H Aerospace Control Design

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H∞ Aerospace Control Design

Author : Richard A. Hyde
Publisher : Springer Science & Business Media
Page : 220 pages
File Size : 48,6 Mb
Release : 2013-03-09
Category : Technology & Engineering
ISBN : 9781447130499

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H∞ Aerospace Control Design by Richard A. Hyde Pdf

Recent Developments in H¿ theory have produced a promising new design approach. However, a large gap between theory and practice has emerged, with as yet very few design examples applied to real industrial control problems. The work described in this monograph aims to narrow this gap, and to address implementation issues associated with multivariable H¿ controllers. An H¿ control law has been developed and tested for the DRA (Defence Research Agency) Bedford research Harrier. The first part of this text introduces the basic components of the flight control and engine systems and describes the models for the different sub-systems. The second part deals with implementational problems including the discretization process, handling limitations on actuators and the nonlinearities in the system.

Aircraft Design

Author : Mohammad H. Sadraey
Publisher : John Wiley & Sons
Page : 811 pages
File Size : 52,9 Mb
Release : 2012-11-20
Category : Technology & Engineering
ISBN : 9781118352809

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Aircraft Design by Mohammad H. Sadraey Pdf

A comprehensive approach to the air vehicle design process using the principles of systems engineering Due to the high cost and the risks associated with development, complex aircraft systems have become a prime candidate for the adoption of systems engineering methodologies. This book presents the entire process of aircraft design based on a systems engineering approach from conceptual design phase, through to preliminary design phase and to detail design phase. Presenting in one volume the methodologies behind aircraft design, this book covers the components and the issues affected by design procedures. The basic topics that are essential to the process, such as aerodynamics, flight stability and control, aero-structure, and aircraft performance are reviewed in various chapters where required. Based on these fundamentals and design requirements, the author explains the design process in a holistic manner to emphasise the integration of the individual components into the overall design. Throughout the book the various design options are considered and weighed against each other, to give readers a practical understanding of the process overall. Readers with knowledge of the fundamental concepts of aerodynamics, propulsion, aero-structure, and flight dynamics will find this book ideal to progress towards the next stage in their understanding of the topic. Furthermore, the broad variety of design techniques covered ensures that readers have the freedom and flexibility to satisfy the design requirements when approaching real-world projects. Key features: • Provides full coverage of the design aspects of an air vehicle including: aeronautical concepts, design techniques and design flowcharts • Features end of chapter problems to reinforce the learning process as well as fully solved design examples at component level • Includes fundamental explanations for aeronautical engineering students and practicing engineers • Features a solutions manual to sample questions on the book’s companion website Companion website - www.wiley.com/go/sadraey

Advances in Aerospace Guidance, Navigation and Control

Author : Florian Holzapfel,Stephan Theil
Publisher : Springer Science & Business Media
Page : 465 pages
File Size : 55,7 Mb
Release : 2011-03-15
Category : Technology & Engineering
ISBN : 9783642198175

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Advances in Aerospace Guidance, Navigation and Control by Florian Holzapfel,Stephan Theil Pdf

Over the last few decades, both the aeronautics and space disciplines have greatly influenced advances in controls, sensors, data fusion and navigation. Many of those achievements that made the word “aerospace” synonymous with “high–tech” were enabled by innovations in guidance, navigation and control. Europe has seen a strong trans-national consolidation process in aerospace over the last few decades. Most of the visible products, like commercial aircraft, fighters, helicopters, satellites, launchers or missiles, are not made by a single country – they are the fruits of cooperation. No European country by itself hosts a specialized guidance, navigation and controls community large enough to cover the whole spectrum of disciplines. However, on a European scale, mutual exchange of ideas, concepts and solutions is enriching for all. The 1st CEAS Specialist Conference on Guidance, Navigation and Control is an attempt to bring this community together. This book is a selection of papers presented at the conference. All submitted papers have gone through a formal review process in compliance with good journal practices. The best papers have been recommended by the reviewers to be published in this book.

Robust Multivariable Control of Aerospace Systems

Author : Declan Bates,Ian Postlethwaite
Publisher : IOS Press
Page : 220 pages
File Size : 41,6 Mb
Release : 2002
Category : Science
ISBN : UOM:39015057632476

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Robust Multivariable Control of Aerospace Systems by Declan Bates,Ian Postlethwaite Pdf

Classical design and analysis techniques, many of which date back to the 1950's, are still predominantly used in the aerospace industry for the design and analysis of automatic flight control and aero-engine control systems. The continued success and popularity of these techniques is particularly impressive considering the radical advances in aircraft and spacecraft design and avionics technology made over this period. Clearly, an understanding of both the advantages and limitations of these methods is essential in order to properly evaluate the likely usefulness of more modern techniques for the design and analysis of aerospace control systems. One of the themes of this book is that the multivariable robust control methods it describes are logical and natural extensions of the more classical methods, and not replacements for them. It is assumed that readers of this publication are already familiar with classical flight control techniques. Emphasis is on the philosophy, advantages and limitations of the classical approach to flight control system design and analysis. Abstracted in Inspec

Aircraft Design

Author : Mohammad H. Sadraey
Publisher : John Wiley & Sons
Page : 811 pages
File Size : 40,9 Mb
Release : 2012-11-28
Category : Technology & Engineering
ISBN : 9781119953401

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Aircraft Design by Mohammad H. Sadraey Pdf

A comprehensive approach to the air vehicle design process using the principles of systems engineering Due to the high cost and the risks associated with development, complex aircraft systems have become a prime candidate for the adoption of systems engineering methodologies. This book presents the entire process of aircraft design based on a systems engineering approach from conceptual design phase, through to preliminary design phase and to detail design phase. Presenting in one volume the methodologies behind aircraft design, this book covers the components and the issues affected by design procedures. The basic topics that are essential to the process, such as aerodynamics, flight stability and control, aero-structure, and aircraft performance are reviewed in various chapters where required. Based on these fundamentals and design requirements, the author explains the design process in a holistic manner to emphasise the integration of the individual components into the overall design. Throughout the book the various design options are considered and weighed against each other, to give readers a practical understanding of the process overall. Readers with knowledge of the fundamental concepts of aerodynamics, propulsion, aero-structure, and flight dynamics will find this book ideal to progress towards the next stage in their understanding of the topic. Furthermore, the broad variety of design techniques covered ensures that readers have the freedom and flexibility to satisfy the design requirements when approaching real-world projects. Key features: • Provides full coverage of the design aspects of an air vehicle including: aeronautical concepts, design techniques and design flowcharts • Features end of chapter problems to reinforce the learning process as well as fully solved design examples at component level • Includes fundamental explanations for aeronautical engineering students and practicing engineers • Features a solutions manual to sample questions on the book’s companion website Companion website - www.wiley.com/go/sadraey

Aircraft Control and Simulation

Author : Brian L. Stevens,Frank L. Lewis,Eric N. Johnson
Publisher : John Wiley & Sons
Page : 768 pages
File Size : 53,7 Mb
Release : 2015-11-02
Category : Technology & Engineering
ISBN : 9781118870983

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Aircraft Control and Simulation by Brian L. Stevens,Frank L. Lewis,Eric N. Johnson Pdf

Get a complete understanding of aircraft control and simulation Aircraft Control and Simulation: Dynamics, Controls Design, and Autonomous Systems, Third Edition is a comprehensive guide to aircraft control and simulation. This updated text covers flight control systems, flight dynamics, aircraft modeling, and flight simulation from both classical design and modern perspectives, as well as two new chapters on the modeling, simulation, and adaptive control of unmanned aerial vehicles. With detailed examples, including relevant MATLAB calculations and FORTRAN codes, this approachable yet detailed reference also provides access to supplementary materials, including chapter problems and an instructor's solution manual. Aircraft control, as a subject area, combines an understanding of aerodynamics with knowledge of the physical systems of an aircraft. The ability to analyze the performance of an aircraft both in the real world and in computer-simulated flight is essential to maintaining proper control and function of the aircraft. Keeping up with the skills necessary to perform this analysis is critical for you to thrive in the aircraft control field. Explore a steadily progressing list of topics, including equations of motion and aerodynamics, classical controls, and more advanced control methods Consider detailed control design examples using computer numerical tools and simulation examples Understand control design methods as they are applied to aircraft nonlinear math models Access updated content about unmanned aircraft (UAVs) Aircraft Control and Simulation: Dynamics, Controls Design, and Autonomous Systems, Third Edition is an essential reference for engineers and designers involved in the development of aircraft and aerospace systems and computer-based flight simulations, as well as upper-level undergraduate and graduate students studying mechanical and aerospace engineering.

Aircraft Performance

Author : Mohammad H. Sadraey
Publisher : CRC Press
Page : 686 pages
File Size : 40,5 Mb
Release : 2023-07-14
Category : Science
ISBN : 9781000898545

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Aircraft Performance by Mohammad H. Sadraey Pdf

Aircraft Performance: An Engineering Approach, Second Edition introduces flight performance analysis techniques of fixed-wing air vehicles, particularly heavier-than-aircraft. It covers maximum speed, absolute ceiling, rate of climb, range, endurance, turn performance, and takeoff run. Enabling the reader to analyze the performance and flight capabilities of an aircraft by utilizing only the aircraft weight data, geometry, and engine characteristics, this book covers the flight performance analysis for both propeller-driven and jet aircraft. The second edition features new content on vertical takeoff and landing, UAV launch, UAV recovery, use of rocket engine as the main engine, range for electric aircraft, electric engine, endurance for electric aircraft, gliding flight, pull-up, and climb-turn. In addition, this book includes end-of-chapter problems, MATLAB® code and examples, and case studies to enhance and reinforce student understanding. This book is intended for senior undergraduate aerospace students taking courses in Aircraft Performance, Flight Dynamics, and Flight Mechanics. Instructors will be able to utilize an updated Solutions Manual and Figure Slides for their course.

Flight Control Systems

Author : Roger Pratt
Publisher : Institution of Engineering & Technology
Page : 424 pages
File Size : 41,8 Mb
Release : 2000
Category : Technology & Engineering
ISBN : UOM:39015050250326

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Flight Control Systems by Roger Pratt Pdf

Annotation Bridging the gap between academic research and real-world applications, this reference on modern flight control methods for fixed-wing aircraft deals with fundamentals of flight control systems design, then concentrates on applications based on the modern control methods used in the latest aircraft. The book is written for practicing engineers who are new to the aviation industry, postgraduate students in strategic or applied research, and advanced undergraduates. Some knowledge of classical control is assumed. Pratt is a member of IEEE and is UK Member for AIAA's Technical Committee on Guidance, Navigation and Control. Annotation c. Book News, Inc., Portland, OR (booknews.com)

Flight Dynamics and Control of Aero and Space Vehicles

Author : Rama K. Yedavalli
Publisher : John Wiley & Sons
Page : 554 pages
File Size : 48,9 Mb
Release : 2020-02-25
Category : Technology & Engineering
ISBN : 9781118934456

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Flight Dynamics and Control of Aero and Space Vehicles by Rama K. Yedavalli Pdf

Flight Vehicle Dynamics and Control Rama K. Yedavalli, The Ohio State University, USA A comprehensive textbook which presents flight vehicle dynamics and control in a unified framework Flight Vehicle Dynamics and Control presents the dynamics and control of various flight vehicles, including aircraft, spacecraft, helicopter, missiles, etc, in a unified framework. It covers the fundamental topics in the dynamics and control of these flight vehicles, highlighting shared points as well as differences in dynamics and control issues, making use of the ‘systems level’ viewpoint. The book begins with the derivation of the equations of motion for a general rigid body and then delineates the differences between the dynamics of various flight vehicles in a fundamental way. It then focuses on the dynamic equations with application to these various flight vehicles, concentrating more on aircraft and spacecraft cases. Then the control systems analysis and design is carried out both from transfer function, classical control, as well as modern, state space control points of view. Illustrative examples of application to atmospheric and space vehicles are presented, emphasizing the ‘systems level’ viewpoint of control design. Key features: Provides a comprehensive treatment of dynamics and control of various flight vehicles in a single volume. Contains worked out examples (including MATLAB examples) and end of chapter homework problems. Suitable as a single textbook for a sequence of undergraduate courses on flight vehicle dynamics and control. Accompanied by a website that includes additional problems and a solutions manual. The book is essential reading for undergraduate students in mechanical and aerospace engineering, engineers working on flight vehicle control, and researchers from other engineering backgrounds working on related topics.

Performance Evaluation and Design of Flight Vehicle Control Systems

Author : Eric T. Falangas
Publisher : John Wiley & Sons
Page : 432 pages
File Size : 49,7 Mb
Release : 2015-12-02
Category : Technology & Engineering
ISBN : 9781119134855

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Performance Evaluation and Design of Flight Vehicle Control Systems by Eric T. Falangas Pdf

The purpose of this book is to assist analysts, engineers, and students toward developing dynamic models, and analyzing the control of flight vehicles with various blended features comprising aircraft, launch vehicles, reentry vehicles, missiles and aircraft. Graphical methods for analysing vehicle performance Methods for trimming deflections of a vehicle that has multiple types of effectors Presents a parameters used for speedily evaluating the performance, stability, and controllability of a new flight vehicle concept along a trajectory or with fixed flight conditions

Reverse Engineering in Control Design

Author : Daniel Alazard
Publisher : John Wiley & Sons
Page : 150 pages
File Size : 48,7 Mb
Release : 2013-03-05
Category : Technology & Engineering
ISBN : 9781118602621

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Reverse Engineering in Control Design by Daniel Alazard Pdf

Reverse Engineering in Control Design proposes practical approaches to building a standard H-infinity problem taking into account an initial controller. Such approaches allow us to mix various control objectives and to initialize procedures for a fixed-structure controller design. They are based on the Observer-Based Realization (OBR) of controllers. The interest of OBR from the controller implementation point of view is detailed and highlighted in this book through academic examples. An open-source toolbox is available to implement these approaches in Matlab®. Throughout the book academic applications are proposed to illustrate the various basic principles. These applications have been chosen by the author for their pedagogic contents and demo files and embedded Matlab® functions can be downloaded so readers can run these illustrations on their personal computers. Contents 1. Observer-based Realization of a Given Controller. 2. Cross Standard Form and Reverse Engineering. 3. Reverse Engineering for Mechanical Systems. Appendix 1. A Preliminary Methodological Example. Appendix 2. Discrete-time Case. Appendix 3. Nominal State-feedback for Mechanical Systems. Appendix 4. Help of Matlab® Functions. About the Authors Daniel Alazard is Professor in System Dynamics and Control at Institut Supérieur de l'Aéronautique et de l’Espace (ISAE), Toulouse, France – SUPAERO Graduate Program. His main research interests concern robust control, flexible structure control and their applications to various aerospace systems.

Practical Methods for Aircraft and Rotorcraft Flight Control Design

Author : Mark Brian Tischler
Publisher : Unknown
Page : 0 pages
File Size : 51,5 Mb
Release : 2017
Category : Airplanes
ISBN : 1624104436

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Practical Methods for Aircraft and Rotorcraft Flight Control Design by Mark Brian Tischler Pdf

Reducing the theoretical methods of flight control to design practice, Practical Methods for Aircraft and Rotorcraft Flight Control Design: An Optimization-Based Approach compiles the authors' extensive experience and lessons learned into a single comprehensive resource for both academics and working flight control engineers.

Automatic Flight Control Systems

Author : Mohammad Sadraey
Publisher : Springer Nature
Page : 159 pages
File Size : 43,7 Mb
Release : 2022-05-31
Category : Technology & Engineering
ISBN : 9783031796494

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Automatic Flight Control Systems by Mohammad Sadraey Pdf

This book provides readers with a design approach to the automatic flight control systems (AFCS). The AFCS is the primary on-board tool for long flight operations, and is the foundation for the airspace modernization initiatives. In this text, AFCS and autopilot are employed interchangeably. It presents fundamentals of AFCS/autopilot, including primary subsystems, dynamic modeling, AFCS categories/functions/modes, servos/actuators, measurement devices, requirements, functional block diagrams, design techniques, and control laws. The book consists of six chapters. The first two chapters cover the fundamentals of AFCS and closed-loop control systems in manned and unmanned aircraft. The last four chapters present features of Attitude control systems (Hold functions), Flight path control systems (Navigation functions), Stability augmentation systems, and Command augmentation systems, respectively.

Design of Unmanned Aerial Systems

Author : Mohammad H. Sadraey
Publisher : John Wiley & Sons
Page : 664 pages
File Size : 48,6 Mb
Release : 2020-02-20
Category : Technology & Engineering
ISBN : 9781119508694

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Design of Unmanned Aerial Systems by Mohammad H. Sadraey Pdf

Provides a comprehensive introduction to the design and analysis of unmanned aircraft systems with a systems perspective Written for students and engineers who are new to the field of unmanned aerial vehicle design, this book teaches the many UAV design techniques being used today and demonstrates how to apply aeronautical science concepts to their design. Design of Unmanned Aerial Systems covers the design of UAVs in three sections—vehicle design, autopilot design, and ground systems design—in a way that allows readers to fully comprehend the science behind the subject so that they can then demonstrate creativity in the application of these concepts on their own. It teaches students and engineers all about: UAV classifications, design groups, design requirements, mission planning, conceptual design, detail design, and design procedures. It provides them with in-depth knowledge of ground stations, power systems, propulsion systems, automatic flight control systems, guidance systems, navigation systems, and launch and recovery systems. Students will also learn about payloads, manufacturing considerations, design challenges, flight software, microcontroller, and design examples. In addition, the book places major emphasis on the automatic flight control systems and autopilots. Provides design steps and procedures for each major component Presents several fully solved, step-by-step examples at component level Includes numerous UAV figures/images to emphasize the application of the concepts Describes real stories that stress the significance of safety in UAV design Offers various UAV configurations, geometries, and weight data to demonstrate the real-world applications and examples Covers a variety of design techniques/processes such that the designer has freedom and flexibility to satisfy the design requirements in several ways Features many end-of-chapter problems for readers to practice Design of Unmanned Aerial Systems is an excellent text for courses in the design of unmanned aerial vehicles at both the upper division undergraduate and beginning graduate levels.

Flight Control Systems

Author : Anonim
Publisher : Unknown
Page : 128 pages
File Size : 48,5 Mb
Release : 2000
Category : Actuators
ISBN : OCLC:838909824

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Flight Control Systems by Anonim Pdf

The book aims to build on the fundamentals of flight dynamics and flight control and embellish these principles by assigning their relevance to the development of flight control systems in the aircraft industry. The book comprises 9 chapters and deals with the following subjects: industrial considerations for flight control; aircraft modelling; actuation systems; handling qualities; automatic flight control system design considerations; ground and flight testing of digital flight control systems; aeroservoelasticity; eigenstructure assignment applied to the design of an autopilot function for a civil aircraft; and H & infin; loop-shaping design for the VAAC Harrier