Applications Of Rapid Prototyping To The Design And Testing Of Uav Flight Control Systems
DOWNLOAD
Download Applications Of Rapid Prototyping To The Design And Testing Of Uav Flight Control Systems PDF/ePub or read online books in Mobi eBooks. Click Download or Read Online button to get Applications Of Rapid Prototyping To The Design And Testing Of Uav Flight Control Systems book now. This website allows unlimited access to, at the time of writing, more than 1.5 million titles, including hundreds of thousands of titles in various foreign languages. If the content not found or just blank you must refresh this page
Applications Of Rapid Prototyping To The Design And Testing Of Uav Flight Control Systems
DOWNLOAD
Author : John Komlosy
language : en
Publisher:
Release Date : 1998-03-01
Applications Of Rapid Prototyping To The Design And Testing Of Uav Flight Control Systems written by John Komlosy and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1998-03-01 with categories.
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 System
DOWNLOAD
Author : John A. Komlosy
language : en
Publisher:
Release Date : 1998
Applications Of Rapid Prototyping To The Design And Testing Of Uav Flight Control System written by John A. Komlosy and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1998 with categories.
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
DOWNLOAD
Author : Bock Aeng Lim
language : en
Publisher:
Release Date : 2002-03-01
Design And Rapid Prototyping Of Flight Control And Navigation System For An Unmanned Aerial Vehicle written by Bock Aeng Lim and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2002-03-01 with categories.
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.
Drone Development From Concept To Flight
DOWNLOAD
Author : Sumit Sharma
language : en
Publisher: Packt Publishing Ltd
Release Date : 2024-04-30
Drone Development From Concept To Flight written by Sumit Sharma and has been published by Packt Publishing Ltd this book supported file pdf, txt, epub, kindle and other format this book has been release on 2024-04-30 with Technology & Engineering categories.
Learn the principles behind building and flying drones, using components like BLDC motors and speed controllers, AeroGCS ground software, Ardupilot and PX4 open-source flight stacks, along with examples and best practices Key Features Explore multicopter physics (roll, pitch, and yaw) and 3D dynamics for defining a drone’s flight Optimize drone performance with powerful propulsion systems such as BLDS motors, lipo batteries, and ESCs Build a custom survey drone to learn vital aspects of drone assembly, configuration, testing, and maiden flight Purchase of the print or Kindle book includes a free PDF eBook Book DescriptionUnlock opportunities in the growing UAV market where drones are revolutionizing diverse sectors like agriculture, surveying, and the military. This book walks you through the complete drone development life cycle, from concept to pilot stage, prototyping, and ultimately, a market-ready product, with domain-specific applications. Starting with an introduction to unmanned systems, principles of drone flight, and it's motion in 3D space, this book shows you how to design a propulsion system tailored to your drone’s needs. You’ll then get hands on with the entire drone assembly process, covering airframe, components, and wiring. Next, you’ll enhance drone connectivity and navigation with communication devices, such as RFD900, Herelink, and H-16 Pro GCS and hardware protocols like I2C, and UART. The book also guides you in using the open-source flight software Ardupilot and PX4, along with firmware architecture and PID tuning for advanced control. Additionally, you’ll go learn about AeroGCS, Mission Planner, and UGCS ground control stations, tips for maiden flight and log analysis for optimizing performance while building a custom survey drone with a 60-min endurance, 10km range, live video feed, and photography options. By the end of this book, you’ll be equipped with all you need to build and fly your own drones and UAVs.What you will learn Explore the design principles for multicopter flight and its physics of motion Grasp terminologies associated with UAV flight systems Gain an in-depth understanding of power trail, communication, and propulsion of a drone Study IMUs and sensors in flight controllers, and protocols like I2C, SPI, and MAvlink Familiarize yourself with open-source drone flight stacks and ground control station software Understand the control law used in multicopter and the basics of PIDs Delve into modes of flying with remote controllers and analysis of flight logs Who this book is for This book is for beginner-level drone engineers, robotics engineers, hardware and design engineers, and hobbyists who want to enter the drone industry and enhance their knowledge of the physics, mechanics, avionics, and programming of drones, multicopters, and UAVs. A basic understanding of circuits, assembly, microcontrollers, and electronic instruments like multimeter and batteries, along with fundamental concepts in physics and mathematics, will be helpful for reading this book.
Uniform System For The Rapid Prototyping And Testing Of Controllers For Unmanned Aerial Vehicles
DOWNLOAD
Author : Naval Postgraduate School
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2015-12-23
Uniform System For The Rapid Prototyping And Testing Of Controllers For Unmanned Aerial Vehicles written by Naval Postgraduate School and has been published by Createspace Independent Publishing Platform this book supported file pdf, txt, epub, kindle and other format this book has been release on 2015-12-23 with categories.
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, . Product Family developed by Integrated Systems Incorporated, allow the designer to 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)
Uniform System For The Rapid Prototyping And Testing Of Controllers For Unmanned Aerial Vehicles
DOWNLOAD
Author : James A. Zanino
language : en
Publisher:
Release Date : 1996-09-01
Uniform System For The Rapid Prototyping And Testing Of Controllers For Unmanned Aerial Vehicles written by James A. Zanino and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1996-09-01 with categories.
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).
In Flight Learning Based Flight Control Of An Unmanned Aircraft System
DOWNLOAD
Author : Mohammed Alabsi
language : en
Publisher:
Release Date : 2018
In Flight Learning Based Flight Control Of An Unmanned Aircraft System written by Mohammed Alabsi and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018 with Drone aircraft categories.
Unmanned Aerial Vehicles (UAVs) popularity has increased substantially in the last few years. UAVs capabilities continue to improve as a result of advances in battery technology, communication, navigation systems and electronics. Increased popularity has driven researchers to improve UAVs reliability and safety which is reflected by the number of publications and accelerating educational programs interest. UAVs are suited for a wide range of civilian and military applications; however, UAVs currently can not integrate with civilian airspace because of stringent safety requirements. Hence, it is necessary to push the envelope for UAVs design and control so that they can learn from nature and have more self-aware capabilities to improve safety and reliability. This dissertation addresses some challenges involved with flight controller learning based on real-time modeling of UAV. Plenty of UAV applications require different operational capabilities within a composite mission. These capabilities include landing and taking off using short runways, while being able to perform missions that require a high cruise speed i.e. tracking applications. A composite mission also requires the aircraft to be able to hover or operate with low cruise speeds for applications involving stationary moments. All of these different operational modes require a hybrid aircraft design that combines fixed wing aircraft capabilities and Vertical Take-Off and Landing (VTOL) aircraft capabilities. However, extensive resources required for hybrid aircraft design prohibited the discovery of different revolutionary designs. The work presented in this dissertation describes the development of a rapid modeling, prototyping and controller design platform of an unmanned quadrotor aircraft. Three main objectives are investigated: intelligent excitation input design, real-time parameter estimation, and learning control. Real-time estimation of dynamic model parameters is important for control adaptation. However, the aircraft model estimation performance can be severely degraded by an active control system and highly collinear model terms such as those found on a quadrotor unmanned aircraft. Recursive Fourier Transform Regression was applied to estimate parameters of different model forms/structures and using different excitation levels. The generated models are utilized to reconfigure a Nonlinear Dynamic Inversion (NDI) controller considering different testing conditions: normal, failure, and learning flights. Finally,an intelligent input design technique is proposed which enables autonomous identification of the vehicle’s response modal frequencies and emphasizes excitation power accordingly.
Design And Integration Of A Flight Management System For The Unmanned Air Vehicle Frog
DOWNLOAD
Author : Timothy C. Rivers
language : en
Publisher:
Release Date : 1998-12-01
Design And Integration Of A Flight Management System For The Unmanned Air Vehicle Frog written by Timothy C. Rivers and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1998-12-01 with categories.
The purpose of this thesis is to design, integrate and flight test a Flight Management System (FMS) for the computer control of an unmanned air vehicle (UAV). By combining modern control design techniques and the capabilities of a Rapid Prototyping System (RPS), we were able to safely go from concept to flight test in a relatively short amount of time without sacrificing thoroughness in computer simulation, code validation and verification, or hardware-in-the-loop ground testing. This ability to quickly field new or modified flight control systems for UAV's is of ever increasing importance as Department of Defense places greater emphasis on the use of UAV's in widely varying mission areas. The primary focus of this thesis is on the design and testing of a heading controller. However, to fully integrate this into the FMS, the research and testing includes airspeed and altitude controllers designed by previous thesis students. Also included as part of the implementation process, is a thorough sensor evaluation to ensure the controller inputs are adequate to support the FMS. The design and test equipment include a highly modified FROG UAV from the U.S. Army, the MATRIX Product Family of software tools developed by Integrated Systems, Inc., and a Ground Station built at NPS from commercially available computer and communication equipment.
Rapid Prototyping Platform For Flight Control System Design
DOWNLOAD
Author : Marius Niculescu
language : en
Publisher:
Release Date : 2000
Rapid Prototyping Platform For Flight Control System Design written by Marius Niculescu and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2000 with Automatic pilot categories.
Rapid Prototyping Software For Avionics Systems
DOWNLOAD
Author : Nicolas Larrieu
language : en
Publisher: John Wiley & Sons
Release Date : 2014-12-03
Rapid Prototyping Software For Avionics Systems written by Nicolas Larrieu and has been published by John Wiley & Sons this book supported file pdf, txt, epub, kindle and other format this book has been release on 2014-12-03 with Computers categories.
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.