F-8 aircraft - Revision history

FelixMueller at 08:29, 27 July 2016

2016-07-27T08:29:12Z

← Older revision		Revision as of 08:29, 27 July 2016
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	\|nx = 3		\|nx = 3
	\|nw = 1		\|nw = 1
			\|nc = 2
	\|nre = 6		\|nre = 6
	}}		}}

FelixMueller: /* Source Code */

2016-06-28T07:49:26Z

Source Code

← Older revision		Revision as of 07:49, 28 June 2016
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	Model descriptions are available in		Model descriptions are available in

	* [[:Category:AMPL \| AMPL]] at [[F-8 aircraft (AMPL)]]		* [[:Category:AMPL \| AMPL code]] at [[F-8 aircraft (AMPL)]]
	* [[:Category:Muscod \| Muscod code]] at [[F-8 aircraft (Muscod)]]		* [[:Category:Muscod \| Muscod code]] at [[F-8 aircraft (Muscod)]]
	* [[:Category:optimica \| optimica]] at [[F-8 aircraft (optimica)]]		* [[:Category:JModelica \| JModelica code]] at [[F-8 aircraft (JModelica)]]
	* [[:Category:JModelica \| JModelica]] at [[F-8 aircraft (JModelica)]]

	== Variants ==		== Variants ==

FelixMueller: /* Optimica */

2016-04-17T09:46:40Z

Optimica

← Older revision		Revision as of 09:46, 17 April 2016
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	</gallery>		</gallery>

	=== ~~Optimica~~ ===		=== jModelica ===

	Objective : 5.12799232		Objective : 5.12799232

MadeleineSchroeter at 12:38, 15 March 2016

2016-03-15T12:38:45Z

← Older revision		Revision as of 12:38, 15 March 2016
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	* [[:Category:Muscod \| Muscod code]] at [[F-8 aircraft (Muscod)]]		* [[:Category:Muscod \| Muscod code]] at [[F-8 aircraft (Muscod)]]
	* [[:Category:optimica \| optimica]] at [[F-8 aircraft (optimica)]]		* [[:Category:optimica \| optimica]] at [[F-8 aircraft (optimica)]]
			* [[:Category:JModelica \| JModelica]] at [[F-8 aircraft (JModelica)]]

	== Variants ==		== Variants ==

SebastianSager: Moved C to Muscod

2016-01-28T09:17:15Z

Moved C to Muscod

← Older revision		Revision as of 09:17, 28 January 2016
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	* [[:Category:AMPL \| AMPL]] at [[F-8 aircraft (AMPL)]]		* [[:Category:AMPL \| AMPL]] at [[F-8 aircraft (AMPL)]]
	* [[:Category:C \| C code]] at [[F-8 aircraft (C)]]		* [[:Category:Muscod \| Muscod code]] at [[F-8 aircraft (Muscod)]]
	* [[:Category:optimica \| optimica]] at [[F-8 aircraft (optimica)]]		* [[:Category:optimica \| optimica]] at [[F-8 aircraft (optimica)]]

FelixMueller at 17:20, 27 January 2016

2016-01-27T17:20:10Z

← Older revision		Revision as of 17:20, 27 January 2016
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	[[Category:Aeronautics]]		[[Category:Aeronautics]]
	[[Category:Outer convexification]]		[[Category:Outer convexification]]
			[[Category: Minimum time]]

JonasSchulze: Text replacement - "\(.*)\<\/bibref\>" to ""

2015-12-30T20:32:10Z

Text replacement - "\<bibref\>(.*)\<\/bibref\>" to "<bib id="$1" />"

← Older revision		Revision as of 20:32, 30 December 2015
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	</math>		</math>

	<math>x_0</math> is the angle of attack in radians, <math>x_1</math> is the pitch angle, <math>x_2</math> is the pitch rate in rad/s, and the control function <math>w = w(t)</math> is the tail deflection angle in radians. This model goes back to Garrard<~~bibref>~~Garrard1977</~~bibref~~>.		<math>x_0</math> is the angle of attack in radians, <math>x_1</math> is the pitch angle, <math>x_2</math> is the pitch rate in rad/s, and the control function <math>w = w(t)</math> is the tail deflection angle in radians. This model goes back to Garrard<bib id="Garrard1977" />.

	In the control problem, both initial and terminal values of the differential states are fixed.		In the control problem, both initial and terminal values of the differential states are fixed.
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	{\| border="1" align="center" cellpadding="5" cellspacing="0"		{\| border="1" align="center" cellpadding="5" cellspacing="0"
	\|- bgcolor=#c7c7c7		\|- bgcolor=#c7c7c7
	! Arc !! w(t) !! Lee et al.<~~bibref>~~Lee1997a</~~bibref~~> !! Kaya<~~bibref>~~Kaya2003</~~bibref~~> !! Sager<~~bibref>~~Sager2005</~~bibref~~> !! [[User:MartinSchlueter \| Schlueter]]/[[User:Matthias.gerdts \| Gerdts]] !! Sager		! Arc !! w(t) !! Lee et al.<bib id="Lee1997a" /> !! Kaya<bib id="Kaya2003" /> !! Sager<bib id="Sager2005" /> !! [[User:MartinSchlueter \| Schlueter]]/[[User:Matthias.gerdts \| Gerdts]] !! Sager
	\|-		\|-
	\| align=center \| 1 \|\| align=center \| 1 \|\| 0.00000 \|\| 0.10292 \|\| 0.10235 \|\| 0.0 \|\| 1.13492		\| align=center \| 1 \|\| align=center \| 1 \|\| 0.00000 \|\| 0.10292 \|\| 0.10235 \|\| 0.0 \|\| 1.13492
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	Image:f8aircraftRelaxedCoarse.png\| Locally optimal relaxed control on a coarse control discretization grid and corresponding differential states.		Image:f8aircraftRelaxedCoarse.png\| Locally optimal relaxed control on a coarse control discretization grid and corresponding differential states.
	Image:f8aircraftRelaxedFine.png\| Locally optimal relaxed control on a fine, adaptively chosen control discretization grid and corresponding differential states.		Image:f8aircraftRelaxedFine.png\| Locally optimal relaxed control on a fine, adaptively chosen control discretization grid and corresponding differential states.
	Image:f8aircraftInteger.png\| Integer control and corresponding differential states from Sager<~~bibref>~~Sager2005</~~bibref~~>.		Image:f8aircraftInteger.png\| Integer control and corresponding differential states from Sager<bib id="Sager2005" />.

	Image:f8aircraftSchlueter.png\| Integer control and corresponding differential states from [[User:MartinSchlueter \| Schlueter]]/[[User:Matthias.gerdts \| Gerdts]] solution.		Image:f8aircraftSchlueter.png\| Integer control and corresponding differential states from [[User:MartinSchlueter \| Schlueter]]/[[User:Matthias.gerdts \| Gerdts]] solution.
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	== Miscellaneous and Further Reading ==		== Miscellaneous and Further Reading ==
	See <~~bibref>~~Kaya2003</~~bibref~~> and <~~bibref>~~Sager2005</~~bibref~~> for details.		See <bib id="Kaya2003" /> and <bib id="Sager2005" /> for details.

	== References ==		== References ==

JonasSchulze: Text replacement - "" to ""

2015-12-30T20:28:26Z

Text replacement - "<bibreferences/>" to "<biblist />"

← Older revision		Revision as of 20:28, 30 December 2015
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	== References ==		== References ==
	<~~bibreferences~~/>		<biblist />

	<!--List of all categories this page is part of. List characterization of solution behavior, model properties, ore presence of implementation details (e.g., AMPL for AMPL model) here -->		<!--List of all categories this page is part of. List characterization of solution behavior, model properties, ore presence of implementation details (e.g., AMPL for AMPL model) here -->

SebastianSager at 14:57, 21 November 2010

2010-11-21T14:57:41Z

← Older revision		Revision as of 14:57, 21 November 2010
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	[[Category:ODE model]]		[[Category:ODE model]]
	[[Category:Aeronautics]]		[[Category:Aeronautics]]
			[[Category:Outer convexification]]

SebastianSager: Moved source code to special pages

2009-08-11T16:01:18Z

Moved source code to special pages

@@ Line 102: / Line 102: @@
 </gallery>
-== Source Code ==
+=== Optimica ===
 Objective     : 5.12799232
 infeasibility : 6.2235588037251599e-10
-<source lang="optimica">
+<gallery caption="Obtained solution plots" widths="240px" heights="167px" perrow="3">
-package F8_aircraft_pack
+Image:f8aircraft1.png| (Probably sub-)Optimal control.
-  optimization F8_aircraft_Opt (objective = tf,
+</gallery>
-    // The time is scaled so that the new
+== Source Code ==
-    der(x0)= tf*(-0.877*x0 + x2 - 0.088*x0*x2 + 0.47*x0^2 - 0.019*x1^2 -x0^2*x2 + 3.846*x0^3
+Model descriptions are available in
-  end F8_aircraft_Opt;
+* [[:Category:AMPL | AMPL]] at [[F-8 aircraft (AMPL)]]
+* [[:Category:C | C code]] at [[F-8 aircraft (C)]]
-end F8_aircraft_pack;
+* [[:Category:optimica | optimica]] at [[F-8 aircraft (optimica)]]
 == Variants ==