546 lines
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546 lines
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<a href="#pub-methods">Public Member Functions</a> |
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<a href="#pri-methods">Private Member Functions</a> |
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<a href="#pri-attribs">Private Attributes</a> |
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<a href="classEnvironment-members.html">List of all members</a> </div>
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<div class="headertitle"><div class="title">Environment Class Reference</div></div>
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<p>Models atmospheric and gravitational conditions for the flight simulation.
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<a href="#details">More...</a></p>
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<p><code>#include <<a class="el" href="Environment_8h_source.html">Environment.h</a>></code></p>
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<table class="memberdecls">
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<tr class="heading"><td colspan="2"><h2 class="groupheader"><a id="pub-methods" name="pub-methods"></a>
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Public Member Functions</h2></td></tr>
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<tr class="memitem:a91d044984a0fce83759a84ba1bbdf713" id="r_a91d044984a0fce83759a84ba1bbdf713"><td class="memItemLeft" align="right" valign="top"> </td><td class="memItemRight" valign="bottom"><a class="el" href="#a91d044984a0fce83759a84ba1bbdf713">Environment</a> (double surfacePressure, double surfaceTemperature, double launchAltitude)</td></tr>
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<tr class="memdesc:a91d044984a0fce83759a84ba1bbdf713"><td class="mdescLeft"> </td><td class="mdescRight">Constructs a new <a class="el" href="classEnvironment.html" title="Models atmospheric and gravitational conditions for the flight simulation.">Environment</a>. <br /></td></tr>
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<tr class="separator:a91d044984a0fce83759a84ba1bbdf713"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:a00d96c0851019b1d243719cab6407c33" id="r_a00d96c0851019b1d243719cab6407c33"><td class="memItemLeft" align="right" valign="top"> </td><td class="memItemRight" valign="bottom"><a class="el" href="#a00d96c0851019b1d243719cab6407c33">~Environment</a> ()=default</td></tr>
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<tr class="memdesc:a00d96c0851019b1d243719cab6407c33"><td class="mdescLeft"> </td><td class="mdescRight">Default destructor. <br /></td></tr>
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<tr class="separator:a00d96c0851019b1d243719cab6407c33"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:a8ab160ee6060f34c35e7914463c43f21" id="r_a8ab160ee6060f34c35e7914463c43f21"><td class="memItemLeft" align="right" valign="top">double </td><td class="memItemRight" valign="bottom"><a class="el" href="#a8ab160ee6060f34c35e7914463c43f21">getAirDensity</a> (double altitude) const</td></tr>
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<tr class="memdesc:a8ab160ee6060f34c35e7914463c43f21"><td class="mdescLeft"> </td><td class="mdescRight">Returns the atmospheric density at a given altitude. <br /></td></tr>
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<tr class="separator:a8ab160ee6060f34c35e7914463c43f21"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:a6b2ce5f1fde4781a58577e239b6f54d9" id="r_a6b2ce5f1fde4781a58577e239b6f54d9"><td class="memItemLeft" align="right" valign="top">double </td><td class="memItemRight" valign="bottom"><a class="el" href="#a6b2ce5f1fde4781a58577e239b6f54d9">getGravity</a> (double altitude) const</td></tr>
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<tr class="memdesc:a6b2ce5f1fde4781a58577e239b6f54d9"><td class="mdescLeft"> </td><td class="mdescRight">Returns the gravitational acceleration at a given altitude. <br /></td></tr>
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<tr class="separator:a6b2ce5f1fde4781a58577e239b6f54d9"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:a96eab8d5936110c7823aa5a5181f8379" id="r_a96eab8d5936110c7823aa5a5181f8379"><td class="memItemLeft" align="right" valign="top">double </td><td class="memItemRight" valign="bottom"><a class="el" href="#a96eab8d5936110c7823aa5a5181f8379">getSurfacePressure</a> () const</td></tr>
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<tr class="memdesc:a96eab8d5936110c7823aa5a5181f8379"><td class="mdescLeft"> </td><td class="mdescRight">Returns the surface pressure at launch site. <br /></td></tr>
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<tr class="separator:a96eab8d5936110c7823aa5a5181f8379"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:a3ceb9efe4e56139341007f537136424d" id="r_a3ceb9efe4e56139341007f537136424d"><td class="memItemLeft" align="right" valign="top">double </td><td class="memItemRight" valign="bottom"><a class="el" href="#a3ceb9efe4e56139341007f537136424d">getSurfaceTemperature</a> () const</td></tr>
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<tr class="memdesc:a3ceb9efe4e56139341007f537136424d"><td class="mdescLeft"> </td><td class="mdescRight">Returns the surface temperature at launch site. <br /></td></tr>
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<tr class="separator:a3ceb9efe4e56139341007f537136424d"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:aa6d85d2441c356543d4ca90836671952" id="r_aa6d85d2441c356543d4ca90836671952"><td class="memItemLeft" align="right" valign="top">double </td><td class="memItemRight" valign="bottom"><a class="el" href="#aa6d85d2441c356543d4ca90836671952">getLaunchAltitude</a> () const</td></tr>
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<tr class="memdesc:aa6d85d2441c356543d4ca90836671952"><td class="mdescLeft"> </td><td class="mdescRight">Returns the launch altitude above sea level. <br /></td></tr>
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<tr class="separator:aa6d85d2441c356543d4ca90836671952"><td class="memSeparator" colspan="2"> </td></tr>
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</table><table class="memberdecls">
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<tr class="heading"><td colspan="2"><h2 class="groupheader"><a id="pri-methods" name="pri-methods"></a>
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Private Member Functions</h2></td></tr>
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<tr class="memitem:a1f21151ddb88388efdb8a8e1da25aeb1" id="r_a1f21151ddb88388efdb8a8e1da25aeb1"><td class="memItemLeft" align="right" valign="top">double </td><td class="memItemRight" valign="bottom"><a class="el" href="#a1f21151ddb88388efdb8a8e1da25aeb1">getStandardTemperature</a> (double altitude) const</td></tr>
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<tr class="memdesc:a1f21151ddb88388efdb8a8e1da25aeb1"><td class="mdescLeft"> </td><td class="mdescRight">Internal method to compute standard atmosphere temperature at altitude. <br /></td></tr>
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<tr class="separator:a1f21151ddb88388efdb8a8e1da25aeb1"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:ad272c06b3036c8874e72ca064efee032" id="r_ad272c06b3036c8874e72ca064efee032"><td class="memItemLeft" align="right" valign="top">double </td><td class="memItemRight" valign="bottom"><a class="el" href="#ad272c06b3036c8874e72ca064efee032">getStandardPressure</a> (double altitude) const</td></tr>
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<tr class="memdesc:ad272c06b3036c8874e72ca064efee032"><td class="mdescLeft"> </td><td class="mdescRight">Internal method to compute standard atmosphere pressure at altitude. <br /></td></tr>
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<tr class="separator:ad272c06b3036c8874e72ca064efee032"><td class="memSeparator" colspan="2"> </td></tr>
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</table><table class="memberdecls">
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<tr class="heading"><td colspan="2"><h2 class="groupheader"><a id="pri-attribs" name="pri-attribs"></a>
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Private Attributes</h2></td></tr>
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<tr class="memitem:a6d359808d63f589eb3c88a6037cdc2d8" id="r_a6d359808d63f589eb3c88a6037cdc2d8"><td class="memItemLeft" align="right" valign="top">double </td><td class="memItemRight" valign="bottom"><a class="el" href="#a6d359808d63f589eb3c88a6037cdc2d8">surfacePressure_</a></td></tr>
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<tr class="memdesc:a6d359808d63f589eb3c88a6037cdc2d8"><td class="mdescLeft"> </td><td class="mdescRight">Surface pressure at launch site [Pa]. <br /></td></tr>
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<tr class="separator:a6d359808d63f589eb3c88a6037cdc2d8"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:acf71031f36ed46d8c51261186183a349" id="r_acf71031f36ed46d8c51261186183a349"><td class="memItemLeft" align="right" valign="top">double </td><td class="memItemRight" valign="bottom"><a class="el" href="#acf71031f36ed46d8c51261186183a349">surfaceTemperature_</a></td></tr>
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<tr class="memdesc:acf71031f36ed46d8c51261186183a349"><td class="mdescLeft"> </td><td class="mdescRight">Surface temperature at launch site [K]. <br /></td></tr>
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<tr class="separator:acf71031f36ed46d8c51261186183a349"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:a1ba78c99df011cb4e499e2d87313a9b7" id="r_a1ba78c99df011cb4e499e2d87313a9b7"><td class="memItemLeft" align="right" valign="top">double </td><td class="memItemRight" valign="bottom"><a class="el" href="#a1ba78c99df011cb4e499e2d87313a9b7">launchAltitude_</a></td></tr>
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<tr class="memdesc:a1ba78c99df011cb4e499e2d87313a9b7"><td class="mdescLeft"> </td><td class="mdescRight">Launch altitude above sea level [m]. <br /></td></tr>
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<tr class="separator:a1ba78c99df011cb4e499e2d87313a9b7"><td class="memSeparator" colspan="2"> </td></tr>
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</table>
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<a name="details" id="details"></a><h2 class="groupheader">Detailed Description</h2>
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<div class="textblock"><p>Models atmospheric and gravitational conditions for the flight simulation. </p>
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<p>The <a class="el" href="classEnvironment.html" title="Models atmospheric and gravitational conditions for the flight simulation.">Environment</a> class provides atmospheric properties (air density, pressure, temperature) and gravity based on altitude. Future versions may support wind models. </p>
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</div><h2 class="groupheader">Constructor & Destructor Documentation</h2>
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<a id="a91d044984a0fce83759a84ba1bbdf713" name="a91d044984a0fce83759a84ba1bbdf713"></a>
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<h2 class="memtitle"><span class="permalink"><a href="#a91d044984a0fce83759a84ba1bbdf713">◆ </a></span>Environment()</h2>
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<div class="memitem">
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<td class="memname">Environment::Environment </td>
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<td>(</td>
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<td class="paramtype">double</td> <td class="paramname"><span class="paramname"><em>surfacePressure</em></span>, </td>
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</tr>
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<td class="paramkey"></td>
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<td></td>
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<td class="paramtype">double</td> <td class="paramname"><span class="paramname"><em>surfaceTemperature</em></span>, </td>
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<td class="paramkey"></td>
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<td class="paramtype">double</td> <td class="paramname"><span class="paramname"><em>launchAltitude</em></span> )</td>
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</tr>
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</div><div class="memdoc">
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<p>Constructs a new <a class="el" href="classEnvironment.html" title="Models atmospheric and gravitational conditions for the flight simulation.">Environment</a>. </p>
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<dl class="params"><dt>Parameters</dt><dd>
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<table class="params">
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<tr><td class="paramname">surfacePressure</td><td>Surface pressure at launch site (Pascals). </td></tr>
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<tr><td class="paramname">surfaceTemperature</td><td>Surface temperature at launch site (Kelvin). </td></tr>
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<tr><td class="paramname">launchAltitude</td><td>Launch site altitude (meters above sea level). </td></tr>
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</table>
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</dd>
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</dl>
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<a id="a00d96c0851019b1d243719cab6407c33" name="a00d96c0851019b1d243719cab6407c33"></a>
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<h2 class="memtitle"><span class="permalink"><a href="#a00d96c0851019b1d243719cab6407c33">◆ </a></span>~Environment()</h2>
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<td class="memname">Environment::~Environment </td>
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<td>(</td>
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<td class="paramname"><span class="paramname"><em></em></span></td><td>)</td>
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<td></td>
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<span class="mlabels"><span class="mlabel default">default</span></span> </td>
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<p>Default destructor. </p>
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</div>
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</div>
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<h2 class="groupheader">Member Function Documentation</h2>
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<a id="a8ab160ee6060f34c35e7914463c43f21" name="a8ab160ee6060f34c35e7914463c43f21"></a>
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<h2 class="memtitle"><span class="permalink"><a href="#a8ab160ee6060f34c35e7914463c43f21">◆ </a></span>getAirDensity()</h2>
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<td class="memname">double Environment::getAirDensity </td>
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<td>(</td>
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<td class="paramtype">double</td> <td class="paramname"><span class="paramname"><em>altitude</em></span></td><td>)</td>
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<td> const</td>
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<p>Returns the atmospheric density at a given altitude. </p>
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<dl class="params"><dt>Parameters</dt><dd>
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<table class="params">
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<tr><td class="paramname">altitude</td><td>Altitude above sea level (meters). </td></tr>
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</dd>
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</dl>
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<dl class="section return"><dt>Returns</dt><dd>Air density in kg/m3. </dd></dl>
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Here is the call graph for this function:</div>
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<div class="center"><img src="classEnvironment_a8ab160ee6060f34c35e7914463c43f21_cgraph.png" border="0" usemap="#aclassEnvironment_a8ab160ee6060f34c35e7914463c43f21_cgraph" alt=""/></div>
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<h2 class="memtitle"><span class="permalink"><a href="#a6b2ce5f1fde4781a58577e239b6f54d9">◆ </a></span>getGravity()</h2>
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<td class="memname">double Environment::getGravity </td>
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<td>(</td>
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<td class="paramtype">double</td> <td class="paramname"><span class="paramname"><em>altitude</em></span></td><td>)</td>
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<p>Returns the gravitational acceleration at a given altitude. </p>
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<dl class="params"><dt>Parameters</dt><dd>
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<table class="params">
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<tr><td class="paramname">altitude</td><td>Altitude above sea level (meters). </td></tr>
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<dl class="section return"><dt>Returns</dt><dd>Gravitational acceleration in m/s2. </dd></dl>
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<h2 class="memtitle"><span class="permalink"><a href="#aa6d85d2441c356543d4ca90836671952">◆ </a></span>getLaunchAltitude()</h2>
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<td class="memname">double Environment::getLaunchAltitude </td>
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<p>Returns the launch altitude above sea level. </p>
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<dl class="section return"><dt>Returns</dt><dd>Altitude in meters. </dd></dl>
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<h2 class="memtitle"><span class="permalink"><a href="#ad272c06b3036c8874e72ca064efee032">◆ </a></span>getStandardPressure()</h2>
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<td class="memname">double Environment::getStandardPressure </td>
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<td class="paramtype">double</td> <td class="paramname"><span class="paramname"><em>altitude</em></span></td><td>)</td>
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<span class="mlabels"><span class="mlabel private">private</span></span> </td>
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<p>Internal method to compute standard atmosphere pressure at altitude. </p>
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<dl class="params"><dt>Parameters</dt><dd>
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<table class="params">
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<tr><td class="paramname">altitude</td><td>Altitude above sea level (meters). </td></tr>
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<dl class="section return"><dt>Returns</dt><dd>Pressure at altitude (Pascals). </dd></dl>
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<h2 class="memtitle"><span class="permalink"><a href="#a1f21151ddb88388efdb8a8e1da25aeb1">◆ </a></span>getStandardTemperature()</h2>
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<td class="memname">double Environment::getStandardTemperature </td>
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<td class="paramtype">double</td> <td class="paramname"><span class="paramname"><em>altitude</em></span></td><td>)</td>
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<span class="mlabels"><span class="mlabel private">private</span></span> </td>
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<p>Internal method to compute standard atmosphere temperature at altitude. </p>
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<dl class="params"><dt>Parameters</dt><dd>
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<table class="params">
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<tr><td class="paramname">altitude</td><td>Altitude above sea level (meters). </td></tr>
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<dl class="section return"><dt>Returns</dt><dd>Temperature at altitude (Kelvin). </dd></dl>
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<h2 class="memtitle"><span class="permalink"><a href="#a96eab8d5936110c7823aa5a5181f8379">◆ </a></span>getSurfacePressure()</h2>
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<td class="memname">double Environment::getSurfacePressure </td>
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<p>Returns the surface pressure at launch site. </p>
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<dl class="section return"><dt>Returns</dt><dd>Pressure in Pascals. </dd></dl>
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<h2 class="memtitle"><span class="permalink"><a href="#a3ceb9efe4e56139341007f537136424d">◆ </a></span>getSurfaceTemperature()</h2>
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<p>Returns the surface temperature at launch site. </p>
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<dl class="section return"><dt>Returns</dt><dd>Temperature in Kelvin. </dd></dl>
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<h2 class="groupheader">Member Data Documentation</h2>
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<a id="a1ba78c99df011cb4e499e2d87313a9b7" name="a1ba78c99df011cb4e499e2d87313a9b7"></a>
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<h2 class="memtitle"><span class="permalink"><a href="#a1ba78c99df011cb4e499e2d87313a9b7">◆ </a></span>launchAltitude_</h2>
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<p>Launch altitude above sea level [m]. </p>
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<h2 class="memtitle"><span class="permalink"><a href="#a6d359808d63f589eb3c88a6037cdc2d8">◆ </a></span>surfacePressure_</h2>
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<p>Surface pressure at launch site [Pa]. </p>
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<h2 class="memtitle"><span class="permalink"><a href="#acf71031f36ed46d8c51261186183a349">◆ </a></span>surfaceTemperature_</h2>
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<p>Surface temperature at launch site [K]. </p>
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<hr/>The documentation for this class was generated from the following files:<ul>
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<li>include/<a class="el" href="Environment_8h_source.html">Environment.h</a></li>
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<li>src/<a class="el" href="Environment_8cpp.html">Environment.cpp</a></li>
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