756 lines
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756 lines
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<a href="#pub-methods">Public Member Functions</a> |
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<a href="#pri-attribs">Private Attributes</a> |
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<div class="headertitle"><div class="title">Motor Class Reference</div></div>
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<p>Represents a rocket motor with thrust characteristics over time.
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<a href="#details">More...</a></p>
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<p><code>#include <<a class="el" href="Motor_8h_source.html">Motor.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:af5e02cef2ac226d6010f8fff41691525" id="r_af5e02cef2ac226d6010f8fff41691525"><td class="memItemLeft" align="right" valign="top"> </td><td class="memItemRight" valign="bottom"><a class="el" href="#af5e02cef2ac226d6010f8fff41691525">Motor</a> (const std::string &name, double initialPropellantMass, double totalImpulse)</td></tr>
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<tr class="memdesc:af5e02cef2ac226d6010f8fff41691525"><td class="mdescLeft"> </td><td class="mdescRight">Constructs a new <a class="el" href="classMotor.html" title="Represents a rocket motor with thrust characteristics over time.">Motor</a> with a given name and mass properties. <br /></td></tr>
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<tr class="separator:af5e02cef2ac226d6010f8fff41691525"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:a063b9cf447524451c905cc9f1ea67261" id="r_a063b9cf447524451c905cc9f1ea67261"><td class="memItemLeft" align="right" valign="top"> </td><td class="memItemRight" valign="bottom"><a class="el" href="#a063b9cf447524451c905cc9f1ea67261">~Motor</a> ()=default</td></tr>
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<tr class="memdesc:a063b9cf447524451c905cc9f1ea67261"><td class="mdescLeft"> </td><td class="mdescRight">Default destructor. <br /></td></tr>
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<tr class="separator:a063b9cf447524451c905cc9f1ea67261"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:aacfe43afae59ccf8de9333b97f20b496" id="r_aacfe43afae59ccf8de9333b97f20b496"><td class="memItemLeft" align="right" valign="top">void </td><td class="memItemRight" valign="bottom"><a class="el" href="#aacfe43afae59ccf8de9333b97f20b496">addThrustDataPoint</a> (double time, double thrust)</td></tr>
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<tr class="memdesc:aacfe43afae59ccf8de9333b97f20b496"><td class="mdescLeft"> </td><td class="mdescRight">Adds a thrust curve data point. <br /></td></tr>
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<tr class="separator:aacfe43afae59ccf8de9333b97f20b496"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:a84c88f99c6dcd106ff621d9bc86d86d2" id="r_a84c88f99c6dcd106ff621d9bc86d86d2"><td class="memItemLeft" align="right" valign="top">void </td><td class="memItemRight" valign="bottom"><a class="el" href="#a84c88f99c6dcd106ff621d9bc86d86d2">ignite</a> ()</td></tr>
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<tr class="memdesc:a84c88f99c6dcd106ff621d9bc86d86d2"><td class="mdescLeft"> </td><td class="mdescRight">Starts motor ignition (sets internal ignition time to zero). <br /></td></tr>
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<tr class="separator:a84c88f99c6dcd106ff621d9bc86d86d2"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:aff6dc2a5d1b86043c3670d5d126fabe0" id="r_aff6dc2a5d1b86043c3670d5d126fabe0"><td class="memItemLeft" align="right" valign="top">void </td><td class="memItemRight" valign="bottom"><a class="el" href="#aff6dc2a5d1b86043c3670d5d126fabe0">update</a> (double deltaTime)</td></tr>
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<tr class="memdesc:aff6dc2a5d1b86043c3670d5d126fabe0"><td class="mdescLeft"> </td><td class="mdescRight">Updates the motor status based on elapsed time. <br /></td></tr>
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<tr class="separator:aff6dc2a5d1b86043c3670d5d126fabe0"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:a2dc32cd5990b69f58b4a2441615a2482" id="r_a2dc32cd5990b69f58b4a2441615a2482"><td class="memItemLeft" align="right" valign="top">double </td><td class="memItemRight" valign="bottom"><a class="el" href="#a2dc32cd5990b69f58b4a2441615a2482">getCurrentThrust</a> () const</td></tr>
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<tr class="memdesc:a2dc32cd5990b69f58b4a2441615a2482"><td class="mdescLeft"> </td><td class="mdescRight">Gets the current thrust output. <br /></td></tr>
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<tr class="separator:a2dc32cd5990b69f58b4a2441615a2482"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:a48d0d93602b089fce9bc24a469ef1a3a" id="r_a48d0d93602b089fce9bc24a469ef1a3a"><td class="memItemLeft" align="right" valign="top">bool </td><td class="memItemRight" valign="bottom"><a class="el" href="#a48d0d93602b089fce9bc24a469ef1a3a">isBurnedOut</a> () const</td></tr>
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<tr class="memdesc:a48d0d93602b089fce9bc24a469ef1a3a"><td class="mdescLeft"> </td><td class="mdescRight">Checks whether the motor has burned out. <br /></td></tr>
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<tr class="separator:a48d0d93602b089fce9bc24a469ef1a3a"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:aefeec4b2190b66d7f0131f91746c05d1" id="r_aefeec4b2190b66d7f0131f91746c05d1"><td class="memItemLeft" align="right" valign="top">double </td><td class="memItemRight" valign="bottom"><a class="el" href="#aefeec4b2190b66d7f0131f91746c05d1">getRemainingPropellantMass</a> () const</td></tr>
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<tr class="memdesc:aefeec4b2190b66d7f0131f91746c05d1"><td class="mdescLeft"> </td><td class="mdescRight">Returns the remaining propellant mass. <br /></td></tr>
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<tr class="separator:aefeec4b2190b66d7f0131f91746c05d1"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:a5bbe913797a4890d917fdfbd055fd7be" id="r_a5bbe913797a4890d917fdfbd055fd7be"><td class="memItemLeft" align="right" valign="top">const std::string & </td><td class="memItemRight" valign="bottom"><a class="el" href="#a5bbe913797a4890d917fdfbd055fd7be">getName</a> () const</td></tr>
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<tr class="memdesc:a5bbe913797a4890d917fdfbd055fd7be"><td class="mdescLeft"> </td><td class="mdescRight">Gets the name of the motor. <br /></td></tr>
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<tr class="separator:a5bbe913797a4890d917fdfbd055fd7be"><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:ab8cd621406d2641b8e0f2961323c65b8" id="r_ab8cd621406d2641b8e0f2961323c65b8"><td class="memItemLeft" align="right" valign="top">double </td><td class="memItemRight" valign="bottom"><a class="el" href="#ab8cd621406d2641b8e0f2961323c65b8">interpolateThrust</a> (double time) const</td></tr>
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<tr class="memdesc:ab8cd621406d2641b8e0f2961323c65b8"><td class="mdescLeft"> </td><td class="mdescRight">Linearly interpolates thrust from the thrust curve. <br /></td></tr>
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<tr class="separator:ab8cd621406d2641b8e0f2961323c65b8"><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:af28ab39a0f1fae7bab69f6a0b6721dbc" id="r_af28ab39a0f1fae7bab69f6a0b6721dbc"><td class="memItemLeft" align="right" valign="top">std::string </td><td class="memItemRight" valign="bottom"><a class="el" href="#af28ab39a0f1fae7bab69f6a0b6721dbc">name_</a></td></tr>
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<tr class="memdesc:af28ab39a0f1fae7bab69f6a0b6721dbc"><td class="mdescLeft"> </td><td class="mdescRight">Name of the motor. <br /></td></tr>
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<tr class="separator:af28ab39a0f1fae7bab69f6a0b6721dbc"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:af4203ea6011fe07e34a49597803874bc" id="r_af4203ea6011fe07e34a49597803874bc"><td class="memItemLeft" align="right" valign="top">double </td><td class="memItemRight" valign="bottom"><a class="el" href="#af4203ea6011fe07e34a49597803874bc">initialPropellantMass_</a></td></tr>
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<tr class="memdesc:af4203ea6011fe07e34a49597803874bc"><td class="mdescLeft"> </td><td class="mdescRight">Initial propellant mass [kg]. <br /></td></tr>
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<tr class="separator:af4203ea6011fe07e34a49597803874bc"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:a962d098d64f48d6025a49ad5c7b8c265" id="r_a962d098d64f48d6025a49ad5c7b8c265"><td class="memItemLeft" align="right" valign="top">double </td><td class="memItemRight" valign="bottom"><a class="el" href="#a962d098d64f48d6025a49ad5c7b8c265">remainingPropellantMass_</a></td></tr>
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<tr class="memdesc:a962d098d64f48d6025a49ad5c7b8c265"><td class="mdescLeft"> </td><td class="mdescRight">Current propellant mass [kg]. <br /></td></tr>
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<tr class="separator:a962d098d64f48d6025a49ad5c7b8c265"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:aff81edcd784fc32bcdf2b663ca1b245c" id="r_aff81edcd784fc32bcdf2b663ca1b245c"><td class="memItemLeft" align="right" valign="top">double </td><td class="memItemRight" valign="bottom"><a class="el" href="#aff81edcd784fc32bcdf2b663ca1b245c">totalImpulse_</a></td></tr>
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<tr class="memdesc:aff81edcd784fc32bcdf2b663ca1b245c"><td class="mdescLeft"> </td><td class="mdescRight">Total impulse [Ns], used for sanity checks. <br /></td></tr>
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<tr class="separator:aff81edcd784fc32bcdf2b663ca1b245c"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:adb6c324afea4c2e17064fdb7709dfe67" id="r_adb6c324afea4c2e17064fdb7709dfe67"><td class="memItemLeft" align="right" valign="top">std::vector< std::pair< double, double > > </td><td class="memItemRight" valign="bottom"><a class="el" href="#adb6c324afea4c2e17064fdb7709dfe67">thrustCurve_</a></td></tr>
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<tr class="memdesc:adb6c324afea4c2e17064fdb7709dfe67"><td class="mdescLeft"> </td><td class="mdescRight">Thrust curve (time, thrust) points. <br /></td></tr>
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<tr class="separator:adb6c324afea4c2e17064fdb7709dfe67"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:a12ac86c4706de3886f7a579f7d54555a" id="r_a12ac86c4706de3886f7a579f7d54555a"><td class="memItemLeft" align="right" valign="top">double </td><td class="memItemRight" valign="bottom"><a class="el" href="#a12ac86c4706de3886f7a579f7d54555a">ignitionTime_</a></td></tr>
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<tr class="memdesc:a12ac86c4706de3886f7a579f7d54555a"><td class="mdescLeft"> </td><td class="mdescRight">Elapsed time since ignition [s]. <br /></td></tr>
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<tr class="separator:a12ac86c4706de3886f7a579f7d54555a"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:a36b00ad7f46dfb1ee0ad5d1d6d173801" id="r_a36b00ad7f46dfb1ee0ad5d1d6d173801"><td class="memItemLeft" align="right" valign="top">bool </td><td class="memItemRight" valign="bottom"><a class="el" href="#a36b00ad7f46dfb1ee0ad5d1d6d173801">ignited_</a></td></tr>
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<tr class="memdesc:a36b00ad7f46dfb1ee0ad5d1d6d173801"><td class="mdescLeft"> </td><td class="mdescRight">Whether the motor has been ignited. <br /></td></tr>
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<tr class="separator:a36b00ad7f46dfb1ee0ad5d1d6d173801"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:a2e3d871b3ba8213170d3649fb2418466" id="r_a2e3d871b3ba8213170d3649fb2418466"><td class="memItemLeft" align="right" valign="top">bool </td><td class="memItemRight" valign="bottom"><a class="el" href="#a2e3d871b3ba8213170d3649fb2418466">burnedOut_</a></td></tr>
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<tr class="memdesc:a2e3d871b3ba8213170d3649fb2418466"><td class="mdescLeft"> </td><td class="mdescRight">Whether the motor has finished burning. <br /></td></tr>
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<tr class="separator:a2e3d871b3ba8213170d3649fb2418466"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:aa92df0cbc929f46a0b45ef733be45db5" id="r_aa92df0cbc929f46a0b45ef733be45db5"><td class="memItemLeft" align="right" valign="top">double </td><td class="memItemRight" valign="bottom"><a class="el" href="#aa92df0cbc929f46a0b45ef733be45db5">currentThrust_</a></td></tr>
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<tr class="memdesc:aa92df0cbc929f46a0b45ef733be45db5"><td class="mdescLeft"> </td><td class="mdescRight">Cached current thrust [N]. <br /></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>Represents a rocket motor with thrust characteristics over time. </p>
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<p>The <a class="el" href="classMotor.html" title="Represents a rocket motor with thrust characteristics over time.">Motor</a> class manages the thrust curve, ignition timing, burn duration, and remaining propellant mass of a single propulsion unit. </p>
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</div><h2 class="groupheader">Constructor & Destructor Documentation</h2>
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<a id="af5e02cef2ac226d6010f8fff41691525" name="af5e02cef2ac226d6010f8fff41691525"></a>
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<h2 class="memtitle"><span class="permalink"><a href="#af5e02cef2ac226d6010f8fff41691525">◆ </a></span>Motor()</h2>
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<div class="memitem">
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<td class="memname">Motor::Motor </td>
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<td>(</td>
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<td class="paramtype">const std::string &</td> <td class="paramname"><span class="paramname"><em>name</em></span>, </td>
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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>initialPropellantMass</em></span>, </td>
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<td class="paramtype">double</td> <td class="paramname"><span class="paramname"><em>totalImpulse</em></span> )</td>
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<p>Constructs a new <a class="el" href="classMotor.html" title="Represents a rocket motor with thrust characteristics over time.">Motor</a> with a given name and mass properties. </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">name</td><td>Name of the motor. </td></tr>
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<tr><td class="paramname">initialPropellantMass</td><td>Initial mass of propellant (kg). </td></tr>
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<tr><td class="paramname">totalImpulse</td><td>Total impulse (Ns) for basic verification. </td></tr>
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</table>
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</dd>
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</dl>
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<h2 class="memtitle"><span class="permalink"><a href="#a063b9cf447524451c905cc9f1ea67261">◆ </a></span>~Motor()</h2>
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<td class="memname">Motor::~Motor </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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<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="aacfe43afae59ccf8de9333b97f20b496" name="aacfe43afae59ccf8de9333b97f20b496"></a>
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<h2 class="memtitle"><span class="permalink"><a href="#aacfe43afae59ccf8de9333b97f20b496">◆ </a></span>addThrustDataPoint()</h2>
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<td class="memname">void Motor::addThrustDataPoint </td>
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<td>(</td>
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<td class="paramtype">double</td> <td class="paramname"><span class="paramname"><em>time</em></span>, </td>
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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>thrust</em></span> )</td>
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<p>Adds a thrust curve data point. </p>
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<p>Should be called during setup. Time must be monotonically increasing.</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">time</td><td>Time since ignition (seconds). </td></tr>
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<tr><td class="paramname">thrust</td><td>Thrust at this time (Newtons). </td></tr>
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</dd>
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<h2 class="memtitle"><span class="permalink"><a href="#a2dc32cd5990b69f58b4a2441615a2482">◆ </a></span>getCurrentThrust()</h2>
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<td class="memname">double Motor::getCurrentThrust </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> const</td>
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</div><div class="memdoc">
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<p>Gets the current thrust output. </p>
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<dl class="section return"><dt>Returns</dt><dd>Current thrust in Newtons. </dd></dl>
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<h2 class="memtitle"><span class="permalink"><a href="#a5bbe913797a4890d917fdfbd055fd7be">◆ </a></span>getName()</h2>
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<td class="memname">const std::string & Motor::getName </td>
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<td>(</td>
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<td> const</td>
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</div><div class="memdoc">
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<p>Gets the name of the motor. </p>
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<dl class="section return"><dt>Returns</dt><dd><a class="el" href="classMotor.html" title="Represents a rocket motor with thrust characteristics over time.">Motor</a> name as a constant reference. </dd></dl>
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<a id="aefeec4b2190b66d7f0131f91746c05d1" name="aefeec4b2190b66d7f0131f91746c05d1"></a>
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<h2 class="memtitle"><span class="permalink"><a href="#aefeec4b2190b66d7f0131f91746c05d1">◆ </a></span>getRemainingPropellantMass()</h2>
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<td class="memname">double Motor::getRemainingPropellantMass </td>
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<td>(</td>
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<td> const</td>
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<p>Returns the remaining propellant mass. </p>
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<dl class="section return"><dt>Returns</dt><dd>Remaining propellant mass in kilograms. </dd></dl>
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<h2 class="memtitle"><span class="permalink"><a href="#a84c88f99c6dcd106ff621d9bc86d86d2">◆ </a></span>ignite()</h2>
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<td class="memname">void Motor::ignite </td>
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<td>(</td>
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<td></td>
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<p>Starts motor ignition (sets internal ignition time to zero). </p>
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<h2 class="memtitle"><span class="permalink"><a href="#ab8cd621406d2641b8e0f2961323c65b8">◆ </a></span>interpolateThrust()</h2>
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<td class="memname">double Motor::interpolateThrust </td>
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<td class="paramtype">double</td> <td class="paramname"><span class="paramname"><em>time</em></span></td><td>)</td>
|
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<td> const</td>
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</td>
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<td class="mlabels-right">
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<span class="mlabels"><span class="mlabel private">private</span></span> </td>
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</div><div class="memdoc">
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<p>Linearly interpolates thrust from the thrust curve. </p>
|
|
<dl class="params"><dt>Parameters</dt><dd>
|
|
<table class="params">
|
|
<tr><td class="paramname">time</td><td>Time since ignition (seconds). </td></tr>
|
|
</table>
|
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</dd>
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<dl class="section return"><dt>Returns</dt><dd>Interpolated thrust (Newtons). </dd></dl>
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<h2 class="memtitle"><span class="permalink"><a href="#a48d0d93602b089fce9bc24a469ef1a3a">◆ </a></span>isBurnedOut()</h2>
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<p>Checks whether the motor has burned out. </p>
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<dl class="section return"><dt>Returns</dt><dd>True if burnout has occurred. </dd></dl>
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<h2 class="memtitle"><span class="permalink"><a href="#aff6dc2a5d1b86043c3670d5d126fabe0">◆ </a></span>update()</h2>
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<td class="memname">void Motor::update </td>
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<td class="paramtype">double</td> <td class="paramname"><span class="paramname"><em>deltaTime</em></span></td><td>)</td>
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</div><div class="memdoc">
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<p>Updates the motor status based on elapsed time. </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">deltaTime</td><td>Time step in seconds. </td></tr>
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<h2 class="groupheader">Member Data Documentation</h2>
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<a id="a2e3d871b3ba8213170d3649fb2418466" name="a2e3d871b3ba8213170d3649fb2418466"></a>
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<h2 class="memtitle"><span class="permalink"><a href="#a2e3d871b3ba8213170d3649fb2418466">◆ </a></span>burnedOut_</h2>
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|
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<span class="mlabels"><span class="mlabel private">private</span></span> </td>
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<p>Whether the motor has finished burning. </p>
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<h2 class="memtitle"><span class="permalink"><a href="#aa92df0cbc929f46a0b45ef733be45db5">◆ </a></span>currentThrust_</h2>
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<td class="memname">double Motor::currentThrust_</td>
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<p>Cached current thrust [N]. </p>
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<h2 class="memtitle"><span class="permalink"><a href="#a36b00ad7f46dfb1ee0ad5d1d6d173801">◆ </a></span>ignited_</h2>
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<p>Whether the motor has been ignited. </p>
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<h2 class="memtitle"><span class="permalink"><a href="#a12ac86c4706de3886f7a579f7d54555a">◆ </a></span>ignitionTime_</h2>
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<p>Elapsed time since ignition [s]. </p>
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<h2 class="memtitle"><span class="permalink"><a href="#af4203ea6011fe07e34a49597803874bc">◆ </a></span>initialPropellantMass_</h2>
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<p>Initial propellant mass [kg]. </p>
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<h2 class="memtitle"><span class="permalink"><a href="#af28ab39a0f1fae7bab69f6a0b6721dbc">◆ </a></span>name_</h2>
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<p>Name of the motor. </p>
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<h2 class="memtitle"><span class="permalink"><a href="#a962d098d64f48d6025a49ad5c7b8c265">◆ </a></span>remainingPropellantMass_</h2>
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<p>Current propellant mass [kg]. </p>
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<h2 class="memtitle"><span class="permalink"><a href="#adb6c324afea4c2e17064fdb7709dfe67">◆ </a></span>thrustCurve_</h2>
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<p>Thrust curve (time, thrust) points. </p>
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<h2 class="memtitle"><span class="permalink"><a href="#aff81edcd784fc32bcdf2b663ca1b245c">◆ </a></span>totalImpulse_</h2>
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<td class="memname">double Motor::totalImpulse_</td>
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<p>Total impulse [Ns], used for sanity checks. </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="Motor_8h_source.html">Motor.h</a></li>
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<li>src/<a class="el" href="Motor_8cpp.html">Motor.cpp</a></li>
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