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		<title>Hadjaz et al 2012b - Revision history</title>
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		<updated>2026-05-11T10:41:00Z</updated>
		<subtitle>Revision history for this page on the wiki</subtitle>
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		<id>http://www.colloquiam.com/wd/index.php?title=Hadjaz_et_al_2012b&amp;diff=204455&amp;oldid=prev</id>
		<title>Scipediacontent: Scipediacontent moved page Draft Content 956049043 to Hadjaz et al 2012b</title>
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				<updated>2021-02-03T15:11:25Z</updated>
		
		<summary type="html">&lt;p&gt;Scipediacontent moved page &lt;a href=&quot;/public/Draft_Content_956049043&quot; class=&quot;mw-redirect&quot; title=&quot;Draft Content 956049043&quot;&gt;Draft Content 956049043&lt;/a&gt; to &lt;a href=&quot;/public/Hadjaz_et_al_2012b&quot; title=&quot;Hadjaz et al 2012b&quot;&gt;Hadjaz et al 2012b&lt;/a&gt;&lt;/p&gt;
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				&lt;td colspan='1' style=&quot;background-color: white; color:black; text-align: center;&quot;&gt;← Older revision&lt;/td&gt;
				&lt;td colspan='1' style=&quot;background-color: white; color:black; text-align: center;&quot;&gt;Revision as of 15:11, 3 February 2021&lt;/td&gt;
				&lt;/tr&gt;&lt;tr&gt;&lt;td colspan='2' style='text-align: center;' lang='en'&gt;&lt;div class=&quot;mw-diff-empty&quot;&gt;(No difference)&lt;/div&gt;
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		<author><name>Scipediacontent</name></author>	</entry>

	<entry>
		<id>http://www.colloquiam.com/wd/index.php?title=Hadjaz_et_al_2012b&amp;diff=204454&amp;oldid=prev</id>
		<title>Scipediacontent: Created page with &quot; == Abstract ==  This paper presents a model based on an hybrid system to numerically simulate the climbing phase of an aircraft. This model is then used within a trajectory p...&quot;</title>
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				<updated>2021-02-03T15:11:22Z</updated>
		
		<summary type="html">&lt;p&gt;Created page with &amp;quot; == Abstract ==  This paper presents a model based on an hybrid system to numerically simulate the climbing phase of an aircraft. This model is then used within a trajectory p...&amp;quot;&lt;/p&gt;
&lt;p&gt;&lt;b&gt;New page&lt;/b&gt;&lt;/p&gt;&lt;div&gt;&lt;br /&gt;
== Abstract ==&lt;br /&gt;
&lt;br /&gt;
This paper presents a model based on an hybrid system to numerically simulate the climbing phase of an aircraft. This model is then used within a trajectory prediction tool. Finally, the Covariance Matrix Adaptation Evolution Strategy (CMA-ES) optimization algorithm is used to tune five selected parameters, and thus improve the accuracy of the model. Incorporated within a trajectory prediction tool, this model can be used to derive the order of magnitude of the prediction error over time, and thus the domain of validity of the trajectory prediction. A first validation experiment of the proposed model is based on the errors along time for a one-time trajectory prediction at the take off of the flight with respect to the default values of the theoretical BADA model. This experiment, assuming complete information, also shows the limit of the model. A second experiment part presents an on-line trajectory prediction, in which the prediction is continuously updated based on the current aircraft position. This approach raises several issues, for which improvements of the basic model are proposed, and the resulting trajectory prediction tool shows statistically significantly more accurate results than those of the default model.&lt;br /&gt;
&lt;br /&gt;
Comment: SESAR 2nd Innovation Days (2012)&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
== Original document ==&lt;br /&gt;
&lt;br /&gt;
The different versions of the original document can be found in:&lt;br /&gt;
&lt;br /&gt;
* [http://arxiv.org/abs/1212.3998 http://arxiv.org/abs/1212.3998]&lt;br /&gt;
&lt;br /&gt;
* [https://hal.inria.fr/hal-00766049 https://hal.inria.fr/hal-00766049],&lt;br /&gt;
: [https://hal.inria.fr/hal-00766049/document https://hal.inria.fr/hal-00766049/document],&lt;br /&gt;
: [https://hal.inria.fr/hal-00766049/file/opwpe.pdf https://hal.inria.fr/hal-00766049/file/opwpe.pdf]&lt;/div&gt;</summary>
		<author><name>Scipediacontent</name></author>	</entry>

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