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
).
varID
An XML-legal name that is unique within the file.
units
The units-of-measure for the signal.
axisSystem
An optional indicator of the axis system (body, inertial, etc.) in which the signal is measured. See Conventions below for best recommended practice for nomenclature.
sign
An optional indicator of which direction is considered positive (+RWD, +UP, etc.). See the section on Conventions below, for best recommended practice for abbreviations.
symbol
A UNICODE Greek symbol for the signal [to be superseded with more formal MathML or TeX element in a later release].
initialValue
An optional initial value for the parameter. This is normally specified for constant parameters only.
variableDef
sub-elements:
description
An optional text description of the variable.
calculation
An 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.
isOutput
This 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.
isStdAIAA
This 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" units="" symbol="M"> <description> Mach number (dimensionless) </description> </variableDef> <variableDef name="dbfll" varID="DBFLL" units="deg" sign="+TED" symbol="δbfll"> <description> Lower left body flap deflection, deg, +TED (so deflections are always zero or positive). </description> <isStdAIAA/> </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> <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> <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>
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/> </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"> atan2 </csymbol> <apply> <tan/> <ci>BETA</ci> </apply> <apply> <sin/> <ci>ALPHA</ci> </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 |