The variableDef element is used to define each
	constant, parameter, or variable used within or generated by the defined subsystem model. It
	contains attributes including the variable name (used for documentation), an XML-unique
	varID identifier (used for automatic code generation), the units of
	measure of the variable, and optional axis system, sign convention, alias, and symbol
	declarations. Optional sub-elements include a written text description and a mathematical
	description, in MathML 2 content markup, of the calculations needed to derive the variable
	from other variables or function table outputs. An optional sub-element,
	isOutput, serves to indicate an intermediate calculation that should be
	brought out to the rest of the simulation. Another optional sub-element,
	isStdAIAA, indicates the variable name is defined in the 
	AIAA simulation standards document. A final sub-element,
	uncertainty, captures the statistical properties of a (normally constant)
	parameter.
There must be a single variableDef for each and every input, output or
	intermediate constant or variable within the DAVEfunc model.
    variableDef+ : name, varID, units, [axisSystem, sign, alias, symbol, initialValue]
        description? :
            (description character data)
        calculation? :
            math (defined in MathML2.0 DTD) :
        isOutput? :
        isStdAIAA? :
        uncertainty? : effect
            (normalPDF : numSigmas | uniformPDF : symmetry )
	variableDef attributes:
name
	    A UNICODE name for the variable (may be same as the
	      varID).
varIDAn XML-legal name that is unique within the file.
unitsThe units-of-measure for the signal.
axisSystemAn optional indicator of the axis system (body, inertial, etc.) in which the signal is measured. See Conventions below for best recommended practice for nomenclature.
signAn optional indicator of which direction is considered positive (+RWD, +UP, etc.). See the section on Conventions below, for best recommended practice for abbreviations.
symbolA UNICODE Greek symbol for the signal [to be superseded with more formal MathML or TeX element in a later release].
initialValueAn optional initial value for the parameter. This is normally specified for constant parameters only.
	    variableDef sub-elements:
	  
descriptionAn optional text description of the variable.
calculationAn optional container for the MathML content markup that
	      describes how this variable is calculated from other variables or function table
	      outputs. This element contains a single math element which is
	      defined in the MathML 2 markup
	      language.
isOutputThis optional element, if present, identifies this variable needs to be passed
	      as an output. How this is accomplished is up to the implementer. Unless specified by
	      this element, a variable is considered an output only if it is the result of a
	      calculation or function AND is not used elsewhere in this DAVEfunc model.
isStdAIAAThis optional element, if present, signifies that this variable is one of the standard AIAA simulation variable names that are defined in the (draft) AIAA Simulation Standard Variable Names [AIAA01]. Such identification should make it easier for the importing application to hook up this variable (probably an input or output of the model) to the appropriate importing facility's signal.
uncertainty
		This optional element, if present, describes the uncertainty of this parameter. See
		the section on Statistics below for more
		information about this element. Note that the uncertainty
		sub-element makes sense only for constant parameters (e.g., those with no
		calculation element but with an initialValue
		specified.
	      
Example 2. Two examples of variableDef elements defining input signals
            In the example below, two input variables are defined: XMACH and
            DBFLL. These two variables are inputs to a table lookup function
            shown in example 10 below.
          
<!--                     ==========================                     -->
<!-- ====================   VARIABLE DEFINITIONS   ==================== -->
<!--                     ==========================                     -->
      <!-- ================== -->
      <!--  Input variables   -->
      <!-- ================== -->
  <variableDef name="MachNumber" varID="XMACH"
 varID="XMACH" units="" symbol="M">
    <description>
 units="" symbol="M">
    <description>  Mach number (dimensionless) 
    </description>
  </variableDef>
  <variableDef name="dbfll" varID="DBFLL" units="deg"
        Mach number (dimensionless) 
    </description>
  </variableDef>
  <variableDef name="dbfll" varID="DBFLL" units="deg" sign="+TED"
 sign="+TED" symbol="δbfll"
 
                symbol="δbfll" >
    <description>
        Lower left body flap deflection, deg, +TED (so deflections are
        always zero or positive).
    </description>
    <isStdAIAA/>
>
    <description>
        Lower left body flap deflection, deg, +TED (so deflections are
        always zero or positive).
    </description>
    <isStdAIAA/> </variableDef>
  </variableDef>
	  |   | The  | 
|   | The  | 
|   | The  | 
|   | The optional  | 
|   | The optional  | 
|   | The optional  | 
|   | The optional  | 
Example 3. A simple local variable
            This example defines CRBFLLO which is the "independent variable"
            output from the table lookup function shown in example 10 below.
          
      <!-- ================== -->
      <!--  Local variables   -->
      <!-- ================== -->
<!-- PRELIMINARY BUILDUP EQUATIONS -->
<!--  LOWER LEFT BODY FLAP CONTRIBUTIONS -->
<!--    table output signal   -->
  <variableDef name="Cldbfll_0" varID="CRBFLL0" units="">
    <description>
        Output of CRBFLL0 function; rolling moment contribution of
        lower left body flap deflection due to alpha^0 (constant
        term).
    </description>
  </variableDef>
	  Example 4. A more complete example using a calculation element
	    Here the local variable CLBFLL is defined as a calculated quantity,
	    based on several other input or local variables (not shown). Note the description element is used to
	    describe the equation, in FORTRANish human-readable text. The calculation element describes this
	    same equation in MathML 2 content markup syntax; this portion should be used by
	    parsing applications to create either source code, documentation, or run-time
	    calculation structures.
	  
<!--    lower left body flap lift buildup -->
  <variableDef name="CLdbfll" varID="CLBFLL" units="">
    <description>
        Lift contribution of lower left body flap deflection
        CLdbfll = CLdbfll_0 + alpha*(CLdbfll_1 + alpha*(CLdbfll_2 
                            + alpha*CLdbfll_3))  </description>
    <calculation>
    </description>
    <calculation>   <math>
        <apply>
      <math>
        <apply>   <plus/>
          <ci>CLBFLL0</ci>
          <apply>
            <times/>
            <ci>ALP</ci>
            <apply>
              <plus/>
              <ci>CLBFLL1</ci>
              <apply>
                <times/>
                <ci>ALP</ci>
                <apply>
                  <plus/>
                  <ci>CLBFLL2</ci>
                  <apply>
        <plus/>
          <ci>CLBFLL0</ci>
          <apply>
            <times/>
            <ci>ALP</ci>
            <apply>
              <plus/>
              <ci>CLBFLL1</ci>
              <apply>
                <times/>
                <ci>ALP</ci>
                <apply>
                  <plus/>
                  <ci>CLBFLL2</ci>
                  <apply>  <times/>
                    <ci>ALP</ci>
                    <ci>CLBFLL3</ci>
                  </apply> <!--            a*c3   -->
                    <times/>
                    <ci>ALP</ci>
                    <ci>CLBFLL3</ci>
                  </apply> <!--            a*c3   -->   </apply> <!--        (c2 + a*c3)  -->
              </apply> <!--        a*(c2 + a*c3)  -->
            </apply> <!--    (c1 + a*(c2 + a*c3)) -->
          </apply> <!--    a*(c1 + a*(c2 + a*c3)) -->
        </apply> <!-- c0 + a*(c1 + a*(c2 + a*c3)) -->
      </math>
    </calculation>
  </variableDef>
                </apply> <!--        (c2 + a*c3)  -->
              </apply> <!--        a*(c2 + a*c3)  -->
            </apply> <!--    (c1 + a*(c2 + a*c3)) -->
          </apply> <!--    a*(c1 + a*(c2 + a*c3)) -->
        </apply> <!-- c0 + a*(c1 + a*(c2 + a*c3)) -->
      </math>
    </calculation>
  </variableDef>
	  Example 5. An output variable based on another calculation element
            This is an example of how an output variable (CL) might be defined
            from previously calculated local variables (in this case, CL0,
            CLBFL, etc.).
          
      <!-- ================== -->
      <!--  Output variables  -->
      <!-- ================== -->
  <variableDef name="CL" varID="CL" units="" sign="+UP" symbol="CL">
    <description>
        Coefficient of lift
        CL = CL0 + CLBFUL + CLBFUR + CLBFLL + CLBFLR + 
                   CLWFL + CLWFR + CLRUD + CLGE + CLLG
    </description>
    <calculation>
      <math>
        <apply>  <plus/>
          <ci>CL0</ci>
          <ci>CLBFUL</ci>
          <ci>CLBFUR</ci>
          <ci>CLBFLL</ci>
          <ci>CLBFLR</ci>
          <ci>CLWFL</ci>
          <ci>CLWFR</ci>
          <ci>CLRUD</ci>
          <ci>CLGE</ci>
          <ci>CLLG</ci>
        </apply>
      </math>
    </calculation>
    <isOutput/>
          <plus/>
          <ci>CL0</ci>
          <ci>CLBFUL</ci>
          <ci>CLBFUR</ci>
          <ci>CLBFLL</ci>
          <ci>CLBFLR</ci>
          <ci>CLWFL</ci>
          <ci>CLWFR</ci>
          <ci>CLRUD</ci>
          <ci>CLGE</ci>
          <ci>CLLG</ci>
        </apply>
      </math>
    </calculation>
    <isOutput/>  </variableDef>
  </variableDef>
	  Example 6. An intermediate variable with a calculation element that uses a
	  DAVE-ML extension (atan2) to the standard MathML function set
	    In this example, we demonstrate a means to encode a non-standard MathML 2 math function,
	    atan2. The atan2 function is used often in C, C++, Java and other modeling languages and
	    has been added to the DAVE-ML standard by use of the MathML csymbol
	    element, specifically provided to allow extension of MathML for cases such as this.
	  
      <!-- ================== -->
      <!--    ATAN2 example   -->  <!-- ================== -->
  <variableDef name="Wind vector roll angle" varID="PHI" units="rad">
    <description>
      This encodes the equation PHI = atan2( tan(BETA), sin(ALPHA) ) where atan2
      is the two-argument arc tangent function from the ANSI C standard math
      library; the first argument represents the sine component and the second
      argument is the cosine component.
    </description>
    <calculation>
      <math>
        <apply>
          <csymbol definitionURL="http://daveml.nasa.gov/function_spaces.html#atan2"
                   encoding="text">
      <!-- ================== -->
  <variableDef name="Wind vector roll angle" varID="PHI" units="rad">
    <description>
      This encodes the equation PHI = atan2( tan(BETA), sin(ALPHA) ) where atan2
      is the two-argument arc tangent function from the ANSI C standard math
      library; the first argument represents the sine component and the second
      argument is the cosine component.
    </description>
    <calculation>
      <math>
        <apply>
          <csymbol definitionURL="http://daveml.nasa.gov/function_spaces.html#atan2"
                   encoding="text">   atan2
          </csymbol>
          <apply>
            <tan/>
            <ci>BETA</ci>
            atan2
          </csymbol>
          <apply>
            <tan/>
            <ci>BETA</ci>    </apply>
          <apply>
            <sin/>
            <ci>ALPHA</ci>
          </apply>
          <apply>
            <sin/>
            <ci>ALPHA</ci>   </apply>
        </apply> 
      </math>
    </calculation>
  </variableDef>
          </apply>
        </apply> 
      </math>
    </calculation>
  </variableDef>
	  |   | This example shows how to calculate wind roll angle, phi, from angle of attack and angle of sideslip; it comes from the Apollo aero data book [NAA64]. | 
|   | 
		The  | 
|   | 
		BETA would be the  | 
|   | 
		ALPHA would be the  |