boom length, measurements are strongly affected by photoelectrons from the spacecraft body, which need to be taken account when interpreting the measurements, especially in the electric field (voltage measurement) mode. During thruster operations, it is assumed that the plasma is dominated by charge- exchange ions from thruster outflow, and electrons from the neutralizing cathode, and photoelectron contribution is negligible. SPEDE can operate in two different configurations: In Langmuir Probe (or Probe Current, PC) mode, a relay connects the output of a bias voltage generator via a small series resistor to the sensor. The probe current is measured as voltage drop across the resistor. The range of currents that can be measured is -470 microA to 240 microA with 5 nanoA resolution, positive sign corresponding to current from the probe (electron current with positive bias). Each sensor has its dedicated source for bias voltage, which can be controlled independently. Stabilized reference voltages and buffering amplifiers provide adjustable bias voltages between -13V and +13V with fine- tuning possibilities close to 0V. In Spacecraft Potential (or Probe Voltage, PV) mode the relays connect the sensors via 6MOhm resistors to ground. Voltage variations w.r.t. ground are measured directly before the series resistor. The range of voltages (probe to spacecraft ground) is +/- 3 volts, with 0.2 mV resolution. The wave measurement, when activated, is performed at the end of a measurement sequence. The voltage difference between the two probes is sampled for one second at 10000 samples/s. The resulting data is analysed with on-board software Fast Wavelet Transform routine, with the number of logarithmically spaced frequency bins given in the command parameters. The analog signals from the probes are translated into frequencies using a separate Voltage-to-Frequency-Converter (VFC) for each channel. The measurement frequencies in the range of 150Hz to 150kHz with about 50kHz for 0V (exact values for zero frequency at each bias code are given in the calibration data). Small values (low frequency) correspond to positive voltages and large values to negative voltages. The VFC readings are digitized by either defining a measurement time window inside which the frequency pulses are counted (frequency measurement), or by defining the number of frequency pulses whose total length is measured (pulse length measurement). The on-board 16-MHz clock is used as time reference. The probe data (frequencies) are saved as 20-bit data values in the telemetry. The -X sensor chain includes additionally an 8-channel analog multiplexer, via which housekeeping parameters can be measured: -X and +X bias voltage, -X and +X reference voltage, ground reference, and temperature of electronics as measured inside the +X VFC chip. The data processing part is based on a 16-bit RISC-processor, implemented directly in the same Field-Programmable-Gate-Array (FPGA) as the controller for the analog part. Several alternative software versions and operational configurations are stored in a 0.5MByte EEPROM, a 0.5MByte RAM is used as intermediate data storage. Boot program, memory paging system, watchdog and real-time clock are also implemented inside the FPGA. An independent FPGA controls the low-level communications protocol with the spacecraft. For each data acquisition and sensor the following parameters have to be defined: measurement type (Langmuir mode - current measurement/ Voltage measurement), bias voltage, digitalization principle (frequency / pulse length measurement) and duration of integration (long/short). When data acquisitions are completed for both probes, the software can retrieve the data. Data acquisitions can be defined either by the hardware access telecommand, returning directly a telemetry packet with the results, or under flight software control, where bias start and increment parameters and relative timing are defined in one of the 9 configuration tables. In each case the hardware configuration during each data acquisition is returned together with the measurement result inside the telemetry. SPEDE has 10 operation modes: o Stand-by (0) - Processor is in idle loop, interpreting telecommands, if any. No scientific measurements. This is the only mode where direct hardware control of the instrument is possible. Stand-by mode is entered on power low condition (spacecraft primary voltage < 45 V) or on telecommand. o Housekeeping (1) - default mode. This mode is entered after reset, after automatic end of any other mode, or on telecommand. The housekeeping mode is controlled by configuration table 1. Default configuration is one Langmuir Probe (Probe Current) measurement with fixed bias voltage per minute, 30 measurements in one measurement vector. o Science modes (2-9) - are controlled by related configuration tables 2-9. The instrument behavior depends on the table's contents. Science modes are entered on explicit telecommand. Each of the science modes 2-9 can be configured to run continuously until replaced by another mode, or to stop after a given number of telemetry blocks (measurement repetitions, 1-255), after which the instrument changes automatically to the housekeeping mode. The parameters contained in mode configuration tables 1-9 are given in detail in chapter 4.3.3. 3 Data Handling Process All PDS data products will be prepared at the Finnish Meteorological Institute (see chapter 1.8 for contact information). All data processing levels mentioned in this document are PSA- compliant, as defined in RO-EST-PL-5011. Level 1a SPEDE data will be fetched from the SMART-1 Data Distribution System (DDS) by FMI, where it will be processed to Level 1b, and further to Level 2 products. 1 Level 1b products (raw data) SPEDE science data is transmitted via ESOC ground stations and processed to level 1a by ESOC (processing levels are defined in [AD- 01]). Level 1a data is made available to SPEDE team via FTP server (SMART-1 Data Distribution System (DDS)). SPEDE team fetches level 1a data from the DDS. The telemetry packets are saved into FMI's local database (still in DDS format). Because SMART-1 payload telemetry packets do not have proper PUS headers, the supposed time of packet generation given by the DDS header is actually the time of packet reception on ground. The real time of packet generation is only saved as spacecraft clock value in the beginning of each SPEDE telemetry packet. When SPEDE telemetry packets are saved into local database, the packet generation times in DDS headers are fixed based on the spacecraft clock. Correlations between the spacecraft clock and UTC (the spacecraft clock was reset several times during the mission) are hardcoded into epoch_data.conf file, used by the database generation routine. From the local database, SPEDE data can be retrieved by spacecraft orbit or date. Orbit division is made according to event files provided by ESOC. The first step of SPEDE PDS product generation is to divide data by orbits (science data) or months (ancillary data). This is done automatically. A script fetches data from the local database and produces DDS-formatted files for each orbit (science data) or month (ancillary data). DDS-formatted files are then processed by another script that produces 5 PDS-compliant level 1b data products: . Raw probe current data - SPEDE-PC-RAW (science, Probe Current (Langmuir) mode) . Raw probe voltage data - SPEDE-PV-RAW (science, Probe Voltage (E- field) mode) . Raw wave electric field data - SPEDE-WEF-RAW (science, extracted from TM files also containing probe current or voltage data) . Configuration table dumps (non-science, ancillary data) . Software dumps of operation parameters (non-science, ancillary data) Raw probe current data (Langmuir) and raw probe voltage data (E- field) are divided into product files according to combination of probe (-X = probe 1, +X = probe 2) and measurement vector length. Each combination is stored into its own file. Other products will also be gathered to their own files. One science product file contains measurements from one spacecraft orbit. Configuration table dump and software dump files contain all dumps for one month. Level 1b data are generally to be used only by SPEDE data producers. For other data users, Level 2 data will be provided. 2 Level 2 products (calibrated data) Level 1b science data is further processed and calibrated using look-up tables. Also information about probe shadow status and S/C position is added. This results in 5 (TBC) PDS-compliant level 2 data products: . Calibrated electron/ion flux data (SPEDE-EF-CAL) - originated from Langmuir probe data measured with constant voltage bias . Calibrated plasma data (SPEDE-PD-CAL) - originated from Langmuir probe data measured with variable voltage bias (sweeps) . Calibrated E-field data (SPEDE-EFF-CAL) - originated from Probe Voltage data. Details TBD. . Calibrated wave electric field data (SPEDE-WEF-CAL) - originated from the wave measurements. . Calibrated housekeeping values (ancillary data) Calibrated data is divided into data files by products, probes (separate files for -X and +X), and spacecraft orbits. 4 Overview of Data Products 1 Pre-Flight Data Products N/A 2 Sub-System Tests N/A 3 Instrument Calibrations Level 1b probe current (PC) data is calibrated to physical values using look-up tables, resulting in Level 2 data (EF and PD). The look- up tables contain for both probes (-X and +X): o Physical values (Volts) corresponding to each raw bias control value o Background values corresponding to each raw bias control value o Calibration coefficients a0, a1, a2, a3, used in the polynomial that calculates currents (in Amperes) from frequencies (raw Langmuir measurements). The polynomial is: I(V(b)) = a3*f(b)3 + a2*f(b)2 + a1*f(b) +a0 , where f(b) = Background(b) - Raw measurement(b), b = bias, f = frequency (Hz) (Calibration of Probe voltage (S/C potential) measurements to physical values (Volts) TBD.) There can exist several versions of the lookup tables. The versions used for a particular data product are given in its header as DATA_QUALITY_ID keyword. Calibrated wave power data (WEF) is calculated from the raw wave data with the following formula: P = w2/(2*N3), where w = raw wave value, and N = 2(10-n), n = frequency bin number 0 ... 9. Before calibration to physical values, some of the measurement results obtained with pulse length measurement mode need to be corrected, because the pulse counter sometimes misses the last pulse of a measurement (resulting for example in 19 instead of 20 pulses in short pulse mode). Since the origin and result of this are known, this feature can be corrected during calibration to Level 2 data. If a pulse measurement result is corrected, this is indicated with a 'P' flag as described below. Level 2 data contains status vectors associated with each measurement value. Their purpose is to give an overview of the measurement quality. A science data quality vector contains places for 16 flags. Currently 4 flags are used, the rest are placeholders marked with an underscore (_). Also flag downs are marked with an underscore. The information currently given by a status vector is: o 16th (LS) flag: 0 = the result is checked and found correct 1 = the result is checked and possibly corrected, warnings concerning quality 2 = the result is checked, and found unreliable (no corrections) 9 = the result is unchecked o 15th flag: F = frequency measurement, p = original pulse measurement, P = corrected pulse measurement, _ = not applicable (wave measurements) o 14th flag: 1 = the first measurement in a measurement vector, _ = following measurements o 13th flag: R = the reference voltage was fluctuating during this measurement, _ = the reference voltage was OK (the reference voltage value is obtained from ancillary housekeeping data; fluctuation means that raw voltage value was outside nominal levels of 95-105) A housekeeping data quality vector contains only two places: status check (as 16th flag above), and reference voltage fluctuation (as 13th flag above). Calibration look-up tables and other information necessary for SPEDE raw data calibration are stored in /CALIB directory of the data archive. Bias and background look-up tables are given in file SPEDE_BIAS_CALIB.TAB, and polynomial coefficients in file SPEDE_CURRENT_CALIB.TAB. Note! /CALIB directory is present only in the data archives containing Level 2 data. 4 Other Files written during Calibration N/A 5 In-Flight Data Products All archived SPEDE data products will be in-flight products of level 1b and 2. The products are described in chapter 2.3. Level 1b products shall be used to produce level 2 products, by the FMI team only. Level 2 calibrated data is intended for other users. See also chapter 2.4.9.2 for important information about SPEDE data interpretation! 6 Software 1 Data processing software . A local database for storing all DDS data. Data is added to the database by generate_db routine. This routine also removes any duplicate packets, and fixes telemetry packet generation times in DDS headers by calculating UTC times from spacecraft clock times. . Scripts to divide DDS data into files according to orbits or time slots (for science data), and months (for ancillary data): get_orbit_dds, get_measurement and get_aux. . Another script to generate PDS-compliant level 1b products from the DDS-formatted files already divided by orbit or month: gen_tab.sh. . A script to generate level 2 products from level 1b products: pds2level2all.tcl . Scripts to generate index files: generate_index.sh (level 1b) and generate_2_index.sh (level 2) These scripts are used only by the data producers, and they are not included in PDS deliveries. 2 Scientific analysis software No special software for scientific analysis is included. SPEDE data is in ASCII format and can be plotted for example with any spreadsheet software. 7 Documentation The data archive contains the following documentation: . This EAICD . SPEDE paper describing the instrument 8 Derived and other Data Products See chapter 2.3.2. 9 Ancillary Data Usage 1 SPEDE ancillary data SPEDE measurements are controlled by configuration tables and operation parameters stored in the EEPROM. They can be changed by telecommands. The performance of SPEDE instrument depends on these settings. Whenever a configuration table or an operation parameter is changed, its new value is returned in telemetry. These dumps are provided in Level 1b datasets as software dump and configuration table dump products. These non-science products are archived together with the science data. In Level 2 datasets, calibrated housekeeping values (reference voltages and temperatures) are given as ancillary data records for reference purposes. 2 Spacecraft auxiliary data SPEDE measurement results are affected by the status of the SMART- 1 propulsion system (the Hall thruster), and the spacecraft's position and attitude. The results can only be interpreted if these are known. Level 2 data products contain Information about s/c position and attitude (probe shadow status). The status of the Hall thruster (ON, OFF, power level) is provided by the Smart-1 team in auxiliary data set with DATA_SET_ID = S1-L-ESOC-6-AUXILIARY-DATA- V1.0. The status is given in the file PRODUCT_ID = S1_EP_THRUST_LOG.TAB. This file is located in DATA/THRUST directory of the dataset. SPEDE data users should also fetch this auxiliary data set before interpreting SPEDE results. Archive Format and Content 1 Format and Conventions 1 Deliveries and Archive Volume Format The following dataset releases will be delivered |dataset |release|orbits |dates | |LEOP-CALIBRATION |1 |e3-e14 |2003-09-29 - 2003-10-04 | |EE-EP-MONITORING |1 |e15-e204,e228-e2|2003-10-04 - 2004-04-01 | | | |59 | | |EE-EP-MONITORING |2 |e260-e331 |2004-04-01 - 2004-11-17 | |LP-EP-MONITORING |1 |m1-m235 |2004-11-17 - 2005-03-01 | |LP-EP-MONITORING |2 |m978-m1252 |2005-08-01 - 2005-09-27 | |SOLAR-WIND |1 |e205-e227 |2004-02-01 - 2004-02-25 | |MOON-PLASMA |1 |m236-m977 |2005-03-01 - 2005-08-01 | |MOON-PLASMA |2 |m1253-m1999 |2005-09-27 - 2006-03-01 | |MOON-PLASMA |3 |m2000- |2006-03-01 - | Both the level 1b and level2 data will be produced. The datasets are split to distinct operational environments. On top of that, some of the datasets are divided to releases [SOP-RSSD-TN-015]. With the release concept, new data can be appended to an existing dataset, without repeating the supplementary data. The first dataset, LEOP-CALIBRATION, contains the instrument commissioning in the low Earth orbit. Both EP-MONITORING datasets, Earth escape and Lunar phase contain data, when the thruster has been operated. While the dataset contain orbit data, when thruster is not operated, it's needed to understand the data in the thruster on moments in the same orbit. The releases are separated from the natural operational border or from about 6 month worth of data. Note, that the first dataset contains a hole in time, during which the thruster was not operated and the data is given in a different dataset. The SOLAR-WIND dataset contains data from the Earth orbits, when the thruster is not operated for a long period. The MOON-PLASMA datasets contains data from the Moon orbit, when the thruster is not operated. The releases are splitted from the natural operational border or from about 6 month worth of data. [pic] Figure 2. SPEDE dataset format. 2 Data Set ID Formation Data set ID will be formed according to PDS standards. It will have the following components: . Instrument host: S1 . Target: X (= other) . Instrument: SPEDE . Data processing level number (CODMAC): 2 for level 1b, 4 for level 2 . Product type: EDR for level 1b, REFDR for level 2 . Description = free description of the data set . Version number Example: "S1-X-SPEDE-4-REFDR-LEOP-CALIBRATION-V1.0" 3 Data Directory Naming Convention Directories are named according to PDS standards. DATA directory is divided into subdirectories each containing data products of one month. Format of the directory name are YYYYMM, for example 200310 for October 2003 data, 200311 for November 2003 data, etc. If several datasets are present in one archive, the DATA directory is first divided into subdirectories for datasets, and only those are then divided to monthly subdirectories. 4 Filenaming Convention 1 Level 1b - raw data Probe current and Probe voltage product types: SP_orbitdYYMMDD_x_tp_ll_RAW.TAB, where orbit = spacecraft orbit number, 5 digits d = delimeter, Earth orbit: _, Moon orbit: M YYMMDD = date of orbit start x = sensor number, 1 = -X, 2 = +X tp = product type, PC or PV ll = vector measurement length Wave electric field product type: SP_orbitdYYMMDD_W_WA_ll_RAW.TAB, where orbit, d, YYMMDD, ll as above. Configuration table dump product type (non-science) are named: SP_YYYYMM_CONFIG_RAW.TAB, where YYYY = year, MM = month. Software dump files (non-science) are named: SP_YYYYMM_SWDUMP_RAW.TAB, where YYYY = year, MM = month. 2 Level 2 - calibrated data Electron/ion flux product: SP_orbitdYYMMDD_x_EF_CAL.TAB Plasma data product: SP_orbitdYYMMDD_x_PD_ll_CAL.TAB E-field product: SP_orbitdYYMMDD_x_EFF_CAL.TAB Wave electric field product: SP_orbitdYYMMDD_W_WA_ll_CAL.TAB Housekeeping data (ancillary): SP_orbitdYYMMDD_HK_CAL.TAB In all of the above: orbit = spacecraft orbit number, 5 digits d = delimeter, Earth orbit: _, Moon orbit: M YYMMDD = date of orbit start x = sensor number, 1 = -X, 2 = +X ll = vector measurement length 2 Standards Used in Data Product Generation 1 PDS Standards PDS standard used is 3.6. All data processing levels mentioned in this document are PSA-compliant, as defined in SMART-1 Data Processing and Archive Plan [AD-03]. 2 Time Standards SPEDE data files use two time standards: Coordinated Universal Time (UTC) as ASCII string, and Modified Julian Date 2000 (MJD2000) as real number. MJD2000 counts days and day fractions since Jan 1, 2000. The PDS header files also use S/C clock counts. Their format is 1/0001234567.89123, where the value before the '/' represents the partition number, which is increased by one for each clock reset on the spacecraft, and the rest is seconds and subseconds. 3 Reference Systems 4 Other Applicable Standards 3 Data Validation Formats are checked with the PSA Validation and Verification Tool (PVV 2.6). 4 Content 1 Volume Set 2 Data Set Data sets will be named according to PDS standards. Each component of the name will match the corresponding component of the data set ID. Data set name components are: . Instrument host: SMART1 . Target: PLASMA . Instrument name: SPEDE . Data processing level . Product type . Description . Version number Example: "SMART1 PLASMA SPEDE 4 REFDR LEOP-CALIBRATION V1.0" 3 Directories 1 Root Directory General archive description: AAREADME.TXT, VOLDESC.CAT 2 Calibration Directory /CALIB directory contains information needed for SPEDE calibration (transfer from level 1b to level 2 data). The calibration files are look-up tables, as defined in chapter 2.4.3: . SPEDE_BIAS_CALIB.TAB contains physical values (Volts) and background values for each raw bias value . SPEDE_CURRENT_CALIB.TAB contains coefficients for the polynomial used to calculate currents from raw Langmuir measurements (frequencies). /CALIB directory is included only in data archives containing level 2 data. 3 Catalog Directory /CATALOG directory contains high-level catalog templates for SPEDE: o INST.CAT - Instrument description o INSTHOST.CAT - Instrument host description, provided by the Project o MISSION.CAT - Mission description, provided by the Project o DATASET.CAT - Data set description o SOFT.CAT - Software description (empty for SPEDE archives) o REFERENCES.CAT - References (empty for SPEDE archives) o RELEASE.CAT - Release information 4 Index Directory /INDEX directory contains index tables for SPEDE science data: o INDEX.TAB - Tabular summary of all data files. o INDEX.LBL - Detached label for the index file. 5 Browse Directory and Browse Files N/A 6 Geometry Directory N/A 7 Software Directory N/A 8 Gazetter Directory N/A 9 Label Directory /LABEL directory contains format container files (*.FMT) used by SPEDE labels: In level 1b archives: o SPEDE_HEADER.FMT - Data objects definitions common to all products. o SPEDE_CONFIGURATION.FMT - Data objects definitions for configuration table dumps. o SPEDE_SWDUMP.FMT - Data object definitions for software dumps (operational parameters). o SPEDE_MEASURE_NN.FMT - Data objects definitions for measurement data with different vector lengths. NN = 20,30,40. In level 2 archives: o SPEDE_FLUX.FMT - Data object definitions for electron/ion flux product. o SPEDE_PLASMA_NN.FMT - Data object definitions for plasma (sweep) data product. NN= 20,40 o SPEDE_WAVE.FMT - Data object definitions for wave measurement data product. o SPEDE_HK.FMT - Data object definitions for housekeeping data product. The labels themselves are always attached to the data files, so they do not appear in /LABEL directory. Only necessary format containers are included in data sets. For example, if some data set does not include any software dumps, the corresponding format container will also not be included. 10 Document Directory /DOCUMENT directory contains SPEDE documentation: o SPEDESIS.ASC - This document in ASCII format o SPEDESIS.PDF - This document in PDF format o SPEDESISxxx.JPG - Figures of this document in JPG format. o SPEDEPAPER.ASC - SPEDE paper in ASCII format o SPEDEPAPER.PDF - SPEDE paper in PDF format o Detached labels: o SPEDESIS.LBL o SPEDEPAPER.LBL 11 Extras Directory N/A 12 Data Directory /DATA directory contains subdirectories by month of data acquisition. For naming convention, see chapter 3.1.3. Data products are stored in monthly subdirectories. If a product spans over two months, it is stored in the directory of the earlier month. Detailed Interface Specifications 1 Structure and Organization Overview /DATA directory will be divided into monthly subdirectories YYYYMM. The data products will be stored in these subdirectories. If some data product will span over two months, it will be stored in the subdirectory of the first month. All SPEDE data products will be stored as TABLEs in ASCII format. The products will use attached labels. Parts of the labels will be stored in format files (*.FMT). The *.FMT files will be archived in the /LABEL directory. 2 Data Sets, Definition and Content SPEDE data products will be divided into data sets as follows: . commissioning and ionospheric calibrations (LEOP, Earth orbits 3- 14) . nominal EP monitoring, Earth escape phase (Earth orbits 15-204, 228-331) . nominal EP monitoring, Lunar phase (Moon orbits 1-235, 978-1252) . Monitoring of natural plasma with EP off (Earth orbits 205-227) . Moon science (Moon orbits 236-977, 1253- ) There will be own data sets for data with different processing level. Currently it is envisaged that for each mission phase defined above there will be two data sets supplied: one with level 1b data and one with level 2 data. 3 Data Product Design 1 Raw probe current (Langmuir) and probe voltage (S/C potential) data product 1 General description Each measurement (row) of raw Probe current and Probe voltage data has the following components: . Spacecraft time in UTC, ASCII format (time of the first measurement point) . Spacecraft time in MJD2000 . TM packet APID . TM packet sequence counter . Spacecraft clock in seconds . Spacecraft clock sub-seconds (1/256 sec) . Probe -X reference voltage . Probe +X reference voltage . Temperature at +X . Ground reference voltage . Instrument mode number (1-9) . Delta time between two measurement steps (stepping time) . Probe: "1" = -X, "2" = +X, "W" = wave measurement . Measurement vector length . Bias type: Langmuir - Probe current ("I") or Probe voltage ("V") . Measurement type: frequency ("F") or pulse ("P") . Integration constant: integration time for frequency measurement, number of pulses for pulse measurement . Repeated for each measurement point (number given by vector length): - Bias value - Measurement value 2 Label example PDS_VERSION_ID = PDS3 LABEL_REVISION_NOTE = "2006-01-03, Jouni Ryno, FMI, initial release" RELEASE_ID = 0001 REVISION_ID = 0000 /* FILE FORMAT */ RECORD_TYPE = FIXED_LENGTH RECORD_BYTES = 335 FILE_RECORDS = 431 LABEL_RECORDS = 9 /* POINTER TO DATA OBJECT */ ^TABLE = 10 /* GENERAL DATA DESCRIPTION PARAMETERS */ FILE_NAME = "SP_00189M050218_2_PV_20_RAW.TAB" DATA_SET_ID = "S1-X-SPEDE-2-EDR-EP-MONITORING2-V1.0" DATA_SET_NAME = "SMART1 PLASMA SPEDE 2 EDR EP MONITORING2 V1.0" PRODUCT_ID = "SP_00189M050218_2_PV_20_RAW.TAB" PRODUCT_TYPE = "EDR" PRODUCT_CREATION_TIME = 2006-01-25 PROCESSING_LEVEL_ID = 2 PROCESSING_LEVEL_DESC = "Edited data, corrected for telemetry errors" MISSION_ID = "SMART1" MISSION_NAME = "SMALL MISSIONS FOR ADVANCED RESEARCH AND TECHNOLOGY" MISSION_PHASE_NAME = "EARTH ESCAPE PHASE" ORBIT_NUMBER = "N/A" INSTRUMENT_HOST_ID = "S1" INSTRUMENT_HOST_NAME = "SMALL MISSIONS FOR ADVANCED RESEARCH AND TECHNOLOGY" TARGET_TYPE = "PLASMA ENVIRONMENT" TARGET_NAME = "PLASMA" TARGET_DESC = "Spacecraft potential and surrounding plasma" START_TIME = 2005-02-18T06:43:34 STOP_TIME = 2005-02-18T12:58:15 SPACECRAFT_CLOCK_START_COUNT = "8/0030993731.23928" SPACECRAFT_CLOCK_STOP_COUNT = "8/0031016212.12239" PRODUCER_ID = "FMI" PRODUCER_INSTITUTION_NAME = "Finnish Meteorological Institute" PRODUCER_FULL_NAME = "Dr. Anssi Malkki" INSTRUMENT_ID = "SPEDE" INSTRUMENT_NAME = "SPACECRAFT POTENTIAL, ELECTRON AND DUST EXPERIMENT" INSTRUMENT_MODE_ID = "PV" INSTRUMENT_MODE_DESC = "Probe voltage (S/C potential)" DATA_QUALITY_ID = -1 DATA_QUALITY_DESC = "-1=not checked" INSTRUMENT_TYPE = "PLASMA INSTRUMENT" OBJECT = TABLE INTERCHANGE_FORMAT = ASCII ROWS = 431 ROW_BYTES = 333 ROW_SUFFIX_BYTES = 2 COLUMNS = 19 NAME = SPEDE_MEASUREMENT DESCRIPTION = "SPEDE header and measurement" ^STRUCTURE = "SPEDE_HEADER.FMT" ^STRUCTURE = "SPEDE_MEASURE_20.FMT" END_OBJECT = TABLE END SPEDE_HEADER.FMT: OBJECT = COLUMN COLUMN_NUMBER = 1 NAME = DATE DATA_TYPE = CHARACTER START_BYTE = 1 BYTES = 23 DESCRIPTION = "S/C clock date in UTC" FORMAT = A23 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 2 NAME = JULIAN_DATE DATA_TYPE = ASCII_REAL START_BYTE = 25 BYTES = 14 DESCRIPTION = "S/C clock date in Modified Julian Date 2000" FORMAT = "F14.8" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 3 NAME = APID DATA_TYPE = ASCII_INTEGER START_BYTE = 40 BYTES = 4 DESCRIPTION = "S/C application identification" FORMAT = I4 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 4 NAME = SEQ_CNT DATA_TYPE = ASCII_INTEGER START_BYTE = 45 BYTES = 5 DESCRIPTION = "SPEDE packet sequence count" FORMAT = I5 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 5 NAME = SC_TIME DATA_TYPE = ASCII_INTEGER START_BYTE = 51 BYTES = 10 DESCRIPTION = "S/C clock in seconds" FORMAT = I10 UNIT = "s" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 6 NAME = SC_SUBTIME DATA_TYPE = ASCII_INTEGER START_BYTE = 62 BYTES = 3 DESCRIPTION = "S/C clock in 1/256 subseconds" FORMAT = I3 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 7 NAME = REF_VOLT_MINUS_X DATA_TYPE = ASCII_INTEGER START_BYTE = 66 BYTES = 3 DESCRIPTION = "2.5V -X reference voltage, data value with frequency measurement using 4ms integration" FORMAT = I3 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 8 NAME = REF_VOLT_PLUS_X DATA_TYPE = ASCII_INTEGER START_BYTE = 70 BYTES = 3 DESCRIPTION = "2.5V +X reference voltage, data value with frequency measurement using 4ms integration" FORMAT = I3 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 9 NAME = TEMP_PLUS_X DATA_TYPE = ASCII_INTEGER START_BYTE = 74 BYTES = 3 DESCRIPTION = "Temperature of +X channel electronics, data value with frequency measurement using 20ms integration -1280, resolution 3C degree" FORMAT = I3 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 10 NAME = GROUND DATA_TYPE = ASCII_INTEGER START_BYTE = 78 BYTES = 3 DESCRIPTION = "Ground reference voltage, data value with frequency measurement using 4ms integration" FORMAT = I3 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 11 NAME = MODE DATA_TYPE = ASCII_INTEGER START_BYTE = 82 BYTES = 5 DESCRIPTION = "Number of configuration table defining the measurement for this data set" FORMAT = I5 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 12 NAME = TIME_INC DATA_TYPE = ASCII_INTEGER START_BYTE = 88 BYTES = 6 DESCRIPTION = "Time difference between start of integration periods of subsequent measurements in units of 1/256 sec" FORMAT = I6 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 13 NAME = PROBE DATA_TYPE = CHARACTER START_BYTE = 96 BYTES = 1 DESCRIPTION = "Sensor probe used for the data set: 1=probe on -X face of spacecraft, 2=probe on +X face of spacecraft, W=wave measurement using the potential difference between both probes" FORMAT = A1 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 14 NAME = LENGTH DATA_TYPE = ASCII_INTEGER START_BYTE = 99 BYTES = 2 DESCRIPTION = " Length of measurement bias and data vectors" FORMAT = I2 END_OBJECT = COLUMN SPEDE_MEASURE_20.FMT OBJECT = COLUMN NAME = BIAS_TYPE DATA_TYPE = CHARACTER START_BYTE = 2 BYTES = 1 DESCRIPTION = "I for Langmuir (current measurement), V for voltage measurement" FORMAT = A1 END_OBJECT = COLUMN OBJECT = COLUMN NAME = MEASUREMENT_TYPE DATA_TYPE = CHARACTER START_BYTE = 6 BYTES = 1 DESCRIPTION = "F = frequency measurement, P = pulse length measurement" FORMAT = A1 END_OBJECT = COLUMN OBJECT = COLUMN NAME = INTEGRATION_CONSTANT DATA_TYPE = ASCII_INTEGER START_BYTE = 9 BYTES = 4 DESCRIPTION = "For frequency measurement, integration time in ms. For pulse measurement, number of VFC pulses used." FORMAT = I4 END_OBJECT = COLUMN OBJECT = COLUMN NAME = BIAS_VECTOR DATA_TYPE = ASCII_INTEGER START_BYTE = 14 BYTES = 79 ITEM_BYTES = 3 ITEMS = 20 ITEM_OFFSET = 4 DESCRIPTION = "Measurement bias" FORMAT = I3 END_OBJECT = COLUMN OBJECT = COLUMN NAME = MEASUREMENT_VECTOR DATA_TYPE = ASCII_INTEGER START_BYTE = 94 BYTES = 139 ITEM_BYTES = 6 ITEMS = 20 ITEM_OFFSET = 7 DESCRIPTION = "Measurement value" FORMAT = I6 END_OBJECT = COLUMN 2 Raw wave electric field data 1 General description Each measurement vector (row) has the following components: . Spacecraft time in UTC, ASCII format (time of the first measurement point) . Spacecraft time in MJD2000 . TM packet APID . TM packet sequence counter . Spacecraft clock in seconds . Spacecraft clock sub-seconds (1/256 sec) . Probe -X reference voltage . Probe +X reference voltage . Temperature at +X . Ground reference voltage . Instrument mode number (1-9) . Delta time between two measurement steps (stepping time) . Probe: "W" = wave measurement . Measurement vector length . Wave data bias for -X . Wave data bias for +X . Repeated for each measurement point (number given by vector length): o Wavelet coefficient 2 Label example PDS_VERSION_ID = PDS3 LABEL_REVISION_NOTE = "2006-01-03, Jouni Ryno, FMI, initial release" RELEASE_ID = 0001 REVISION_ID = 0000 /* FILE FORMAT */ RECORD_TYPE = FIXED_LENGTH RECORD_BYTES = 180 FILE_RECORDS = 144 LABEL_RECORDS = 24 /* POINTER TO DATA OBJECT */ ^TABLE = 25 /* GENERAL DATA DESCRIPTION PARAMETERS */ FILE_NAME = "SP_00235M050228_W_WA_10_RAW.TAB" DATA_SET_ID = "S1-X-SPEDE-2-EDR-EP-MONITORING2-V1.0" DATA_SET_NAME = "SMART1 PLASMA SPEDE 2 EDR EP MONITORING2 V1.0" PRODUCT_ID = "SP_00235M050228_W_WA_10_RAW.TAB" PRODUCT_TYPE = "EDR" PRODUCT_CREATION_TIME = 2006-01-25 PROCESSING_LEVEL_ID = 2 PROCESSING_LEVEL_DESC = "Edited data, corrected for telemetry errors" MISSION_ID = "SMART1" MISSION_NAME = "SMALL MISSIONS FOR ADVANCED RESEARCH AND TECHNOLOGY" MISSION_PHASE_NAME = "EARTH ESCAPE PHASE" ORBIT_NUMBER = "N/A" INSTRUMENT_HOST_ID = "S1" INSTRUMENT_HOST_NAME = "SMALL MISSIONS FOR ADVANCED RESEARCH AND TECHNOLOGY" TARGET_TYPE = "PLASMA ENVIRONMENT" TARGET_NAME = "PLASMA" TARGET_DESC = "Spacecraft potential and surrounding plasma" START_TIME = 2005-02-28T21:46:40 STOP_TIME = 2005-02-28T23:22:00 SPACECRAFT_CLOCK_START_COUNT = "8/0031911897.24132" SPACECRAFT_CLOCK_STOP_COUNT = "8/0031917617.12239" PRODUCER_ID = "FMI" PRODUCER_INSTITUTION_NAME = "Finnish Meteorological Institute" PRODUCER_FULL_NAME = "Dr. Anssi Malkki" INSTRUMENT_ID = "SPEDE" INSTRUMENT_NAME = "SPACECRAFT POTENTIAL, ELECTRON AND DUST EXPERIMENT" INSTRUMENT_MODE_ID = "WA" INSTRUMENT_MODE_DESC = "Wave measurement (Voltage mode)" DATA_QUALITY_ID = -1 DATA_QUALITY_DESC = "-1=not checked" INSTRUMENT_TYPE = "PLASMA INSTRUMENT" OBJECT = TABLE INTERCHANGE_FORMAT = ASCII ROWS = 144 ROW_BYTES = 178 ROW_SUFFIX_BYTES = 2 COLUMNS = 17 NAME = SPEDE_MEASUREMENT OBJECT = CONTAINER NAME = SPEDE_HEADER_DATA START_BYTE = 1 BYTES = 100 REPETITIONS = 1 DESCRIPTION = "SPEDE header" ^STRUCTURE = "SPEDE_HEADER.FMT" END_OBJECT = CONTAINER OBJECT = COLUMN COLUMN_NUMBER = 15 NAME = MINUS_X_BIAS DATA_TYPE = ASCII_INTEGER START_BYTE = 102 BYTES = 3 DESCRIPTION = "Wave data -X bias" FORMAT = I3 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 16 NAME = PLUS_X_BIAS DATA_TYPE = ASCII_INTEGER START_BYTE = 106 BYTES = 3 DESCRIPTION = "Wave data +X bias" FORMAT = I3 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 17 NAME = WAVE_COEFFICIENT_VECTOR DATA_TYPE = ASCII_INTEGER START_BYTE = 110 BYTES = 69 ITEM_BYTES = 6 ITEMS = 10 ITEM_OFFSET = 7 DESCRIPTION = "Wavelet coefficiens vector" FORMAT = I6 END_OBJECT = COLUMN END_OBJECT = TABLE END 3 Raw configuration table dump (ancillary data) 1 General description Each table dump (row) has the following components: . Spacecraft time in UTC, ASCII format (time of the dump) . Spacecraft time in MJD2000 . TM packet APID . TM packet sequence counter . Spacecraft clock in seconds . Spacecraft clock sub-seconds (1/256 sec) . Table number . Table contents - Bias voltage start value for probe -X - Bias increment for probe -X - Number of bias steps for probe -X - Bias voltage start value for probe +X - Bias increment for probe +X - Number of bias steps for probe +X - Control byte for probe -X (in HEX) - Control byte for probe +X (in HEX) - Delta time between two measurement steps (stepping time) - Delta time between measurement repetitions (repetition time) - Number of measurement repetitions: 1-255, or 0 = infinite - Number of frequencies for wave measurement - Plasma wave measurement bias for probe +X - Plasma wave measurement bias for probe -X 2 Label example PDS_VERSION_ID = PDS3 LABEL_REVISION_NOTE = "2006-01-03, Jouni Ryno, FMI, initial release" RELEASE_ID = 0001 REVISION_ID = 0000 /* FILE FORMAT */ RECORD_TYPE = FIXED_LENGTH RECORD_BYTES = 133 FILE_RECORDS = 5 LABEL_RECORDS = 19 /* POINTER TO DATA OBJECT */ ^TABLE = 20 /* GENERAL DATA DESCRIPTION PARAMETERS */ FILE_NAME = "SP_200310_CONFIG_RAW.TAB" DATA_SET_ID = "S1-X-SPEDE-2-EDR-LEOP-CALIBRATION-V1.0" DATA_SET_NAME = "SMART1 PLASMA SPEDE 2 EDR LEOP CALIBRATION V1.0" PRODUCT_ID = "SP_200310_CONFIG_RAW.TAB" PRODUCT_TYPE = "ANCDR" PRODUCT_CREATION_TIME = 2006-01-25 PROCESSING_LEVEL_ID = 2 PROCESSING_LEVEL_DESC = "Edited data, corrected for telemetry errors" MISSION_ID = "SMART1" MISSION_NAME = "SMALL MISSIONS FOR ADVANCED RESEARCH AND TECHNOLOGY" MISSION_PHASE_NAME = "EARTH ESCAPE PHASE" ORBIT_NUMBER = "N/A" INSTRUMENT_HOST_ID = "S1" INSTRUMENT_HOST_NAME = "SMALL MISSIONS FOR ADVANCED RESEARCH AND TECHNOLOGY" TARGET_TYPE = "PLASMA ENVIRONMENT" TARGET_NAME = "PLASMA" TARGET_DESC = "Spacecraft potential and surrounding plasma" START_TIME = 2003-10-01T16:50:14 STOP_TIME = 2003-10-02T19:20:35 SPACECRAFT_CLOCK_START_COUNT = "4/0000010419.54255" SPACECRAFT_CLOCK_STOP_COUNT = "4/0000105840.54167" PRODUCER_ID = "FMI" PRODUCER_INSTITUTION_NAME = "Finnish Meteorological Institute" PRODUCER_FULL_NAME = "Dr. Anssi Malkki" INSTRUMENT_ID = "SPEDE" INSTRUMENT_NAME = "SPACECRAFT POTENTIAL, ELECTRON AND DUST EXPERIMENT" INSTRUMENT_MODE_ID = "N/A" INSTRUMENT_MODE_DESC = "N/A" DATA_QUALITY_ID = -1 DATA_QUALITY_DESC = "-1=not checked" INSTRUMENT_TYPE = "PLASMA INSTRUMENT" OBJECT = TABLE INTERCHANGE_FORMAT = ASCII ROWS = 5 ROW_BYTES = 131 ROW_SUFFIX_BYTES = 2 COLUMNS = 21 NAME = SPEDE_CONFIGURATION ^STRUCTURE = "SPEDE_CONFIGURATION.FMT" END_OBJECT = TABLE END SPEDE_CONFIGURATION.FMT: OBJECT = COLUMN COLUMN_NUMBER = 1 NAME = DATE DATA_TYPE = CHARACTER START_BYTE = 1 BYTES = 23 DESCRIPTION = "S/C clock date in UTC" FORMAT = A22 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 2 NAME = JULIAN_DATE DATA_TYPE = ASCII_REAL START_BYTE = 25 BYTES = 14 DESCRIPTION = "S/C clock date in Modified Julian Date 2000" FORMAT = "F14.8" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 3 NAME = APID DATA_TYPE = ASCII_INTEGER START_BYTE = 40 BYTES = 4 DESCRIPTION = "S/C application identification" FORMAT = I4 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 4 NAME = SEQ_CNT DATA_TYPE = ASCII_INTEGER START_BYTE = 45 BYTES = 5 DESCRIPTION = "SPEDE packet sequence count" FORMAT = I5 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 5 NAME = SC_TIME DATA_TYPE = ASCII_INTEGER START_BYTE = 51 BYTES = 10 DESCRIPTION = "S/C clock in seconds" FORMAT = I10 UNIT = "s" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 6 NAME = SC_SUBTIME DATA_TYPE = ASCII_INTEGER START_BYTE = 62 BYTES = 3 DESCRIPTION = "S/C clock in 1/256 subseconds" FORMAT = I3 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 7 NAME = CONFIGURATION_TABLE DATA_TYPE = ASCII_INTEGER START_BYTE = 66 BYTES = 3 DESCRIPTION = "SPEDE configuration table number, range 1-9" FORMAT = I3 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 8 NAME = MINUS_X_LP_BIAS_START DATA_TYPE = ASCII_INTEGER START_BYTE = 70 BYTES = 3 DESCRIPTION = "First bias control value for -X probe in Langmuir mode" FORMAT = I3 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 9 NAME = MINUS_X_LP_BIAS_INCREMENT DATA_TYPE = ASCII_INTEGER START_BYTE = 74 BYTES = 3 DESCRIPTION = "If not zero, defines a Langmuir sweep: difference between subsequent measurement points. The related bias voltages are not linearily related to the control values." FORMAT = I3 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 10 NAME = MINUS_X_STEPS DATA_TYPE = ASCII_INTEGER START_BYTE = 78 BYTES = 3 DESCRIPTION = "Number of measurement points in one measurement. In Langmuir mode with INCREMENT > 0 this is the number of bias voltages used in an upward sweep. If the bias code value would become larger than the largest allowed value 255, the value will be 255 for those measurements. If hysteresis measurements are defined (see CONTROL_MINUS_X/_PLUS_X below) another sequence will be performed with same number of measurements and reversed stepping starting from end value of first measurement. The total measurement vector length will then be twice the given number here." FORMAT = I3 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 11 NAME = PLUS_X_LP_BIAS_START DATA_TYPE = ASCII_INTEGER START_BYTE = 82 BYTES = 3 DESCRIPTION = "First bias control value for +X probe in Langmuir mode" FORMAT = I3 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 12 NAME = PLUS_X_LP_BIAS_INCREMENT DATA_TYPE = ASCII_INTEGER START_BYTE = 86 BYTES = 3 DESCRIPTION = "If not zero, defines a Langmuir sweep: difference between subsequent measurement points. The related bias voltages are not linearly related to the control values." FORMAT = I3 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 13 NAME = PLUS_X_STEPS DATA_TYPE = ASCII_INTEGER START_BYTE = 90 BYTES = 3 DESCRIPTION = "Number of measurement points in one measurement. In Langmuir mode with INCREMENT > 0 this is the number of bias voltages used in an upward sweep. If the bias code value would become larger than the largest allowed value 255, the value will be 255 for those measurements. If hysteresis measurements are defined (see CONTROL_MINUS_X/_PLUS_X below) another sequence will be performed with same number of measurements and reversed stepping starting from end value of first measurement. The total measurement vector length will then be twice the given number here." FORMAT = I3 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 14 NAME = CONTROL_MINUS_X DATA_TYPE = ASCII_INTEGER START_BYTE = 94 BYTES = 3 DESCRIPTION = "Decimal representation of the control bit pattern for -X probe. The different powers of 2 and groups thereof have the following meaning: V*2^0: V=0: Voltage mode, V=1: Langmuir (current) mode F*2^1: F=0: Frequency measurement, F=1: Pulse length measurement H*2^2: H=0: no hysteresis measurement, H=1: Hysteresis measurement I*2^3: I=0: large integration constant, I=1: small integration constant 2^4 2^6 are only relevant if H=1 (hysteresis measurement activated) V2*2^4: V2=0 Voltage mode in second measurement phase, V2=1: Langmuir mode F2*2^5: F2=0: Frequency measurement, F2=1: pulse length measurement I2*2^6: I2=0: large integration constant, I2=1: short integration constant W*2^7: W=0: No wave measurement, W=1: wave measurement included" FORMAT = I3 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 15 NAME = CONTROL_PLUS_X DATA_TYPE = ASCII_INTEGER START_BYTE = 98 BYTES = 3 DESCRIPTION = "Decimal representation of the control bit pattern for +X probe. The different powers of 2 and groups thereof have the following meaning: V*2^0: V=0: Voltage mode, V=1: Langmuir (current) mode F*2^1: F=0: Frequency measurement, F=1: Pulse length measurement H*2^2: H=0: no hysteresis measurement, H=1: Hysteresis measurement I*2^3: I=0: large integration constant, I=1: small integration constant 2^4 2^6 are only relevant if H=1 (hysteresis measurement activated) V2*2^4: V2=0 Voltage mode in second measurement phase, V2=1: Langmuir mode F2*2^5: F2=0: Frequency measurement, F2=1: pulse length measurement I2*2^6: I2=0: large integration constant, I2=1: short integration constant W*2^7: W=0: No wave measurement, W=1: wave measurement included" FORMAT = I3 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 16 NAME = STEPPING_INTERVAL DATA_TYPE = ASCII_INTEGER START_BYTE = 102 BYTES = 6 DESCRIPTION = "Time interval between start of integration times in units of 1/256s" FORMAT = I6 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 17 NAME = REPETITION_INTERVAL DATA_TYPE = ASCII_INTEGER START_BYTE = 109 BYTES = 7 DESCRIPTION = "Time interval between start of telemetry packets in units of 1/16s" FORMAT = I7 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 18 NAME = REPETITIONS DATA_TYPE = ASCII_INTEGER START_BYTE = 117 BYTES = 3 DESCRIPTION = "Number of automatic telemetry packet repetitions. 0=infinte (continuous measurement)." FORMAT = I3 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 19 NAME = FREQUENCY_BANDS DATA_TYPE = ASCII_INTEGER START_BYTE = 121 BYTES = 3 DESCRIPTION = "If wave measurements are activated: number for frequency bins" FORMAT = I3 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 20 NAME = WAVE_BIAS_MINUS_X DATA_TYPE = ASCII_INTEGER START_BYTE = 125 BYTES = 3 DESCRIPTION = "Bias voltage on -X probe. If =0, probe is set to voltage" FORMAT = I3 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 21 NAME = WAVE_BIAS_PLUS_X DATA_TYPE = ASCII_INTEGER START_BYTE = 129 BYTES = 3 DESCRIPTION = "Bias voltage on +X probe. If =0, probe is set to voltage" FORMAT = I3 END_OBJECT = COLUMN 4 Raw operation parameters (software dumps) product (ancillary data) 1 General description Level 1b software dump files will contain certain operation parameters (listed below) that affect SPEDE measurements. Each row of the software dump file will contain the time of the dump in UTC and JMD2000, and placeholders for 12 SPEDE operation parameters: . Long frequency integration time in EEPROM . Short frequency integration time in EEPROM . Long pulse measurement value for -X in EEPROM . Short pulse measurement value for -X in EEPROM . Long pulse measurement value for +X in EEPROM . Short pulse measurement value for +X in EEPROM . Long frequency integration time in RAM . Short frequency integration time in RAM . Long pulse measurement value for -X in RAM . Short pulse measurement value for -X in RAM . Long pulse measurement value for +X in RAM . Short pulse measurement value for +X in RAM Each row of the dump contains parameters returned in one telemetry packet. Parameter values not present in a certain memory dump are marked as "N/A". 2 Label example PDS_VERSION_ID = PDS3 LABEL_REVISION_NOTE = "2006-01-03, Jouni Ryno, FMI, initial release" RELEASE_ID = 0001 REVISION_ID = 0000 /* FILE FORMAT */ RECORD_TYPE = FIXED_LENGTH RECORD_BYTES = 198 FILE_RECORDS = 10 LABEL_RECORDS = 13 /* POINTER TO DATA OBJECT */ ^TABLE = 14 /* GENERAL DATA DESCRIPTION PARAMETERS */ FILE_NAME = "SP_200309_SWDUMP_RAW.TAB" DATA_SET_ID = "S1-X-SPEDE-2-EDR-LEOP-CALIBRATION-V1.0" DATA_SET_NAME = "SMART1 PLASMA SPEDE 2 EDR LEOP CALIBRATION V1.0" PRODUCT_ID = "SP_200309_SWDUMP_RAW.TAB" PRODUCT_TYPE = "ANCDR" PRODUCT_CREATION_TIME = 2006-01-25 PROCESSING_LEVEL_ID = 2 PROCESSING_LEVEL_DESC = "Edited data, corrected for telemetry errors" MISSION_ID = "SMART1" MISSION_NAME = "SMALL MISSIONS FOR ADVANCED RESEARCH AND TECHNOLOGY" MISSION_PHASE_NAME = "EARTH ESCAPE PHASE" ORBIT_NUMBER = "N/A" INSTRUMENT_HOST_ID = "S1" INSTRUMENT_HOST_NAME = "SMALL MISSIONS FOR ADVANCED RESEARCH AND TECHNOLOGY" TARGET_TYPE = "PLASMA ENVIRONMENT" TARGET_NAME = "PLASMA" TARGET_DESC = "Spacecraft potential and surrounding plasma" START_TIME = 2003-09-29T17:08:01 STOP_TIME = 2003-09-29T17:14:21 SPACECRAFT_CLOCK_START_COUNT = "2/0000064482.42013" SPACECRAFT_CLOCK_STOP_COUNT = "2/0000064862.47974" PRODUCER_ID = "FMI" PRODUCER_INSTITUTION_NAME = "Finnish Meteorological Institute" PRODUCER_FULL_NAME = "Dr. Anssi Malkki" INSTRUMENT_ID = "SPEDE" INSTRUMENT_NAME = "SPACECRAFT POTENTIAL, ELECTRON AND DUST EXPERIMENT" INSTRUMENT_MODE_ID = "N/A" INSTRUMENT_MODE_DESC = "N/A" DATA_QUALITY_ID = -1 DATA_QUALITY_DESC = "-1=not checked" INSTRUMENT_TYPE = "PLASMA INSTRUMENT" OBJECT = TABLE INTERCHANGE_FORMAT = ASCII ROWS = 10 ROW_BYTES = 196 ROW_SUFFIX_BYTES = 2 COLUMNS = 18 NAME = SPEDE_PARAMETERS ^STRUCTURE = "SPEDE_PARAMETERS.FMT" END_OBJECT = TABLE END SPEDE_PARAMETERS.FMT OBJECT = COLUMN COLUMN_NUMBER = 1 NAME = DATE DATA_TYPE = CHARACTER START_BYTE = 1 BYTES = 23 DESCRIPTION = "S/C clock date in UTC" FORMAT = A23 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 2 NAME = JULIAN_DATE DATA_TYPE = ASCII_REAL START_BYTE = 25 BYTES = 14 DESCRIPTION = "S/C clock date in Modified Julian Date 2000" FORMAT = "F14.8" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 3 NAME = APID DATA_TYPE = ASCII_INTEGER START_BYTE = 40 BYTES = 4 DESCRIPTION = "S/C application identification" FORMAT = I4 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 4 NAME = SEQ_CNT DATA_TYPE = ASCII_INTEGER START_BYTE = 45 BYTES = 5 DESCRIPTION = "SPEDE packet sequence count" FORMAT = I5 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 5 NAME = SC_TIME DATA_TYPE = ASCII_INTEGER START_BYTE = 51 BYTES = 10 DESCRIPTION = "S/C clock in seconds" FORMAT = I10 UNIT = "s" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 6 NAME = SC_SUBTIME DATA_TYPE = ASCII_INTEGER START_BYTE = 62 BYTES = 3 DESCRIPTION = "S/C clock in 1/256 subseconds" FORMAT = I3 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 7 NAME = FREQ_LONG_EEPROM DATA_TYPE = ASCII_INTEGER START_BYTE = 66 BYTES = 10 DESCRIPTION = "Number of 16-MHz clock pulses defining the long integration time. This value is used after each instrument reboot" FORMAT = I10 UNIT = "ms" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 8 NAME = FREQ_SHORT_EEPROM DATA_TYPE = ASCII_INTEGER START_BYTE = 77 BYTES = 10 DESCRIPTION = "Number of 16-MHz clock pulses defining the short integration time. This value is used after each instrument reboot. EEPROM store." FORMAT = I10 UNIT = "ms" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 9 NAME = PULSE_LONG_MINUS_X_EEPROM DATA_TYPE = ASCII_INTEGER START_BYTE = 88 BYTES = 10 DESCRIPTION = "Number of pulses from -X sensor VFC used to determine the pulselength by comparision with 16-MHz clock (long). EEPROM store." FORMAT = I10 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 10 NAME = PULSE_SHORT_MINUS_X_EEPROM DATA_TYPE = ASCII_INTEGER START_BYTE = 99 BYTES = 10 DESCRIPTION = "Number of pulses from -X sensor VFC used to determine the pulselength by comparision with 16-MHz clock (short). EEPROM store." FORMAT = I10 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 11 NAME = PULSE_LONG_PLUS_X_EEPROM DATA_TYPE = ASCII_INTEGER START_BYTE = 110 BYTES = 10 DESCRIPTION = "Number of pulses from +X sensor VFC used to determine the pulselength by comparision with 16-MHz clock (long). EEPROM store." FORMAT = I10 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 12 NAME = PULSE_SHORT_PLUS_X_EEPROM DATA_TYPE = ASCII_INTEGER START_BYTE = 121 BYTES = 10 DESCRIPTION = "Number of pulses from -+ sensor VFC used to determine the pulselength by comparision with 16-MHz clock (short). EEPROM store." FORMAT = I10 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 13 NAME = FREQ_LONG_RAM DATA_TYPE = ASCII_INTEGER START_BYTE = 132 BYTES = 10 DESCRIPTION = "Number of 16-MHz clock pulses defining the long integration time. This value is used after each instrument reboot. RAM store." FORMAT = I10 UNIT = "ms" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 14 NAME = FREQ_SHORT_RAM DATA_TYPE = ASCII_INTEGER START_BYTE = 143 BYTES = 10 DESCRIPTION = "Number of 16-MHz clock pulses defining the short integration time. This value is used after each instrument reboot. RAM store." FORMAT = I10 UNIT = "ms" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 15 NAME = PULSE_LONG_MINUS_X_RAM DATA_TYPE = ASCII_INTEGER START_BYTE = 154 BYTES = 10 DESCRIPTION = "Number of pulses from -X sensor VFC used to determine the pulselength by comparision with 16-MHz clock (long). RAM store." FORMAT = I10 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 16 NAME = PULSE_SHORT_MINUS_X_RAM DATA_TYPE = ASCII_INTEGER START_BYTE = 165 BYTES = 10 DESCRIPTION = "Number of pulses from -X sensor VFC used to determine the pulselength by comparision with 16-MHz clock (short). RAM store." FORMAT = I10 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 17 NAME = PULSE_LONG_PLUS_X_RAM DATA_TYPE = ASCII_INTEGER START_BYTE = 176 BYTES = 10 DESCRIPTION = "Number of pulses from +X sensor VFC used to determine the pulselength by comparision with 16-MHz clock (long). RAM store." FORMAT = I10 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 18 NAME = PULSE_SHORT_PLUS_X_RAM DATA_TYPE = ASCII_INTEGER START_BYTE = 187 BYTES = 10 DESCRIPTION = "Number of pulses from +X sensor VFC used to determine the pulselength by comparision with 16-MHz clock (short). RAM store." FORMAT = I10 END_OBJECT = COLUMN 5 Calibrated electron/ion flux data product 1 General description Each measurement point (row) of calibrated electron/ion flux data has the following components: . Spacecraft time in UTC, ASCII format (time of the measurement) . Spacecraft time in MJD2000 . -X probe shadow status flag (S/C shadow, Earth or Moon umbra, etc.) . Angles between S/C -X, -Y and -Z axis and Sun . Angle between S/C +Z axis and solar array +Z axis . S/C position in GSE coordinates: X, Y, Z . S/C position in LSE coordinates: X, Y, Z . Instrument bias voltage in Volts . Measurement value representing the flux in Amperes . Status flag for the measurement point. Details of the flag as in the label example below. 2 Label example PDS_VERSION_ID = PDS3 LABEL_REVISION_NOTE = "2006-01-03, Jouni Ryno, FMI, initial release" RELEASE_ID = 0001 REVISION_ID = 0000 /* FILE FORMAT */ RECORD_TYPE = FIXED_LENGTH RECORD_BYTES = 173 FILE_RECORDS = 480 LABEL_RECORDS = 16 /* POINTER TO DATA OBJECT */ ^TABLE = 17 /* GENERAL DATA DESCRIPTION PARAMETERS */ FILE_NAME = "SP_00135M050201_1_EF_CAL.TAB" DATA_SET_ID = "S1-X-SPEDE-4-REFDR-EP-MONITORING2-V1.0" DATA_SET_NAME = "SMART1 PLASMA SPEDE 4 REFDR EP- MONITORING2 V1.0" PRODUCT_ID = "SP_00135M050201_1_EF_CAL.TAB" PRODUCT_TYPE = "REFDR" PRODUCT_CREATION_TIME = 2006-01-26 PROCESSING_LEVEL_ID = 4 PROCESSING_LEVEL_DESC = "Calibrated data" MISSION_ID = "SMART1" MISSION_NAME = "SMALL MISSIONS FOR ADVANCED RESEARCH AND TECHNOLOGY" MISSION_PHASE_NAME = "EARTH ESCAPE PHASE" ORBIT_NUMBER = "N/A" INSTRUMENT_HOST_ID = "S1" INSTRUMENT_HOST_NAME = "SMALL MISSIONS FOR ADVANCED RESEARCH AND TECHNOLOGY" TARGET_TYPE = "PLASMA ENVIRONMENT" TARGET_NAME = "PLASMA" TARGET_DESC = "Spacecraft potential and surrounding plasma" START_TIME = 2005-02-01T05:04:34 STOP_TIME = 2005-02-01T13:03:34 SPACECRAFT_CLOCK_START_COUNT = " 8/0029518991.10547" SPACECRAFT_CLOCK_STOP_COUNT = " 8/0029547731.31640" PRODUCER_ID = "FMI" PRODUCER_INSTITUTION_NAME = "Finnish Meteorological Institute" PRODUCER_FULL_NAME = "Dr. Anssi Malkki" INSTRUMENT_ID = "SPEDE" INSTRUMENT_NAME = "SPACECRAFT POTENTIAL, ELECTRON AND DUST EXPERIMENT" INSTRUMENT_MODE_ID = "PC" INSTRUMENT_MODE_DESC = "Probe current (Langmuir)" DATA_QUALITY_ID = -1 DATA_QUALITY_DESC = "-1 = not checked Calibration tables: bias 1.0 background 1.0 frequency_to_current 1.0" INSTRUMENT_TYPE = "PLASMA INSTRUMENT" OBJECT = TABLE INTERCHANGE_FORMAT = ASCII ROWS = 480 ROW_BYTES = 171 ROW_SUFFIX_BYTES = 2 COLUMNS = 14 NAME = SPEDE_ELECTRON_FLUX DESCRIPTION = "SPEDE calibrated electron flux data" ^STRUCTURE = "SPEDE_FLUX.FMT" END_OBJECT = TABLE END SPEDE_FLUX.FMT: OBJECT = COLUMN COLUMN_NUMBER = 1 NAME = DATE DATA_TYPE = TIME START_BYTE = 1 BYTES = 23 DESCRIPTION = "S/C clock date in UTC" FORMAT = A22 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 2 NAME = JULIAN_DATE DATA_TYPE = ASCII_REAL START_BYTE = 25 BYTES = 14 DESCRIPTION = "S/C clock date in Modified Julian Date 2000" FORMAT = "F14.8" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 3 NAME = SHADOW DATA_TYPE = ASCII_INTEGER START_BYTE = 40 BYTES = 1 DESCRIPTION = "Status flag, if the SPEDE -X probe is in shadow or not: 0 = in sun 1 = in S/C shadow 2 = in Earth or Moon umbra 3 = in S/C and Earth or Moon umbra 4 = in Earth or Moon penumbra 5 = in S/C shadow and Earth or Moon penumbra 9 = unknown situation" FORMAT = "I1" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 4 NAME = SC_MX_SUN_ANGLE DATA_TYPE = ASCII_REAL START_BYTE = 42 BYTES = 7 DESCRIPTION = "The angular separation between the spacecraft -X-axis and the sun direction" UNIT = "Deg" MISSING_CONSTANT= "1.E32" FORMAT = "F7.2" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 4 NAME = SC_MY_SUN_ANGLE DATA_TYPE = ASCII_REAL START_BYTE = 50 BYTES = 7 DESCRIPTION = "The angular separation between the spacecraft -Y-axis and the sun direction" UNIT = "Deg" MISSING_CONSTANT= "1.E32" FORMAT = "F7.2" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 4 NAME = SC_MZ_SUN_ANGLE DATA_TYPE = ASCII_REAL START_BYTE = 58 BYTES = 7 DESCRIPTION = "The angular separation between the spacecraft -Z-axis and the sun direction" UNIT = "Deg" MISSING_CONSTANT= "1.E32" FORMAT = "F7.2" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 5 NAME = SC_SA_ANGLE DATA_TYPE = ASCII_REAL START_BYTE = 66 BYTES = 7 DESCRIPTION = "The angular separation between the spacecraft +Z-axis and the solar array +Z-axis." UNIT = "Deg" MISSING_CONSTANT= "1.E32" FORMAT = "F7.2" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 6 NAME = GSE_X DATA_TYPE = ASCII_REAL START_BYTE = 74 BYTES = 9 DESCRIPTION = "S/C position X-component in GSE coordinates" UNIT = "km" MISSING_CONSTANT= "1.E32" FORMAT = "F9.1" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 7 NAME = GSE_Y DATA_TYPE = ASCII_REAL START_BYTE = 84 BYTES = 9 DESCRIPTION = "S/C position Y-component in GSE coordinates" UNIT = "km" MISSING_CONSTANT= "1.E32" FORMAT = "F9.1" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 8 NAME = GSE_Z DATA_TYPE = ASCII_REAL START_BYTE = 94 BYTES = 9 DESCRIPTION = "S/C position Z-component in GSE coordinates" UNIT = "km" MISSING_CONSTANT= "1.E32" FORMAT = "F9.1" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 9 NAME = LSE_X DATA_TYPE = ASCII_REAL START_BYTE = 104 BYTES = 9 DESCRIPTION = "S/C position X-component in LSE coordinates" UNIT = "km" MISSING_CONSTANT= "1.E32" FORMAT = "F9.1" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 10 NAME = LSE_Y DATA_TYPE = ASCII_REAL START_BYTE = 114 BYTES = 9 DESCRIPTION = "S/C position Y-component in LSE coordinates" UNIT = "km" MISSING_CONSTANT= "1.E32" FORMAT = "F9.1" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 11 NAME = LSE_Z DATA_TYPE = ASCII_REAL START_BYTE = 124 BYTES = 9 DESCRIPTION = "S/C position Z-component in LSE coordinates" UNIT = "km" MISSING_CONSTANT= "1.E32" FORMAT = "F9.1" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 12 NAME = BIAS DATA_TYPE = ASCII_REAL START_BYTE = 134 BYTES = 6 DESCRIPTION = "Bias voltage" UNIT = "V" FORMAT = "F6.2" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 13 NAME = MEASUREMENT DATA_TYPE = ASCII_REAL START_BYTE = 141 BYTES = 12 DESCRIPTION = "Measurement value" UNIT = "A" FORMAT = "E12.5E3" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 14 NAME = FLAGS DATA_TYPE = CHARACTER START_BYTE = 155 BYTES = 16 DESCRIPTION = "16th (LS) flag: 0 = the result is checked and found correct 1 = the result is checked and possibly corrected, warnings concerning quality 2 = the result is checked, and found unreliable (no corrections) 9 = the result is unchecked 15th flag: F = frequency measurement, p = original pulse measurement, P = corrected pulse measurement 14th flag: 1 = the first measurement in an measurement vector, _ = following measurements 13th flag: R = the reference voltage was fluctuating during this measurement, _ = the reference voltage was OK (the reference voltage value is obtained from the housekeeping data)" FORMAT = "A16" END_OBJECT = COLUMN 6 Calibrated plasma data product 1 General description Each row of calibrated plasma data has the following components: . Spacecraft time in UTC, ASCII format (time of the first measurement point of the sweep) . Spacecraft time in MJD2000 . -X probe shadow status flag (No shadow, S/C shadow, Earth or Moon umbra, etc.) . Angles between S/C -X, -Y and -Z axis and Sun . Angle between S/C +Z axis and solar array +Z axis . S/C position in GSE coordinates: X, Y, Z . S/C position in LSE coordinates: X, Y, Z . Time increment in seconds: Delta time between two measurement points of the sweep . Vector containing instrument bias voltages of the sweep in Volts . Vector containing measurement values of the sweep in Amperes . Vector containing status flags for each measurement point. Details of the flag as in the label example below. The length of the sweeps can vary. Currently 20 and 40 points are used. In the label example below, 20 points are used. 2 Label example PDS_VERSION_ID = PDS3 LABEL_REVISION_NOTE = "2006-01-03, Jouni Ryno, FMI, initial release" RELEASE_ID = 0001 REVISION_ID = 0000 /* FILE FORMAT */ RECORD_TYPE = FIXED_LENGTH RECORD_BYTES = 1705 FILE_RECORDS = 8 LABEL_RECORDS = 2 /* POINTER TO DATA OBJECT */ ^TABLE = 3 /* GENERAL DATA DESCRIPTION PARAMETERS */ FILE_NAME = "SP_00205_040201_1_PD_40_CAL.TAB" DATA_SET_ID = "S1-X-SPEDE-4-REFDR-BKGRPLASMA-V1.0" DATA_SET_NAME = "SMART1 PLASMA SPEDE 4 REFDR BKGRPLASMA V1.0" PRODUCT_ID = "SP_00205_040201_1_PD_40_CAL.TAB" PRODUCT_TYPE = "REFDR" PRODUCT_CREATION_TIME = 2006-01-26 PROCESSING_LEVEL_ID = 4 PROCESSING_LEVEL_DESC = "Calibrated data" MISSION_ID = "SMART1" MISSION_NAME = "SMALL MISSIONS FOR ADVANCED RESEARCH AND TECHNOLOGY" MISSION_PHASE_NAME = "EARTH ESCAPE PHASE" ORBIT_NUMBER = "N/A" INSTRUMENT_HOST_ID = "S1" INSTRUMENT_HOST_NAME = "SMALL MISSIONS FOR ADVANCED RESEARCH AND TECHNOLOGY" TARGET_TYPE = "PLASMA ENVIRONMENT" TARGET_NAME = "PLASMA" TARGET_DESC = "Spacecraft potential and surrounding plasma" START_TIME = 2004-02-01T23:46:27 STOP_TIME = 2004-02-02T22:39:53 SPACECRAFT_CLOCK_START_COUNT = " 6/0008779952.84375" SPACECRAFT_CLOCK_STOP_COUNT = " 6/0008862358.22656" PRODUCER_ID = "FMI" PRODUCER_INSTITUTION_NAME = "Finnish Meteorological Institute" PRODUCER_FULL_NAME = "Dr. Anssi Malkki" INSTRUMENT_ID = "SPEDE" INSTRUMENT_NAME = "SPACECRAFT POTENTIAL, ELECTRON AND DUST EXPERIMENT" INSTRUMENT_MODE_ID = "PC" INSTRUMENT_MODE_DESC = "Probe current (Langmuir)" DATA_QUALITY_ID = -1 DATA_QUALITY_DESC = "-1 = not checked Calibration tables: bias 1.0 background 1.0 frequency_to_current 1.0" INSTRUMENT_TYPE = "PLASMA INSTRUMENT" OBJECT = TABLE INTERCHANGE_FORMAT = ASCII ROWS = 8 ROW_BYTES = 1703 ROW_SUFFIX_BYTES = 2 COLUMNS = 15 NAME = SPEDE_PLASMA DESCRIPTION = "SPEDE calibrated plasma data" ^STRUCTURE = "SPEDE_PLASMA_40.FMT" END_OBJECT = TABLE END SPEDE_PLASMA_40.FMT: OBJECT = COLUMN COLUMN_NUMBER = 1 NAME = DATE DATA_TYPE = TIME START_BYTE = 1 BYTES = 23 DESCRIPTION = "S/C clock date in UTC" FORMAT = A22 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 2 NAME = JULIAN_DATE DATA_TYPE = ASCII_REAL START_BYTE = 25 BYTES = 14 DESCRIPTION = "S/C clock date in Modified Julian Date 2000" FORMAT = "F14.8" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 3 NAME = SHADOW DATA_TYPE = ASCII_INTEGER START_BYTE = 40 BYTES = 1 DESCRIPTION = "Status flag, if the SPEDE -X probe is in shadow or not: 0 = in sun 1 = in S/C shadow 2 = in Earth or Moon umbra 3 = in S/C and Earth or Moon umbra 4 = in Earth or Moon penumbra 5 = in S/C shadow and Earth or Moon penumbra 9 = unknown situation" FORMAT = "I1" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 4 NAME = SC_MX_SUN_ANGLE DATA_TYPE = ASCII_REAL START_BYTE = 42 BYTES = 7 DESCRIPTION = "The angular separation between the spacecraft -X-axis and the sun direction" UNIT = "Deg" MISSING_CONSTANT= "1.E32" FORMAT = "F7.2" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 5 NAME = SC_MY_SUN_ANGLE DATA_TYPE = ASCII_REAL START_BYTE = 50 BYTES = 7 DESCRIPTION = "The angular separation between the spacecraft -Y-axis and the sun direction" UNIT = "Deg" MISSING_CONSTANT= "1.E32" FORMAT = "F7.2" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 6 NAME = SC_MZ_SUN_ANGLE DATA_TYPE = ASCII_REAL START_BYTE = 58 BYTES = 7 DESCRIPTION = "The angular separation between the spacecraft -Z-axis and the sun direction" UNIT = "Deg" MISSING_CONSTANT= "1.E32" FORMAT = "F7.2" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 7 NAME = SC_SA_ANGLE DATA_TYPE = ASCII_REAL START_BYTE = 66 BYTES = 7 DESCRIPTION = "The angular separation between the spacecraft +Z-axis and the solar array +Z-axis." UNIT = "Deg" MISSING_CONSTANT= "1.E32" FORMAT = "F7.2" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 8 NAME = GSE_X DATA_TYPE = ASCII_REAL START_BYTE = 74 BYTES = 9 DESCRIPTION = "S/C position X-component in GSE coordinates" UNIT = "km" MISSING_CONSTANT= "1.E32" FORMAT = "F9.1" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 9 NAME = GSE_Y DATA_TYPE = ASCII_REAL START_BYTE = 84 BYTES = 9 DESCRIPTION = "S/C position Y-component in GSE coordinates" UNIT = "km" MISSING_CONSTANT= "1.E32" FORMAT = "F9.1" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 10 NAME = GSE_Z DATA_TYPE = ASCII_REAL START_BYTE = 94 BYTES = 9 DESCRIPTION = "S/C position Z-component in GSE coordinates" UNIT = "km" MISSING_CONSTANT= "1.E32" FORMAT = "F9.1" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 11 NAME = LSE_X DATA_TYPE = ASCII_REAL START_BYTE = 104 BYTES = 9 DESCRIPTION = "S/C position X-component in LSE coordinates" UNIT = "km" MISSING_CONSTANT= "1.E32" FORMAT = "F9.1" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 12 NAME = LSE_Y DATA_TYPE = ASCII_REAL START_BYTE = 114 BYTES = 9 DESCRIPTION = "S/C position Y-component in LSE coordinates" UNIT = "km" MISSING_CONSTANT= "1.E32" FORMAT = "F9.1" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 13 NAME = LSE_Z DATA_TYPE = ASCII_REAL START_BYTE = 124 BYTES = 9 DESCRIPTION = "S/C position Z-component in LSE coordinates" UNIT = "km" MISSING_CONSTANT= "1.E32" FORMAT = "F9.1" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 14 NAME = TIME_INCREMENT DATA_TYPE = ASCII_REAL START_BYTE = 134 BYTES = 7 UNIT = "s" DESCRIPTION = "Time difference between start of integration periods of subsequent measurements in units of seconds" FORMAT = "F7.3" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 15 NAME = BIAS DATA_TYPE = ASCII_REAL START_BYTE = 142 BYTES = 280 ITEM_BYTES = 6 ITEMS = 40 ITEM_OFFSET = 7 DESCRIPTION = "Bias voltage" UNIT = "V" FORMAT = "F6.2" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 16 NAME = MEASUREMENT DATA_TYPE = ASCII_REAL START_BYTE = 422 BYTES = 520 ITEM_BYTES = 12 ITEMS = 40 ITEM_OFFSET = 13 DESCRIPTION = "Measurement value" UNIT = "A" FORMAT = "E12.5E3" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 17 NAME = FLAGS DATA_TYPE = CHARACTER START_BYTE = 943 BYTES = 760 ITEM_BYTES = 16 ITEMS = 40 ITEM_OFFSET = 19 DESCRIPTION = "16th (LS) flag: 0 = the result is checked and found correct 1 = the result is checked and possibly corrected, warnings concerning quality 2 = the result is checked, and found unreliable (no corrections) 9 = the result is unchecked 15th flag: F = frequency measurement, p = original pulse measurement, P = corrected pulse measurement 14th flag: 1 = the first measurement in an measurement vector, _ = following measurements 13th flag: R = the reference voltage was fluctuating during this measurement, _ = the reference voltage was OK (the reference voltage value is obtained from the housekeeping data)" FORMAT = "A16" END_OBJECT = COLUMN 7 Calibrated electric field data product N/A. No electric data field products are included in the present datasets. 8 Calibrated wave data 1 General description Each row of calibrated wave data has the following components: . Spacecraft time in UTC, ASCII format (time of the first measurement point of the wave measurement) . Spacecraft time in MJD2000 . -X probe shadow status flag (No shadow, S/C shadow, Earth or Moon umbra, etc.) . Angles between S/C -X, -Y and -Z axis and Sun . Angle between S/C +Z axis and solar array +Z axis . S/C position in GSE coordinates: X, Y, Z . S/C position in LSE coordinates: X, Y, Z . Time increment in seconds: Delta time between two measurement points of the measurement . Wave data -X bias voltage . Wave data +X bias voltage . Wave power vector: wave power at steps 5000 Hz, 2500 Hz, 1250 Hz, 625 Hz, 313 Hz, 156 Hz, 78 Hz, 39 Hz, 20 Hz, 10 Hz. . Vector containing status flags for each measurement point. Details of the flag as in the label example below. 2 Label example PDS_VERSION_ID = PDS3 LABEL_REVISION_NOTE = "2006-01-03, Jouni Ryno, FMI, initial release" RELEASE_ID = 0001 REVISION_ID = 0000 /* FILE FORMAT */ RECORD_TYPE = FIXED_LENGTH RECORD_BYTES = 305 FILE_RECORDS = 144 LABEL_RECORDS = 9 /* POINTER TO DATA OBJECT */ ^TABLE = 10 /* GENERAL DATA DESCRIPTION PARAMETERS */ FILE_NAME = "SP_00235M050228_W_WA_10_CAL.TAB" DATA_SET_ID = "S1-X-SPEDE-4-REFDR-EP-MONITORING2-V1.0" DATA_SET_NAME = "SMART1 PLASMA SPEDE 4 REFDR EP- MONITORING2 V1.0" PRODUCT_ID = "SP_00235M050228_W_WA_10_CAL.TAB" PRODUCT_TYPE = "REFDR" PRODUCT_CREATION_TIME = 2006-01-26 PROCESSING_LEVEL_ID = 4 PROCESSING_LEVEL_DESC = "Calibrated data" MISSION_ID = "SMART1" MISSION_NAME = "SMALL MISSIONS FOR ADVANCED RESEARCH AND TECHNOLOGY" MISSION_PHASE_NAME = "EARTH ESCAPE PHASE" ORBIT_NUMBER = "N/A" INSTRUMENT_HOST_ID = "S1" INSTRUMENT_HOST_NAME = "SMALL MISSIONS FOR ADVANCED RESEARCH AND TECHNOLOGY" TARGET_TYPE = "PLASMA ENVIRONMENT" TARGET_NAME = "PLASMA" TARGET_DESC = "Spacecraft potential and surrounding plasma" START_TIME = 2005-02-28T21:46:40 STOP_TIME = 2005-02-28T23:22:00 SPACECRAFT_CLOCK_START_COUNT = " 8/0031911897.44531" SPACECRAFT_CLOCK_STOP_COUNT = " 8/0031917617.48047" PRODUCER_ID = "FMI" PRODUCER_INSTITUTION_NAME = "Finnish Meteorological Institute" PRODUCER_FULL_NAME = "Dr. Anssi Malkki" INSTRUMENT_ID = "SPEDE" INSTRUMENT_NAME = "SPACECRAFT POTENTIAL, ELECTRON AND DUST EXPERIMENT" INSTRUMENT_MODE_ID = "WA" INSTRUMENT_MODE_DESC = "Wave measurement (Voltage mode)" DATA_QUALITY_ID = -1 DATA_QUALITY_DESC = "-1 = not checked Calibration tables: bias 1.0 background 1.0 frequency_to_current 1.0" INSTRUMENT_TYPE = "PLASMA INSTRUMENT" OBJECT = TABLE INTERCHANGE_FORMAT = ASCII ROWS = 144 ROW_BYTES = 303 ROW_SUFFIX_BYTES = 2 COLUMNS = 16 NAME = SPEDE_WAVE_MEASUREMENT DESCRIPTION = "SPEDE power spectrum" ^STRUCTURE = "SPEDE_WAVE.FMT" END_OBJECT = TABLE END SPEDE_WAVE.FMT OBJECT = COLUMN COLUMN_NUMBER = 1 NAME = DATE DATA_TYPE = TIME START_BYTE = 1 BYTES = 23 DESCRIPTION = "S/C clock date in UTC" FORMAT = A22 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 2 NAME = JULIAN_DATE DATA_TYPE = ASCII_REAL START_BYTE = 25 BYTES = 14 DESCRIPTION = "S/C clock date in Modified Julian Date 2000" FORMAT = "F14.8" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 3 NAME = SHADOW DATA_TYPE = ASCII_INTEGER START_BYTE = 40 BYTES = 1 DESCRIPTION = "Status flag, if the SPEDE -X probe is in shadow or not: 0 = in sun 1 = in S/C shadow 2 = in Earth or Moon umbra 3 = in S/C and Earth or Moon umbra 4 = in Earth or Moon penumbra 5 = in S/C shadow and Earth or Moon penumbra 9 = unknown situation" FORMAT = "I1" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 4 NAME = SC_MX_SUN_ANGLE DATA_TYPE = ASCII_REAL START_BYTE = 42 BYTES = 7 DESCRIPTION = "The angular separation between the spacecraft -X-axis and the sun direction" UNIT = "Deg" MISSING_CONSTANT= "1.E32" FORMAT = "F7.2" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 5 NAME = SC_MY_SUN_ANGLE DATA_TYPE = ASCII_REAL START_BYTE = 50 BYTES = 7 DESCRIPTION = "The angular separation between the spacecraft -Y-axis and the sun direction" UNIT = "Deg" MISSING_CONSTANT= "1.E32" FORMAT = "F7.2" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 6 NAME = SC_MZ_SUN_ANGLE DATA_TYPE = ASCII_REAL START_BYTE = 58 BYTES = 7 DESCRIPTION = "The angular separation between the spacecraft -Z-axis and the sun direction" UNIT = "Deg" MISSING_CONSTANT= "1.E32" FORMAT = "F7.2" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 7 NAME = SC_SA_ANGLE DATA_TYPE = ASCII_REAL START_BYTE = 66 BYTES = 7 DESCRIPTION = "The angular separation between the spacecraft +Z-axis and the solar array +Z-axis." UNIT = "Deg" MISSING_CONSTANT= "1.E32" FORMAT = "F7.2" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 8 NAME = GSE_X DATA_TYPE = ASCII_REAL START_BYTE = 74 BYTES = 9 DESCRIPTION = "S/C position X-component in GSE coordinates" UNIT = "km" MISSING_CONSTANT= "1.E32" FORMAT = "F9.1" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 9 NAME = GSE_Y DATA_TYPE = ASCII_REAL START_BYTE = 84 BYTES = 9 DESCRIPTION = "S/C position Y-component in GSE coordinates" UNIT = "km" MISSING_CONSTANT= "1.E32" FORMAT = "F9.1" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 10 NAME = GSE_Z DATA_TYPE = ASCII_REAL START_BYTE = 94 BYTES = 9 DESCRIPTION = "S/C position Z-component in GSE coordinates" UNIT = "km" MISSING_CONSTANT= "1.E32" FORMAT = "F9.1" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 11 NAME = LSE_X DATA_TYPE = ASCII_REAL START_BYTE = 104 BYTES = 9 DESCRIPTION = "S/C position X-component in LSE coordinates" UNIT = "km" MISSING_CONSTANT= "1.E32" FORMAT = "F9.1" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 12 NAME = LSE_Y DATA_TYPE = ASCII_REAL START_BYTE = 114 BYTES = 9 DESCRIPTION = "S/C position Y-component in LSE coordinates" UNIT = "km" MISSING_CONSTANT= "1.E32" FORMAT = "F9.1" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 13 NAME = LSE_Z DATA_TYPE = ASCII_REAL START_BYTE = 124 BYTES = 9 DESCRIPTION = "S/C position Z-component in LSE coordinates" UNIT = "km" MISSING_CONSTANT= "1.E32" FORMAT = "F9.1" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 14 NAME = TIME_INCREMENT DATA_TYPE = ASCII_REAL START_BYTE = 134 BYTES = 7 UNIT = "s" DESCRIPTION = "Time difference between start of integration periods of subsequent measurements in units of seconds" FORMAT = "F7.3" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 15 NAME = MINUS_X_BIAS DATA_TYPE = ASCII_REAL START_BYTE = 142 BYTES = 6 DESCRIPTION = "wave data -X bias voltage" UNIT = "V" FORMAT = "F6.2" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 16 NAME = PLUS_X_BIAS DATA_TYPE = ASCII_REAL START_BYTE = 149 BYTES = 6 DESCRIPTION = "wave data +X bias voltage" UNIT = "V" FORMAT = "F6.2" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 17 NAME = WAVE_POWER DATA_TYPE = ASCII_REAL START_BYTE = 156 BYTES = 130 ITEM_BYTES = 12 ITEMS = 10 ITEM_OFFSET = 13 DESCRIPTION = "Wave power at the frequency step, starting from 5 kHz, then decreasing by half in each step: item 1: 5000 Hz item 2: 2500 Hz item 3: 1250 Hz item 4: 625 Hz item 5: 313 Hz item 6: 156 Hz item 7: 78 Hz item 8: 39 Hz item 9: 20 Hz item 10: 10 Hz. The power is calculated from the raw data with the formula p = raw^2/(2*N^3)" FORMAT = "E12.5E3" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 18 NAME = FLAGS DATA_TYPE = CHARACTER START_BYTE = 287 BYTES = 16 DESCRIPTION = "16th (LS) flag: 0 = the result is checked and found correct 1 = the result is checked and possibly corrected, warnings concerning quality 2 = the result is checked, and found unreliable (no corrections) 9 = the result is unchecked 15th flag: F = frequency measurement, p = original pulse measurement, P = corrected pulse measurement, _ = not applicaple (as in wave measurement) 14th flag: 1 = the first measurement in an measurement vector, _ = following measurements 13th flag: R = the reference voltage was fluctuating during this measurement, _ = the reference voltage was OK (the reference voltage value is obtained from the housekeeping data)" FORMAT = "A16" END_OBJECT = COLUMN 9 Calibrated housekeeping data (ancillary product) 1 General description Each row of calibrated housekeeping data product has the following components: . Spacecraft time in UTC, ASCII format (time of the measurement) . Spacecraft time in MJD2000 . Reference voltage of -X probe in Volts (nominal value ? 2.5 V) . Reference voltage of +X probe in Volts (nominal value ? 2.5 V) . Temperature of +X channel electronics in Celcius degrees . Ground reference voltage in Volts . Status flag vector: 1st flag: R = reference fluctuation, _ = no fluctuation (fluctuation means that raw value was outside nominal values of 95-105). 2nd (LS) flag: 0 = the result is checked and found correct 1 = the result is checked and possibly corrected, warnings concerning quality 2 = the result is checked, and found unreliable (no corrections) 9 = the result is unchecked Fluctuation of a reference voltage can be clearly seen in abnormally high or low reference voltage values. Also the scientific measurements performed at that time with the fluctuating probe cannot be trusted. In case of probe +X, fluctuating reference voltage also affects temperature measurement. Reference fluctuation flags ('R') in status vectors of Level 2 scientific products (electron/ion flux and plasma data) are obtained from ancillary housekeeping data. 2 Label example PDS_VERSION_ID = PDS3 LABEL_REVISION_NOTE = "2006-01-03, Jouni Ryno, FMI, initial release" RELEASE_ID = 0001 REVISION_ID = 0000 /* FILE FORMAT */ RECORD_TYPE = FIXED_LENGTH RECORD_BYTES = 74 FILE_RECORDS = 16 LABEL_RECORDS = 36 /* POINTER TO DATA OBJECT */ ^TABLE = 37 /* GENERAL DATA DESCRIPTION PARAMETERS */ FILE_NAME = "SP_00135M050201_HK_CAL.TAB" DATA_SET_ID = "S1-X-SPEDE-4-REFDR-EP-MONITORING2-V1.0" DATA_SET_NAME = "SMART1 PLASMA SPEDE 4 REFDR EP- MONITORING2 V1.0" PRODUCT_ID = "SP_00135M050201_HK_CAL.TAB" PRODUCT_TYPE = "ANCDR" PRODUCT_CREATION_TIME = 2006-01-26 PROCESSING_LEVEL_ID = 4 PROCESSING_LEVEL_DESC = "Calibrated data" MISSION_ID = "SMART1" MISSION_NAME = "SMALL MISSIONS FOR ADVANCED RESEARCH AND TECHNOLOGY" MISSION_PHASE_NAME = "EARTH ESCAPE PHASE" ORBIT_NUMBER = "N/A" INSTRUMENT_HOST_ID = "S1" INSTRUMENT_HOST_NAME = "SMALL MISSIONS FOR ADVANCED RESEARCH AND TECHNOLOGY" TARGET_TYPE = "PLASMA ENVIRONMENT" TARGET_NAME = "PLASMA" TARGET_DESC = "Spacecraft potential and surrounding plasma" START_TIME = 2005-02-01T05:04:34 STOP_TIME = 2005-02-01T12:34:34 SPACECRAFT_CLOCK_START_COUNT = " 8/0029518991.10550" SPACECRAFT_CLOCK_STOP_COUNT = " 8/0029545991.31640" PRODUCER_ID = "FMI" PRODUCER_INSTITUTION_NAME = "Finnish Meteorological Institute" PRODUCER_FULL_NAME = "Dr. Anssi Malkki" INSTRUMENT_ID = "SPEDE" INSTRUMENT_NAME = "SPACECRAFT POTENTIAL, ELECTRON AND DUST EXPERIMENT" INSTRUMENT_MODE_ID = "N/A" INSTRUMENT_MODE_DESC = "Not applicable" DATA_QUALITY_ID = -1 DATA_QUALITY_DESC = "-1 = not checked Calibration tables: bias 1.0 background 1.0 frequency_to_current 1.0" INSTRUMENT_TYPE = "PLASMA INSTRUMENT" OBJECT = TABLE INTERCHANGE_FORMAT = ASCII ROWS = 16 ROW_BYTES = 72 ROW_SUFFIX_BYTES = 2 COLUMNS = 7 NAME = SPEDE_HK ^STRUCTURE = "SPEDE_HK.FMT" END_OBJECT = TABLE END SPEDE_HK.FMT: OBJECT = COLUMN COLUMN_NUMBER = 1 NAME = DATE DATA_TYPE = TIME START_BYTE = 1 BYTES = 23 DESCRIPTION = "S/C clock date in UTC" FORMAT = A22 END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 2 NAME = JULIAN_DATE DATA_TYPE = ASCII_REAL START_BYTE = 25 BYTES = 14 DESCRIPTION = "S/C clock date in Modified Julian Date 2000" FORMAT = "F14.8" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 3 NAME = REF_VOLT_MINUS_X_CAL DATA_TYPE = ASCII_INTEGER START_BYTE = 40 BYTES = 6 DESCRIPTION = "2.5V -X reference voltage, data value with frequency measurement using 4ms integration. Calculated from: (REF_VOLT_MINUS_X-GROUND)*250/-10039.6" UNIT = "V" FORMAT = "F6.3" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 4 NAME = REF_VOLT_PLUS_X_CAL DATA_TYPE = ASCII_INTEGER START_BYTE = 47 BYTES = 6 DESCRIPTION = "2.5V +X reference voltage, data value with frequency measurement using 4ms integration Calculated from: (REF_VOLT_PLUS_X-GROUND)*250/-10039.6" UNIT = "V" FORMAT = "6.3" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 5 NAME = TEMP_PLUS_X_CAL DATA_TYPE = ASCII_INTEGER START_BYTE = 54 BYTES = 6 DESCRIPTION = "Temperature of +X channel electronics, data value with frequency measurement using 20ms integration -1280, resolution 3C degree. Calculated from: -3.18314*(TEMP_PLUS_X-7.8*(GROUND- 200))+603.51" UNIT = "DegC" FORMAT = "7.2" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 6 NAME = GROUND_CAL DATA_TYPE = ASCII_INTEGER START_BYTE = 62 BYTES = 6 DESCRIPTION = "Ground reference voltage, data value with frequency measurement using 4ms integration Calculated from: (GROUND-200)*250/-10033.0" UNIT = "V" FORMAT = "6.3" END_OBJECT = COLUMN OBJECT = COLUMN COLUMN_NUMBER = 7 NAME = STATE DATA_TYPE = ASCII_INTEGER START_BYTE = 70 BYTES = 2 DESCRIPTION = "2nd (LS) flag: 0 = the result is checked and found correct 1 = the result is checked and possibly corrected, warnings concerning quality 2 = the result is checked, and found unreliable (no corrections) 9 = the result is unchecked 1st flag: R = the reference voltage was fluctuating during this measurement, _ = the reference voltage was OK" FORMAT = "A2" END_OBJECT = COLUMN 4 Indices - summary tables of data products Each data set has an index that summarizes the data products (files). The index table contains parameters that identify each product found in the archive and describes the observation / instrument state and its related information. 1 Level 1b The parameters chosen for the index tables describe the product type (science, configuration table dump, or software dump), start and end time of the product in UTC and spacecraft clock seconds, and for science also: measurement orbit number, probe (1,2, or W), and bias type (probe current, or probe voltage). Parameters not applicable to the non-science products are set to N/A in the index table. Details of the parameters are given in the index label below: PDS_VERSION_ID = PDS3 RECORD_TYPE = FIXED_LENGTH RECORD_BYTES = 229 FILE_RECORDS = 79 ^INDEX_TABLE = "INDEX.TAB" DATA_SET_ID = "S1-X-SPEDE-2-EDR-LEOP-CALIBRATION-V1.0" PRODUCT_ID = "INDEX" VOLUME_ID = "N/A" PRODUCT_CREATION_TIME = 2005-08-15 MISSION_ID = "SMART1" INSTRUMENT_HOST_ID = "S1" INSTRUMENT_ID = "SPEDE" OBJECT = INDEX_TABLE INTERCHANGE_FORMAT = ASCII ROWS = 79 COLUMNS = 12 ROW_BYTES = 227 INDEX_TYPE = SINGLE DESCRIPTION = "The index table contains parameters that identify each product found in the archive and describes the observation/instrument state and related information for it." OBJECT = COLUMN NAME = FILE_SPECIFICATION_NAME COLUMN_NUMBER = 1 DATA_TYPE = "CHARACTER" START_BYTE = 2 BYTES = 52 FORMAT = "A52" DESCRIPTION = "Complete file name." END_OBJECT = COLUMN OBJECT = COLUMN NAME = PRODUCT_ID COLUMN_NUMBER = 2 DATA_TYPE = "CHARACTER" START_BYTE = 57 BYTES = 31 FORMAT = "A31" DESCRIPTION = "Product ID." END_OBJECT = COLUMN OBJECT = COLUMN NAME = PRODUCT_TYPE COLUMN_NUMBER = 3 DATA_TYPE = "CHARACTER" START_BYTE = 91 BYTES = 7 FORMAT = "A7" DESCRIPTION = "Product type, either SCIENCE, CONFIG or SWDUMP" END_OBJECT = COLUMN OBJECT = COLUMN NAME = START_TIME COLUMN_NUMBER = 4 DATA_TYPE = TIME START_BYTE = 101 BYTES = 19 FORMAT = "A19" DESCRIPTION = "Start time of the product." END_OBJECT = COLUMN OBJECT = COLUMN NAME = STOP_TIME COLUMN_NUMBER = 5 DATA_TYPE = TIME START_BYTE = 123 BYTES = 19 FORMAT = "A19" DESCRIPTION = "Stop time of the product." END_OBJECT = COLUMN OBJECT = COLUMN NAME = SPACECRAFT_CLOCK_START_COUNT COLUMN_NUMBER = 6 DATA_TYPE = TIME START_BYTE = 145 BYTES = 19 FORMAT = "A19" DESCRIPTION = "Start time of the product presented as on-board clock." END_OBJECT = COLUMN OBJECT = COLUMN NAME = SPACECRAFT_CLOCK_STOP_COUNT COLUMN_NUMBER = 7 DATA_TYPE = TIME START_BYTE = 167 BYTES = 19 FORMAT = "A19" DESCRIPTION = "Stop time of the product presented as on-board clock." END_OBJECT = COLUMN OBJECT = COLUMN NAME = ORBIT COLUMN_NUMBER = 8 DATA_TYPE = ASCII_INTEGER START_BYTE = 189 BYTES = 5 FORMAT = "A5" DESCRIPTION = "Spacecraft orbit number" END_OBJECT = COLUMN OBJECT = COLUMN NAME = PRODUCT_CREATION_TIME COLUMN_NUMBER = 9 DATA_TYPE = TIME START_BYTE = 197 BYTES = 10 FORMAT = "A10" DESCRIPTION = "Time when the product was created." END_OBJECT = COLUMN OBJECT = COLUMN NAME = PROBE COLUMN_NUMBER = 10 DATA_TYPE = CHARACTER START_BYTE = 210 BYTES = 3 DESCRIPTION = "1 = -X probe, 2 = +X probe, W = wave measurement" FORMAT = A3 END_OBJECT = COLUMN OBJECT = COLUMN NAME = BIAS_TYPE COLUMN_NUMBER = 11 DATA_TYPE = CHARACTER START_BYTE = 216 BYTES = 3 DESCRIPTION = "I = probe current, V = probe voltage" FORMAT = A3 END_OBJECT = COLUMN OBJECT = COLUMN NAME = LENGTH COLUMN_NUMBER = 12 DATA_TYPE = ASCII_INTEGER START_BYTE = 222 BYTES = 3 DESCRIPTION = "Measurement vector length" FORMAT = I3 END_OBJECT = COLUMN END_OBJECT = INDEX_TABLE END 2 Level 2 The parameters chosen for level 2 index tables describe the product type (electron/ion flux, plasma data (sweep) or housekeeping), start and end time of the product in UTC and spacecraft clock seconds, measurement orbit number, and probe (1,2, or W). Details of the parameters are given in the index label below: PDS_VERSION_ID = PDS3 RECORD_TYPE = FIXED_LENGTH RECORD_BYTES = 213 FILE_RECORDS = 56 ^INDEX_TABLE = "INDEX.TAB" DATA_SET_ID = "S1-X-SPEDE-4-REFDR-LEOP-CALIBRATION- V1.0" PRODUCT_ID = "INDEX" VOLUME_ID = "N/A" PRODUCT_CREATION_TIME = 2005-09-09 MISSION_ID = "SMART1" INSTRUMENT_HOST_ID = "S1" INSTRUMENT_ID = "SPEDE" OBJECT = INDEX_TABLE INTERCHANGE_FORMAT = ASCII ROWS = 56 COLUMNS = 10 ROW_BYTES = 213 INDEX_TYPE = SINGLE DESCRIPTION = "The index table contains parameters that identify each product found in the archive and describes the observation/instrument state and related information for it." OBJECT = COLUMN NAME = FILE_SPECIFICATION_NAME COLUMN_NUMBER = 1 DATA_TYPE = "CHARACTER" START_BYTE = 2 BYTES = 52 FORMAT = "A52" DESCRIPTION = "Complete file name." END_OBJECT = COLUMN OBJECT = COLUMN NAME = PRODUCT_ID COLUMN_NUMBER = 2 DATA_TYPE = "CHARACTER" START_BYTE = 57 BYTES = 31 FORMAT = "A31" DESCRIPTION = "Product ID." END_OBJECT = COLUMN OBJECT = COLUMN NAME = PRODUCT_TYPE COLUMN_NUMBER = 3 DATA_TYPE = "CHARACTER" START_BYTE = 91 BYTES = 5 FORMAT = "A5" DESCRIPTION = "Product type, either FLUX for the electron flux data, SWEEP for the plasma data, WAVE for wavelet data or HK for the housekeeping data." END_OBJECT = COLUMN OBJECT = COLUMN NAME = START_TIME COLUMN_NUMBER = 4 DATA_TYPE = TIME START_BYTE = 99 BYTES = 19 FORMAT = "A19" DESCRIPTION = "Start time of the product." END_OBJECT = COLUMN OBJECT = COLUMN NAME = STOP_TIME COLUMN_NUMBER = 5 DATA_TYPE = TIME START_BYTE = 121 BYTES = 19 FORMAT = "A19" DESCRIPTION = "Stop time of the product." END_OBJECT = COLUMN OBJECT = COLUMN NAME = SPACECRAFT_CLOCK_START_COUNT COLUMN_NUMBER = 6 DATA_TYPE = TIME START_BYTE = 143 BYTES = 19 FORMAT = "A19" DESCRIPTION = "Start time of the product presented as on-board clock." END_OBJECT = COLUMN OBJECT = COLUMN NAME = SPACECRAFT_CLOCK_STOP_COUNT COLUMN_NUMBER = 7 DATA_TYPE = TIME START_BYTE = 165 BYTES = 19 FORMAT = "A19" DESCRIPTION = "Stop time of the product presented as on-board clock." END_OBJECT = COLUMN OBJECT = COLUMN NAME = ORBIT COLUMN_NUMBER = 8 DATA_TYPE = ASCII_INTEGER START_BYTE = 187 BYTES = 5 FORMAT = "A5" DESCRIPTION = "Spacecraft orbit number" END_OBJECT = COLUMN OBJECT = COLUMN NAME = PRODUCT_CREATION_TIME COLUMN_NUMBER = 9 DATA_TYPE = TIME START_BYTE = 195 BYTES = 10 FORMAT = "A10" DESCRIPTION = "Time when the product was created." END_OBJECT = COLUMN OBJECT = COLUMN NAME = PROBE COLUMN_NUMBER = 10 DATA_TYPE = CHARACTER START_BYTE = 208 BYTES = 3 DESCRIPTION = "1 = -X probe, 2 = +X probe, W = wave measurement" FORMAT = A3 END_OBJECT = COLUMN END_OBJECT = INDEX_TABLE END Appendix: Available Software to read PDS files No software is included in present datasets. Appendix: Example of Directory Listing of Data Set: S1-X-SPEDE-4-REFDR-LEOP-CALIBRATION-V1.0 TOP-LEVEL DIRECTORY | |- AAREADME.TXT README document for the dataset. | |- VOLDESC.CAT Description of the data volume | | |- [CALIB] Calibration data directory. | | | |- CALINFO.TXT Info about CALIB directory contents. | | | |- SPEDE_BIAS_CALIB.TAB Lookup table for bias calibration. | | | |- SPEDE_CURRENT_CALIB.TAB Coefficients for current calibration. | | |- [CATALOG] The directory containing information | | about SPEDE LEOP calibration data set. | | | |- CATINFO.TXT Info about CATALOG directory contents. | | | |- MISSION.CAT SMART-1 mission description, provided | | by SMART-1 project. | | | |- INSTHOST.CAT SMART-1 spacecraft description, | | provided by SMART-1 project. | | | |- INST.CAT SPEDE instrument description. | | | |- DATASET.CAT Data set description. | | | |- SOFT.CAT Software description. Empty. | | |- REFERENCES.CAT References. Empty. | | | |- RELEASE.CAT Release information. | | |- [DATA] The directory for instrument data | | products. | | | |- [200309] September 2003 data products. | | | | | data products | | | |- [200310] October 2003 data products. | | | data products | | |- [DOCUMENT] The directory containing documentation. | | | |- DOCINFO.TXT Info about DOCUMENT directory contents. | | | |- SPEDESIS.ASC SPEDE PDS interface description in | | ASCII format. | | | |- SPEDESISXXX.JPG Pictures to SPEDESIS document in JPG. | | | |- SPEDESIS.PDF SPEDE PDS interface description in | | PDF format (including pictures). | | | |- SPEDESIS.LBL PDS detached label for SPEDESIS doc. | | | |- SPEDEPAPER.ASC SPEDE paper in ASCII format. | | | |- SPEDEPAPER.PDF SPEDE paper in PDF format. | | | |- SPEDEPAPER.LBL PDS detached label for SPEDE paper. | | | |- [INDEX] The directory for INDEX files. | | | |- INDEX.LBL A PDS detached label describing | | INDEX.TAB | |- INDEX.TAB Tabular summary of data files. | | | |- INDXINFO.TXT Info about INDEX directory contents. | | |- [LABEL] The directory for formatting containers | | used by attached labels. | | | |- LABINFO.TXT Info about LABEL directory contents. | | | |- SPEDE_FLUX.FMT Format file used by electron/ion flux | | data product label. | |- SPEDE_HK.FMT Format file used by housekeeping | | data product labels. | |- SPEDE_PLASMA_20.FMT Format file for 20-point SPEDE | | plasma data product labels. | |- SPEDE_PLASMA_40.FMT Format file for 40-point SPEDE | | plasma data product labels.