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Integrated Design of Flight Control Surfaces and Laws for New Aircraft

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Integrated Design of Flight Control Surfaces and Laws for New Aircraft Integrated design of flight control surfaces and laws for new aircraft configurations Yann Denieul, Joël Bordeneuve-Guibé, Daniel Alazard, Clément Toussaint, Gilles Taquin To cite this version: Yann Denieul, Joël Bordeneuve-Guibé, Daniel Alazard, Clément Toussaint, Gilles Taquin. Integrated design of flight control surfaces and laws for new aircraft configurations. IFAC World Congress 2017, Jul 2017, Toulouse, France. pp. 14180-14187, 10.1016/j.ifacol.2017.08.2085. hal-01738089 HAL Id: hal-01738089 https://hal.archives-ouvertes.fr/hal-01738089 Submitted on 20 Mar 2018 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. an author's https://oatao.univ-toulouse.fr/19596 http://dx.doi.org/10.1016/j.ifacol.2017.08.2085 Denieul, Yann and Bordeneuve-Guibé, Joël and Alazard, Daniel and Toussaint, Clément and Taquin, Gilles Integrated design of flight control surfaces and laws for new aircraft configurations. (2017) In: IFAC World Congress 2017, 9 July 2017 - 14 July 2017 (Toulouse, France). Proceedings of the 20th World Congress Proceedings of the 20th World Congress ProceedingsThe International of the Federation 20th World of CongressAutomatic Control The International Federation of Automatic Control TheToulouse, International France, Federation July 9-14, 2017of Automatic Control Toulouse, France, July 9-14, 2017 Toulouse, France, July 9-14, 2017 Integrated design of flight control surfaces Integrated design of flight control surfaces and laws for new aircraft configurations and laws for new aircraft configurations Y. Denieul ∗ J. Bordeneuve-Guib´e ∗∗ D. Alazard ∗∗∗ Y. Denieul ∗ J. Bordeneuve-Guib´e ∗∗ D. Alazard ∗∗∗ Y. Denieul ∗C.J. Toussaint Bordeneuve-Guib´e∗∗∗∗ G. Taquin∗∗ D.† Alazard ∗∗∗ ∗C. Toussaint ∗∗∗∗ G. Taquin∗∗ † ∗∗∗ C. Toussaint ∗∗∗∗ G. Taquin † C. Toussaint ∗∗∗∗ G. Taquin † ∗ PhD Student, University of Toulouse, ISAE-SUPAERO, 10, Av. ∗ PhD Student, University of Toulouse, ISAE-SUPAERO, 10, Av. ∗ PhD Student,Edouard University Belin, of 31055 Toulouse, Toulouse ISAE-SUPAERO, FRANCE 10, Av. ∗ PhD Student,Edouard University Belin, of 31055 Toulouse, Toulouse ISAE-SUPAERO, FRANCE 10, Av. ∗∗ Associated Professor,Edouard Belin, University 31055 of Toulouse Toulouse, FRANCE ISAE-SUPAERO, 10, ∗∗ Associated Professor, University of Toulouse, ISAE-SUPAERO, 10, ∗∗ AssociatedAv. Professor, Edouard University Belin, 31055 of Toulouse,Toulouse FRANCE. ISAE-SUPAERO, 10, ∗∗ AssociatedAv. Professor, Edouard University Belin, 31055 of Toulouse,Toulouse FRANCE. ISAE-SUPAERO, 10, ∗∗∗ Professor,Av. Edouard University Belin, of Toulouse, 31055 Toulouse ISAE-SUPAERO, FRANCE. 10, Av. ∗∗∗ Professor, University of Toulouse, ISAE-SUPAERO, 10, Av. ∗∗∗ Professor,Edouard University Belin, of 31055 Toulouse, Toulouse ISAE-SUPAERO, FRANCE. 10, Av. ∗∗∗ Professor,Edouard University Belin, of 31055 Toulouse, Toulouse ISAE-SUPAERO, FRANCE. 10, Av. ∗∗∗∗ ResearchEdouard Engineer, Belin, ONERA, 31055 Toulouse 2, Av. Edouard FRANCE. Belin, 31055 ∗∗∗∗ Research Engineer, ONERA, 2, Av. Edouard Belin, 31055 ∗∗∗∗ Research Engineer,Toulouse ONERA, FRANCE. 2, Av. Edouard Belin, 31055 ∗∗∗∗ Research Engineer,Toulouse ONERA, FRANCE. 2, Av. Edouard Belin, 31055 † Handling Qualities Expert,Toulouse Airbus FRANCE. Op´erations SAS, 316 route de † Handling Qualities Expert, Airbus Op´erations SAS, 316 route de † Handling QualitiesBayonne, Expert, 31060 Airbus Toulouse Op´erations FRANCE. SAS, 316 route de † Handling QualitiesBayonne, Expert, 31060 Airbus Toulouse Op´erations FRANCE. SAS, 316 route de Bayonne, 31060 Toulouse FRANCE. Abstract: Control architecture sizing is a main challenge for new aircraft design like blended Abstract: Control architecture sizing is a main challenge for new aircraft design like blended Abstract:wing-body design.Control This architecture aircraft configuration sizing is a main typically challenge features for redundantnew aircraft elevons design located like blended at the wing-bodyAbstract: design.Control This architecture aircraft configuration sizing is a main typically challenge features for redundantnew aircraft elevons design located like blended at the wing-bodytrailing edge design. of the This wing, aircraft acting configurationsimultaneously typically on pitch features and roll redundant axes. The elevonsproblem located of integrated at the trailingwing-body edge design. of the This wing, aircraft acting configurationsimultaneously typically on pitch features and roll redundant axes. The elevonsproblem located of integrated at the trailingdesign of edge control of the surface wing, sizes acting and simultaneously flight control on laws pitch for and an unstable roll axes. blended The problem wing-body of integrated aircraft designtrailing of edge control of the surface wing, sizes acting and simultaneously flight control on laws pitch for and an unstable roll axes. blended The problem wing-body of integrated aircraft designis addressed of control here. surface Latest sizes tools and for flightH controlnon-smooth laws for optimization an unstable of blended structured wing-body controllers aircraft are isdesign addressed of control here. surface Latest sizes tools and for flightH∞ controlnon-smooth laws for optimization an unstable of blended structured wing-body controllers aircraft are isused addressed to optimize here. in Latest a single tools step for theH gains∞ non-smooth for both longitudinal optimization and of lateral structured control controllers laws, and are a isused addressed to optimize here. in Latest a single tools step for theH gains∞ non-smooth for both longitudinal optimization and of lateral structured control controllers laws, and are a controlused to allocationoptimize in module, a single while step the minimizing gains∞ for control both longitudinal surfaces total and span. lateral Following control laws, constraints and a controlused to allocationoptimize in module, a single while step the minimizing gains for control both longitudinal surfaces total and span. lateral Following control laws, constraints and a arecontrol ensured: allocation maximal module, deflection while angles minimizing and rates control for 1)surfaces pilot longitudinal total span. Following pull-up 2) constraints pilot bank arecontrol ensured: allocation maximal module, deflection while angles minimizing and rates control for 1)surfaces pilot longitudinal total span. Following pull-up 2) constraints pilot bank angleare ensured: order and maximal 3) longitudinal deflection angles turbulence. and rates Using for this 1) pilot coupled longitudinal approach, pull-up significant 2) pilot gains bank in angleare ensured: order and maximal 3) longitudinal deflection angles turbulence. and rates Using for this 1) pilot coupled longitudinal approach, pull-up significant 2) pilot gains bank in termsangleorder of outer and elevons 3) longitudinal span compared turbulence. to the Using initial this layout coupled are demonstrated, approach, significant while closed-loop gains in termsangleorder of outer and elevons 3) longitudinal span compared turbulence. to the Using initial this layout coupled are demonstrated, approach, significant while closed-loop gains in handlingterms of outer qualities elevons constraints span compared are guaranteed. to the initial layout are demonstrated, while closed-loop handlingterms of outer qualities elevons constraints span compared are guaranteed. to the initial layout are demonstrated, while closed-loop handling qualities constraints are guaranteed. Keywords: Integrated design, Flight Control Law, Aircraft, H control, Dynamics, BWB Keywords: Integrated design, Flight Control Law, Aircraft, H∞ control, Dynamics, BWB Keywords: Integrated design, Flight Control Law, Aircraft, H∞ control, Dynamics, BWB Keywords: Integrated design, Flight Control Law, Aircraft, H∞ control, Dynamics, BWB 1. INTRODUCTION already addressed∞ in a previous work Saucez and Boiffier 1. INTRODUCTION already addressed in a previous work Saucez and Boiffier 1. INTRODUCTION already(2012). addressed in a previous work Saucez and Boiffier (2012). Among other disruptive aircraft configurations, the Blended Then(2012). concerning control surfaces area sizing, two phenom- Among other disruptive aircraft configurations, the Blended Then concerning control surfaces area sizing, two phenom- AmongWing-Body other (BWB) disruptive was aircraft identified configurations, for years as a the promising Blended enaThen have concerning a combined control detrimental surfaces area effect sizing, both two on actuators phenom- Wing-Body (BWB) was identified for years as a promising enaThen have concerning a combined control detrimental surfaces area effect sizing, both two on actuators phenom- Wing-Bodycandidate for (BWB) the future was identified of civil aviation for years Liebeck as a promising (2004). massena have and a power combined consumption detrimental Roskam effect (1985). both on On actuators the one candidate for the future of civil aviation Liebeck (2004). massena have and a power combined consumption detrimental Roskam
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