Applications Of Rapid Prototyping To The Design And Testing Of Uav Flight Control Systems

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Applications of Rapid Prototyping to the Design and Testing of UAV Flight Control System

Author : John A. Komlosy
Publisher :
ISBN 13 :
Total Pages : 289 pages
Book Rating : 4.:/5 (64 download)

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Book Synopsis Applications of Rapid Prototyping to the Design and Testing of UAV Flight Control System by : John A. Komlosy

Download or read book Applications of Rapid Prototyping to the Design and Testing of UAV Flight Control System written by John A. Komlosy and published by . This book was released on 1998 with total page 289 pages. Available in PDF, EPUB and Kindle. Book excerpt: The modern engineer has a myriad of new tools to assist in the design and implementation of ever increasingly complex control systems. A promising emerging technology is rapid prototyping. By totally integrating the development process, a Rapid Prototyping System (RPS) takes the designer from initial concept to testing on actual hardware in a systematic, logical sequence. At the Naval Postgraduate School (NPS), we have applied the concept of rapid prototyping to the discipline of flight control. The NPS RPS consists of a commercially available rapid prototyping software suite and open architecture hardware to permit the greatest possible range of control and navigation projects. The RPS is crucial in that it allows students to participate in projects from the initial concept to the flight testing phase of the design process. This thesis will describe in detail two of these projects; the development of an Airspeed Controller using the RPS tools; and the integration of a Voice Control System developed by ViA, Inc. of Northfield, Minnesota. Both projects demonstrate the inherent flexibility and risk reduction of the rapid prototyping a roach to system design.

Applications of Rapid Prototyping to the Design and Testing of UAV Flight Control Systems

Author : John Komlosy
Publisher :
ISBN 13 : 9781423561576
Total Pages : 108 pages
Book Rating : 4.5/5 (615 download)

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Book Synopsis Applications of Rapid Prototyping to the Design and Testing of UAV Flight Control Systems by : John Komlosy

Download or read book Applications of Rapid Prototyping to the Design and Testing of UAV Flight Control Systems written by John Komlosy and published by . This book was released on 1998-03-01 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt: The modern engineer has a myriad of new tools to assist in the design and implementation of ever increasingly complex control systems. A promising emerging technology is rapid prototyping. By totally integrating the development process, a Rapid Prototyping System (RPS) takes the designer from initial concept to testing on actual hardware in a systematic, logical sequence. At the Naval Postgraduate School (NPS), we have applied the concept of rapid prototyping to the discipline of flight control. The NPS RPS consists of a commercially available rapid prototyping software suite and open architecture hardware to permit the greatest possible range of control and navigation projects. The RPS is crucial in that it allows students to participate in projects from the initial concept to the flight testing phase of the design process. This thesis will describe in detail two of these projects; the development of an Airspeed Controller using the RPS tools; and the integration of a Voice Control System developed by ViA, Inc. of Northfield, Minnesota. Both projects demonstrate the inherent flexibility and risk reduction of the rapid prototyping a roach to system design.

Design and Rapid Prototyping of Flight Control and Navigation System for an Unmanned Aerial Vehicle

Author : Bock Aeng Lim
Publisher :
ISBN 13 : 9781423510277
Total Pages : 121 pages
Book Rating : 4.5/5 (12 download)

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Book Synopsis Design and Rapid Prototyping of Flight Control and Navigation System for an Unmanned Aerial Vehicle by : Bock Aeng Lim

Download or read book Design and Rapid Prototyping of Flight Control and Navigation System for an Unmanned Aerial Vehicle written by Bock Aeng Lim and published by . This book was released on 2002-03-01 with total page 121 pages. Available in PDF, EPUB and Kindle. Book excerpt: The work in this thesis is in support of a larger research effort to implement a cluster of autonomous airborne vehicles with the capability to conduct coordinated flight maneuver planning and to perform distributed sensor fusion, Specifically, it seeks to design and implement an onboard flight control and navigation system for NPS FROG UAV, which will be used as the autonomous airborne vehicle for the research, using the newly marketed xPC Target Rapid Prototyping System from The Mathworks, Inc Part I briefly introduces the aircraft and explains the necessity for an onboard computer for the UAV. Part II describes the construction of the miniature aircraft computer, INS/GPS and air data sensor integration implementation as well as the rapid prototyping process. Part III covers the process to create a 6DOF model for the aircraft and the design of the aircraft autopilot, while Part IV presents a vision-based navigation algorithm that can be implemented on the UAV to give it some form of autonomous flight trajectory planning capability. Preliminary ground test results are presented in Part V to conclude this study.

Unmanned Aircraft Systems

Author : Ella Atkins
Publisher : John Wiley & Sons
ISBN 13 : 1118866452
Total Pages : 740 pages
Book Rating : 4.1/5 (188 download)

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Book Synopsis Unmanned Aircraft Systems by : Ella Atkins

Download or read book Unmanned Aircraft Systems written by Ella Atkins and published by John Wiley & Sons. This book was released on 2017-01-17 with total page 740 pages. Available in PDF, EPUB and Kindle. Book excerpt: UNMANNED AIRCRAF T SYSTEMS UNMANNED AIRCRAF T SYSTEMS An unmanned aircraft system (UAS), sometimes called a drone, is an aircraft without a human pilot on board ??? instead, the UAS can be controlled by an operator station on the ground or may be autonomous in operation. UAS are capable of addressing a broad range of applications in diverse, complex environments. Traditionally employed in mainly military applications, recent regulatory changes around the world are leading to an explosion of interest and wide-ranging new applications for UAS in civil airspace. Covering the design, development, operation, and mission profiles of unmanned aircraft systems, this single, comprehensive volume forms a complete, stand-alone reference on the topic. The volume integrates with the online Wiley Encyclopedia of Aerospace Engineering, providing many new and updated articles for existing subscribers to that work. The chapters cover the following items: Airframe configurations and design (launch systems, power generation, propulsion) Operations (missions, integration issues, and airspace access) Coordination (multivehicle cooperation and human oversight) With contributions from leading experts, this volume is intended to be a valuable addition, and a useful resource, for aerospace manufacturers and suppliers, governmental and industrial aerospace research establishments, airline and aviation industries, university engineering and science departments, and industry analysts, consultants, and researchers.

Unmanned Aircraft Systems

Author : Kimon P. Valavanis
Publisher : Springer Science & Business Media
ISBN 13 : 1402091370
Total Pages : 533 pages
Book Rating : 4.4/5 (2 download)

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Book Synopsis Unmanned Aircraft Systems by : Kimon P. Valavanis

Download or read book Unmanned Aircraft Systems written by Kimon P. Valavanis and published by Springer Science & Business Media. This book was released on 2008-12-21 with total page 533 pages. Available in PDF, EPUB and Kindle. Book excerpt: Unmanned Aircraft Systems (UAS) have seen unprecedented levels of growth during the last decade in both military and civilian domains. It is anticipated that civilian applications will be dominant in the future, although there are still barriers to be overcome and technical challenges to be met. Integrating UAS into, for example, civilian space, navigation, autonomy, see-detect-and-avoid systems, smart designs, system integration, vision-based navigation and training, to name but a few areas, will be of prime importance in the near future. This special volume is the outcome of research presented at the International Symposium on Unmanned Aerial Vehicles, held in Orlando, Florida, USA, from June 23-25, 2008, and presents state-of-the-art findings on topics such as: UAS operations and integration into the national airspace system; UAS navigation and control; micro-, mini-, small UAVs; UAS simulation testbeds and frameworks; UAS research platforms and applications; UAS applications. This book aims at serving as a guide tool on UAS for engineers and practitioners, academics, government agencies and industry. Previously published in the Journal of Intelligent and Robotic Systems, 54 (1-3, 2009).

Uniform System for the Rapid Prototyping and Testing of Controllers for Unmanned Aerial Vehicles

Author : James A. Zanino
Publisher :
ISBN 13 : 9781423574613
Total Pages : 97 pages
Book Rating : 4.5/5 (746 download)

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Book Synopsis Uniform System for the Rapid Prototyping and Testing of Controllers for Unmanned Aerial Vehicles by : James A. Zanino

Download or read book Uniform System for the Rapid Prototyping and Testing of Controllers for Unmanned Aerial Vehicles written by James A. Zanino and published by . This book was released on 1996-09-01 with total page 97 pages. Available in PDF, EPUB and Kindle. Book excerpt: The field of control systems has witnessed an explosion in state- space techniques addressing a variety of critical design issues facing control engineers today. Modem computational tools, such as the MATRIX(x) Product Family developed by Integrated Systems Incorporated, allow the designer o quickly design, test and implement control systems based on these state-space techniques. These new computing advances shorten the time required to complete a control design from a few years to a few months. However, as the design process progressed new inputs and outputs were required, which usually resulted in a confusing mess of connections that were hard to follow. Therefore, a universal system was needed that could be used on any controller design to aid in the understanding and tracking of the controller's inputs and outputs. A description of this system is given along with a detailed step by step process on how it was implemented on a Unmanned Air Vehicle (UAV).

Rapid Prototyping Software for Avionics Systems

Author : Nicolas Larrieu
Publisher : John Wiley & Sons
ISBN 13 : 1119050634
Total Pages : 152 pages
Book Rating : 4.1/5 (19 download)

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Book Synopsis Rapid Prototyping Software for Avionics Systems by : Nicolas Larrieu

Download or read book Rapid Prototyping Software for Avionics Systems written by Nicolas Larrieu and published by John Wiley & Sons. This book was released on 2014-10-13 with total page 152 pages. Available in PDF, EPUB and Kindle. Book excerpt: The design, implementation and validation of avionics and aeronautical systems have become extremely complex tasks due to the increase of functionalities that are deployed in current avionics systems and the need to be able certify them before putting them into production. This book proposes a methodology to enable the rapid prototyping of such a system by considering from the start the certification aspects of the solution produced. This method takes advantage of the model-based design approaches as well as the use of formal methods for the validation of these systems. Furthermore, the use of automatic software code generation tools using models makes it possible to reduce the development phase as well as the final solution testing. This book presents, firstly, an overview of the model-based design approaches such as those used in the field of aeronautical software engineering. Secondly, an original methodology that is perfectly adapted to the field of aeronautical embedded systems is introduced. Finally, the authors illustrate the use of this method using a case study for the design, implementation and testing of a new generation aeronautical router.

On Subscale Flight Testing

Author : Alejandro Sobron
Publisher : Linköping University Electronic Press
ISBN 13 : 9176852202
Total Pages : 112 pages
Book Rating : 4.1/5 (768 download)

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Book Synopsis On Subscale Flight Testing by : Alejandro Sobron

Download or read book On Subscale Flight Testing written by Alejandro Sobron and published by Linköping University Electronic Press. This book was released on 2018-11-05 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt: Downscaled physical models, also referred to as subscale models, have played an essential role in the investigation of the complex physics of flight until the recent disruption of numerical simulation. Despite the fact that improvements in computational methods are slowly pushing experimental techniques towards a secondary role as verification or calibration tools, real-world testing of physical prototypes still provides an unmatched confidence. Physical models are very effective at revealing issues that are sometimes not correctly identified in the virtual domain, and hence can be a valuable complement to other design tools. But traditional wind-tunnel testing cannot always meet all of the requirements of modern aeronautical research and development. It is nowadays too expensive to use these scarce facilities to explore different design iterations during the initial stages of aircraft development, or to experiment with new and immature technologies. Testing of free-flight subscale models, referred to as Subscale Flight Testing (SFT), could offer an affordable and low-risk alternative for complementing conventional techniques with both qualitative and quantitative information. The miniaturisation of mechatronic systems, the advances in rapid-prototyping techniques and power storage, as well as new manufacturing methods, currently enable the development of sophisticated test objects at scales that were impractical some decades ago. Moreover, the recent boom in the commercial drone industry has driven a quick development of specialised electronics and sensors, which offer nowadays surprising capabilities at competitive prices. These recent technological disruptions have significantly altered the cost-benefit function of SFT and it is necessary to re-evaluate its potential in the contemporary aircraft development context. This thesis aims to increase the comprehension and knowledge of the SFT method in order to define a practical framework for its use in aircraft design; focusing on low-cost, short-time solutions that don’t require more than a small organization and few resources. This objective is approached from a theoretical point of view by means of an analysis of the physical and practical limitations of the scaling laws; and from an empirical point of view by means of field experiments aimed at identifying practical needs for equipment, methods, and tools. A low-cost data acquisition system is developed and tested; a novel method for semi-automated flight testing in small airspaces is proposed; a set of tools for analysis and visualisation of flight data is presented; and it is also demonstrated that it is possible to explore and demonstrate new technology using SFT with a very limited amount of economic and human resources. All these, together with a theoretical review and contextualisation, contribute to increasing the comprehension and knowledge of the SFT method in general, and its potential applications in aircraft conceptual design in particular.

Advances in Aerospace Guidance, Navigation and Control

Author : Florian Holzapfel
Publisher : Springer Science & Business Media
ISBN 13 : 3642198171
Total Pages : 465 pages
Book Rating : 4.6/5 (421 download)

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Book Synopsis Advances in Aerospace Guidance, Navigation and Control by : Florian Holzapfel

Download or read book Advances in Aerospace Guidance, Navigation and Control written by Florian Holzapfel and published by Springer Science & Business Media. This book was released on 2011-03-15 with total page 465 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.

Foundations of Circulation Control Based Small-Scale Unmanned Aircraft

Author : Konstantinos Kanistras
Publisher : Springer
ISBN 13 : 3319678523
Total Pages : 138 pages
Book Rating : 4.3/5 (196 download)

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Book Synopsis Foundations of Circulation Control Based Small-Scale Unmanned Aircraft by : Konstantinos Kanistras

Download or read book Foundations of Circulation Control Based Small-Scale Unmanned Aircraft written by Konstantinos Kanistras and published by Springer. This book was released on 2017-11-02 with total page 138 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book focuses on using and implementing Circulation Control (CC) - an active flow control method used to produce increased lift over the traditionally used systems, like flaps, slats, etc. - to design a new type of fixed-wing unmanned aircraft that are endowed with improved aerodynamic efficiency, enhanced endurance, increased useful payload (fuel capacity, battery cells, on-board sensors) during cruise flight, delayed stall, and reduced runway during takeoff and landing. It presents the foundations of a step-by-step comprehensive methodology from design to implementation and experimental testing of Coandǎ based Circulation Control Wings (CCWs) and CC system, both integral components of the new type of aircraft, called Unmanned Circulation Control Air Vehicle. The methodology is composed of seven coupled phases: theoretical and mathematical analysis, design, simulation, 3-D printing/prototyping, wind tunnel testing, wing implementation and integration, and flight testing. The theoretical analysis focuses on understanding the physics of the flow and on defining the design parameters of the geometry restrictions of the wing and the plenum. The design phase centers on: designs of Coandǎ surfaces based on wing geometry specifications; designing and modifying airfoils from well-known ones (NACA series, Clark-Y, etc.); plenum designs for flow uniformity; dual radius flap designs to delay flow separation and reduce cruise drag. The simulation phase focuses on Computational Fluid Dynamics (CFD) analysis and simulations, and on calculating lift and drag coefficients of the designed CCWs in a simulation environment. 3-D printing and prototyping focuses on the actual construction of the CCWs. Wind tunnel testing centers on experimental studies in a laboratory environment. One step before flight testing is implementation of the qualified CCW and integration on the UAV platform, along with the CC system. Flight testing is the final phase, where design validation is performed. This book is the first of its kind, and it is suitable for students and researchers interested in the design and development of CCWs for small-scale aircraft. Background knowledge on fundamental Aerodynamics is required.

Multisensor Attitude Estimation

Author : Hassen Fourati
Publisher : CRC Press
ISBN 13 : 1498745806
Total Pages : 580 pages
Book Rating : 4.4/5 (987 download)

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Book Synopsis Multisensor Attitude Estimation by : Hassen Fourati

Download or read book Multisensor Attitude Estimation written by Hassen Fourati and published by CRC Press. This book was released on 2016-11-03 with total page 580 pages. Available in PDF, EPUB and Kindle. Book excerpt: There has been an increasing interest in multi-disciplinary research on multisensor attitude estimation technology driven by its versatility and diverse areas of application, such as sensor networks, robotics, navigation, video, biomedicine, etc. Attitude estimation consists of the determination of rigid bodies’ orientation in 3D space. This research area is a multilevel, multifaceted process handling the automatic association, correlation, estimation, and combination of data and information from several sources. Data fusion for attitude estimation is motivated by several issues and problems, such as data imperfection, data multi-modality, data dimensionality, processing framework, etc. While many of these problems have been identified and heavily investigated, no single data fusion algorithm is capable of addressing all the aforementioned challenges. The variety of methods in the literature focus on a subset of these issues to solve, which would be determined based on the application in hand. Historically, the problem of attitude estimation has been introduced by Grace Wahba in 1965 within the estimate of satellite attitude and aerospace applications. This book intends to provide the reader with both a generic and comprehensive view of contemporary data fusion methodologies for attitude estimation, as well as the most recent researches and novel advances on multisensor attitude estimation task. It explores the design of algorithms and architectures, benefits, and challenging aspects, as well as a broad array of disciplines, including: navigation, robotics, biomedicine, motion analysis, etc. A number of issues that make data fusion for attitude estimation a challenging task, and which will be discussed through the different chapters of the book, are related to: 1) The nature of sensors and information sources (accelerometer, gyroscope, magnetometer, GPS, inclinometer, etc.); 2) The computational ability at the sensors; 3) The theoretical developments and convergence proofs; 4) The system architecture, computational resources, fusion level.

Smart Autonomous Aircraft

Author : Yasmina Bestaoui Sebbane
Publisher : CRC Press
ISBN 13 : 148229916X
Total Pages : 434 pages
Book Rating : 4.4/5 (822 download)

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Book Synopsis Smart Autonomous Aircraft by : Yasmina Bestaoui Sebbane

Download or read book Smart Autonomous Aircraft written by Yasmina Bestaoui Sebbane and published by CRC Press. This book was released on 2015-11-18 with total page 434 pages. Available in PDF, EPUB and Kindle. Book excerpt: With the extraordinary growth of Unmanned Aerial Vehicles (UAV) in research, military, and commercial contexts, there has been a need for a reference that provides a comprehensive look at the latest research in the area. Filling this void, Smart Autonomous Aircraft: Flight Control and Planning for UAV introduces the advanced methods of flight contr

International Aerospace Abstracts

Author :
Publisher :
ISBN 13 :
Total Pages : 1020 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis International Aerospace Abstracts by :

Download or read book International Aerospace Abstracts written by and published by . This book was released on 1999 with total page 1020 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Design and Evaluation of a Digital Flight Control System for the FROG Unmanned Aerial Vehicle

Author : Christopher H. Flood
Publisher :
ISBN 13 : 9781423525813
Total Pages : 130 pages
Book Rating : 4.5/5 (258 download)

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Book Synopsis Design and Evaluation of a Digital Flight Control System for the FROG Unmanned Aerial Vehicle by : Christopher H. Flood

Download or read book Design and Evaluation of a Digital Flight Control System for the FROG Unmanned Aerial Vehicle written by Christopher H. Flood and published by . This book was released on 2001-09-01 with total page 130 pages. Available in PDF, EPUB and Kindle. Book excerpt: The importance of unmanned aerial vehicles (UAVs) to current and future military operations cannot be understated. This rapidly developing field requires the ability to quickly develop and evaluate advanced control concepts. The FROG UAV serves as a test bed for advanced control and sensor projects at the Naval Postgraduate School. Previous control system projects have made use of a low performance electromechanical autopilot onboard the UAV. This autopilot imposed significant limitations on the responsiveness of the FROG. This project developed and tested an off board digital flight control system for use in lieu of the previous electromechanical device. The digital flight controller was developed using the Matrixx rapid prototyping system and a previously validated dynamic model of the FROG. Surrogate flight control servo actuators were characterized in the laboratory and added to the plant model. Classic inner/ outer loop controllers were developed for yaw damping and speed, altitude and heading control. The system was then successfully demonstrated%ted with hardware in the loop in the lab. The FROG was then instrumented and a command uplink latency of 170 MS was discovered. This introduced excessive phase lag into the system, which drove the flight controllers unstable. An alternate serial uplink method was developed and tested which reduced the command latency to 76 MS however the remaining phase lag resulted in limit cycle oscillation. Laboratory tests indicated that the current flight controller could withstand a maximum of 50 MS command path delay; without modification.

L1 Adaptive Control Theory

Author : Naira Hovakimyan
Publisher : SIAM
ISBN 13 : 0898717043
Total Pages : 333 pages
Book Rating : 4.8/5 (987 download)

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Book Synopsis L1 Adaptive Control Theory by : Naira Hovakimyan

Download or read book L1 Adaptive Control Theory written by Naira Hovakimyan and published by SIAM. This book was released on 2010-09-30 with total page 333 pages. Available in PDF, EPUB and Kindle. Book excerpt: Contains results not yet published in technical journals and conference proceedings.

Robust Formation Control for Multiple Unmanned Aerial Vehicles

Author : Hao Liu
Publisher : CRC Press
ISBN 13 : 1000788504
Total Pages : 145 pages
Book Rating : 4.0/5 (7 download)

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Book Synopsis Robust Formation Control for Multiple Unmanned Aerial Vehicles by : Hao Liu

Download or read book Robust Formation Control for Multiple Unmanned Aerial Vehicles written by Hao Liu and published by CRC Press. This book was released on 2022-12-01 with total page 145 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book is based on the authors’ recent research results on formation control problems, including time-varying formation, communication delays, fault-tolerant formation for multiple UAV systems with highly nonlinear and coupled, parameter uncertainties, and external disturbances. Differentiating from existing works, this book presents a robust optimal formation approach to designing distributed cooperative control laws for a group of UAVs, based on the linear quadratic regulator control method and the robust compensation theory. The proposed control method is composed of two parts: the nominal part to achieve desired tracking performance and the robust compensation part to restrain the influence of highly nonlinear and strongly coupled parameter uncertainties, and external disturbances on the global closed-loop control system. Furthermore, this book gives proof of their robust properties. The influence of communication delays and actuator fault tolerance can be restrained by the proposed robust formation control protocol, and the formation tracking errors can converge into a neighborhood of the origin bounded by a given constant in a finite time. Moreover, the book provides details about the practical application of the proposed method to design formation control systems for multiple quadrotors and tail-sitters. Additional features include a robust control method that is proposed to address the formation control problem for UAVs and theoretical and experimental research for the cooperative flight of the quadrotor UAV group and the tail-sitter UAV group. Robust Formation Control for Multiple Unmanned Aerial Vehicles is suitable for graduate students, researchers, and engineers in the system and control community, especially those engaged in the areas of robust control, UAV swarming, and multi-agent systems.

Department of Defense Authorization for Appropriations for Fiscal Year 1997 and the Future Years Defense Program

Author : United States. Congress. Senate. Committee on Armed Services
Publisher :
ISBN 13 :
Total Pages : 308 pages
Book Rating : 4.0/5 ( download)

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Book Synopsis Department of Defense Authorization for Appropriations for Fiscal Year 1997 and the Future Years Defense Program by : United States. Congress. Senate. Committee on Armed Services

Download or read book Department of Defense Authorization for Appropriations for Fiscal Year 1997 and the Future Years Defense Program written by United States. Congress. Senate. Committee on Armed Services and published by . This book was released on 1997 with total page 308 pages. Available in PDF, EPUB and Kindle. Book excerpt: