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Author: André Luís da Silva
Publisher: LAP Lambert Academic Publishing
ISBN: 9783659300417
Category :
Languages : en
Pages : 216
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Book Description
Every aircraft is a flexible body and its motion should be evaluated by the continuum mechanics. However, in the flight mechanics, they are commonly treated as rigid. In other way, in the structural dynamics scenario, rigid body modes are usually neglected. Such segregation is acceptable when sufficient separation exist between the frequencies of rigid and flexible modes. But, trends in the aircraft industry are leading to longer fuselages, larger aspect ratios, smaller thicknesses and the use of composite materials. Such configurations are more flexible and integrated models for flight mechanics and structural dynamics should be taken. This book develops the theme in a scenario of modelling, simulation and optimal control. Models of conceptual flexible aircraft are built in order to be used in control studies. A nonlinear optimal model following control is proposed. Linear solutions are developed, nonlinear approaches are also investigated, via neural networks. The technique is used to approximate the flexible aircraft as a rigid body, letting the job of controlling flexible modes to the automatic control, while an human or autopilot can see the aircraft as a usual rigid body.
Author: André Luís da Silva
Publisher: LAP Lambert Academic Publishing
ISBN: 9783659300417
Category :
Languages : en
Pages : 216
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Book Description
Every aircraft is a flexible body and its motion should be evaluated by the continuum mechanics. However, in the flight mechanics, they are commonly treated as rigid. In other way, in the structural dynamics scenario, rigid body modes are usually neglected. Such segregation is acceptable when sufficient separation exist between the frequencies of rigid and flexible modes. But, trends in the aircraft industry are leading to longer fuselages, larger aspect ratios, smaller thicknesses and the use of composite materials. Such configurations are more flexible and integrated models for flight mechanics and structural dynamics should be taken. This book develops the theme in a scenario of modelling, simulation and optimal control. Models of conceptual flexible aircraft are built in order to be used in control studies. A nonlinear optimal model following control is proposed. Linear solutions are developed, nonlinear approaches are also investigated, via neural networks. The technique is used to approximate the flexible aircraft as a rigid body, letting the job of controlling flexible modes to the automatic control, while an human or autopilot can see the aircraft as a usual rigid body.
Author: Gerasimos Rigatos
Publisher: Cambridge Scholars Publishing
ISBN: 1527562468
Category : Technology & Engineering
Languages : en
Pages : 741
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Book Description
This volume discusses advances in applied nonlinear optimal control, comprising both theoretical analysis of the developed control methods and case studies about their use in robotics, mechatronics, electric power generation, power electronics, micro-electronics, biological systems, biomedical systems, financial systems and industrial production processes. The advantages of the nonlinear optimal control approaches which are developed here are that, by applying approximate linearization of the controlled systems’ state-space description, one can avoid the elaborated state variables transformations (diffeomorphisms) which are required by global linearization-based control methods. The book also applies the control input directly to the power unit of the controlled systems and not on an equivalent linearized description, thus avoiding the inverse transformations met in global linearization-based control methods and the potential appearance of singularity problems. The method adopted here also retains the known advantages of optimal control, that is, the best trade-off between accurate tracking of reference setpoints and moderate variations of the control inputs. The book’s findings on nonlinear optimal control are a substantial contribution to the areas of nonlinear control and complex dynamical systems, and will find use in several research and engineering disciplines and in practical applications.
Author: Travis Eli Gibson
Publisher:
ISBN:
Category :
Languages : en
Pages : 192
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Book Description
One of the main features of adaptive systems is an oscillatory convergence that exacerbates with the speed of adaptation. Over the past two decades several attempts have been made to provide adaptive solutions with guaranteed transient properties. In this work it is shown that Closed-loop Reference Models (CRMs) can result in improved transient performance over their open-loop counterparts in model reference adaptive control. In addition to deriving bounds on L-2 norms of the derivatives of the adaptive parameters which are shown to be smaller, an optimal design of CRMs is proposed which minimizes an underlying peaking phenomenon. The analytical tools proposed are shown to be applicable for a range of adaptive control problems including direct control, composite control with observer feedback and partial states accessible control. In addition a detailed study of the applicability of CRM adaptive control to very flexible aircraft is presented. Following the NASA Helios flight mishap in 2003 there has been a push for greater understanding of the aerodynamic-structural coupling that occurs in light, very flexible, flying wings. Previous efforts in that direction revealed that the flexible aircraft had instability in the phugoid mode for large dihedral angles and that including the flexible dynamics was necessary to arrive at an appropriate trim condition. In this thesis, we show how these large dihedral excursions can occur in the presence of turbulence, by constructing an overall nonlinear model that captures the dominant dynamics of a very flexible aircraft. The thesis closes with the application of CRM adaptive control to the VFA model.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 36
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Book Description
Author: Horst Salzwedel
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 420
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Book Description
Author: Nikolaos Tantaroudas
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Author: Mark A. Mitchell
Publisher:
ISBN:
Category :
Languages : en
Pages : 172
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Book Description
Author: Declan Bates
Publisher: Springer
ISBN: 3540737197
Category : Technology & Engineering
Languages : en
Pages : 358
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Book Description
This is the first book to focus on the use of nonlinear analysis and synthesis techniques for aircraft control. It is also the first book to address in detail closed-loop control problems for aircraft "on-ground" – i.e. speed and directional control of aircraft before take-off and after touch down. The book will be of interest to engineers, researchers, and students in control engineering, and especially aircraft control.
Author: S. Sivasundaram
Publisher: CRC Press
ISBN: 9789056992224
Category : Technology & Engineering
Languages : en
Pages : 404
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Book Description
The study of nonlinear phenomena in aviation and aerospace includes developments in computer technology and the use of nonlinear mathematical models. Nonlinearities are a feature of aircraft dynamics and flight control systems and need to respond to achieve stability and performance. This multiauthor volume comprises selected papers from the conference Nonlinear Problems in Aviation and Aerospace at Embry-Riddle Aeronautical University and additional invited papers from many distinguished scientists. Coverage includes orbit determination of a tethered satellite system using laser and radar tracking, and intelligent control of agile aircraft, flight control with and without control surfaces.
Author: Mustafa Remzi Barlas
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 238
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Book Description
