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        <logical_identifier>urn:nasa:pds:ody_accel:document:raw_dataset</logical_identifier>
        <version_id>1.0</version_id>
        <title>ODY ACCELEROMETER RAW DATA RECORDS V2.0</title>
        <information_model_version>1.3.0.1</information_model_version>
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        <Citation_Information>
            <editor_list>Tolson, R.H. </editor_list>
            <publication_year>2007</publication_year>
            <description>PDS3 ODY ACCELEROMETER Raw Data Set Description</description>
        </Citation_Information>
        <Modification_History>
            <Modification_Detail>
                <modification_date>2015-01-14</modification_date>
                <version_id>1.0</version_id>
                <description>This file was modified to convert to PDS4 standards</description>
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        </Modification_History>
    </Identification_Area>
    <Reference_List>
        <Internal_Reference>
            <lid_reference>urn:nasa:pds:context:instrument:accel.ody</lid_reference>
            <reference_type>document_to_instrument</reference_type>
        </Internal_Reference>
        <External_Reference>
            <reference_text>TOLSONETAL2005</reference_text>
            <description>Tolson, R., et al., Application of
                Accelerometer Data to Mars Odyssey Aerobraking and Atmospheric Modeling,
                Journal of Spacecraft and Rockets, Vol 42, No. 3, pp. 435-443, 2005.</description>
        </External_Reference>
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    <Document>
        <revision_id>2.0</revision_id>
        <document_name>ODY ACCELEROMETER RAW DATA RECORDS V2.0</document_name>
        <editor_list>Tolson, R.H.</editor_list>
        <copyright>PDS</copyright>
        <publication_date>2007-11-01</publication_date>
        <document_editions>1</document_editions>
        <description>
            Data Set Overview
            =================
            All level zero accelerometer data are packaged by periapsis number for 
            each aerobraking orbit.  Each orbit is identified by a file with name  
            Pyyy where where 'yyy' is the three digit periapsis number. Level 0 
            accelerometer data are provided every 1.0 seconds during an interval of 
            time that generally assures 60 seconds of data before and after the 
            spacecraft passes through the 170 km altitude above the surface of Mars.
        </description>
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