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Book Masters Theses in the Pure and Applied Sciences

Download or read book Masters Theses in the Pure and Applied Sciences written by Wade H. Shafer and published by Springer Science & Business Media. This book was released on 2012-12-06 with total page 426 pages. Available in PDF, EPUB and Kindle. Book excerpt: Masters Theses in the Pure and Applied Sciences was first conceived, published, and disseminated by the Center for Information and Numerical Data Analysis and Synthesis (CINDAS)* at Purdue University in 1957, starting its coverage of theses with the academic year 1955. Beginning with Volume 13, the printing and dis semination phases of the activity were transferred to University Microfilms/Xerox of Ann Arbor, Michigan, with the thought that such an arrangement would be more beneficial to the academic and general scientific and technical community. After five years of this joint undertaking we had concluded that it was in the interest of all concerned if the printing and distribution of the volumes were handled by an international publishing house to assure improved service and broader dissemination. Hence, starting with Volume 18, Masters Theses in the Pure and Applied Sciences has been disseminated on a worldwide basis by Plenum Publishing Corporation of New York, and in the same year the coverage was broadened to include Canadian universities. All back issues can also be ordered from Plenum. We have reported in Volume 38 (thesis year 1993) a total of 13,787 thesis titles from 22 Canadian and 164 United States universities. We are sure that this broader base for these titles reported will greatly enhance the value of this impor tant annual reference work. While Volume 38 reports theses submitted in 1993, on occasion, certain uni versities do report theses submitted in previous years but not reported at the time.

Book Scientific and Technical Aerospace Reports

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 456 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Book Masters Theses in the Pure and Applied Sciences

Download or read book Masters Theses in the Pure and Applied Sciences written by Sade H Shafer and published by Springer Science & Business Media. This book was released on 1995 with total page 440 pages. Available in PDF, EPUB and Kindle. Book excerpt: Cited in Sheehy, Chen, and Hurt . Volume 38 (thesis year 1993) reports a total of 13,787 thesis titles from 22 Canadian and 164 US universities. As in previous volumes, thesis titles are arranged by discipline and by university within each discipline. Any accredited university or college with a grad

Book Conceptual   Preliminary Design of a Vertical Take Off and Landing UAV with High Endurance

Download or read book Conceptual Preliminary Design of a Vertical Take Off and Landing UAV with High Endurance written by Todor Ilchev Ilchevski and published by . This book was released on 2021 with total page 145 pages. Available in PDF, EPUB and Kindle. Book excerpt: The goal for this project is to conduct a conceptual design study of an unmanned vertical take-off and landing electric aircraft with maximum take-off mass of 25kg. The aircraft in question features the PICOMA (Pitch Control by Mass Actuation) patented concept, which is used to control the stability of the aircraft around its lateral axis by moving a mass along its longitudinal one. Previously, two separate design studies were performed on aircraft using the PICOMA concept and the gathered experience, where possible, is applied to this project.This report includes the creation of the needed CAD models, performance calculations for the vertical and horizontal flight phases, and the CFD analysis performed on the aerodynamic surfaces of the airplane. Furthermore, the used design methods are outlined in the report along with several identified design challenges, stemming from the unique control mechanism of the aircraft. Respectively, possible solutions to the design challenges are proposed and discussed throughout this report.*****The goal for this project is to conduct a conceptual design study of an unmanned vertical take-off and landing electric aircraft with maximum take-off mass of 25kg. The aircraft in question features the PICOMA (Pitch Control by Mass Actuation) patented concept, which is used to control the stability of the aircraft around its lateral axis by moving a mass along its longitudinal one. Previously, two separate design studies were performed on aircraft using the PICOMA concept and the gathered experience, where possible, is applied to this project.This report includes the creation of the needed CAD models, performance calculations for the vertical and horizontal flight phases, and the CFD analysis performed on the aerodynamic surfaces of the airplane. Furthermore, the used design methods are outlined in the report along with several identified design challenges, stemming from the unique control mechanism of the aircraft. Respectively, possible so

Book Unmanned Aerial Vehicles

Download or read book Unmanned Aerial Vehicles written by United States. General Accounting Office and published by . This book was released on 1990 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aeronautical Engineering

Download or read book Aeronautical Engineering written by and published by . This book was released on 1991 with total page 538 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Unmanned Aerial Vehicles   More Testing Needed Before Production of Short range System

Download or read book Unmanned Aerial Vehicles More Testing Needed Before Production of Short range System written by United States. General Accounting Office and published by . This book was released on 1992 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Data Link Development for the Archytas Vertical Takeoff and Landing Transitional Flight Unmanned Aerial Vehicle

Download or read book Data Link Development for the Archytas Vertical Takeoff and Landing Transitional Flight Unmanned Aerial Vehicle written by Frederick W. Reichert and published by . This book was released on 1993 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt: This thesis chronicles the development of a data link for the Archytas, a vertical takeoff and landing, transitional flight unmanned aerial vehicle (UAV) prototype being built by the Aeronautics Department at the Naval Postgraduate School. Archytas is intended to be a proof-of-concept platform to satisfy the Navy's real-time, over-the-horizon intelligence mission with a UAV that could be launched and recovered from a small combatant ship. This thesis provides a history of the Archytas command and control data link development, a full description of the data link as delivered for use on the prototype, principles for near term enhancements, and future considerations for the data link should the Archytas concept be adapted for use in an operational combat environment.

Book Data Link Development for the Archytas Vertical Takeoff and Landing Transitional Flight Unmanned Aerial Vehicle

Download or read book Data Link Development for the Archytas Vertical Takeoff and Landing Transitional Flight Unmanned Aerial Vehicle written by and published by . This book was released on 1993 with total page 95 pages. Available in PDF, EPUB and Kindle. Book excerpt: This thesis chronicles the development of a data link for the Archytas, a vertical takeoff and landing, transitional flight unmanned aerial vehicle (UAV) prototype being built by the Aeronautics Department at the Naval Postgraduate School. Archytas is intended to be a proof-of-concept platform to satisfy the Navy's real-time, over-the-horizon intelligence mission with a UAV that could be launched and recovered from a small combatant ship. This thesis provides a history of the Archytas command and control data link development, a full description of the data link as delivered for use on the prototype, principles for near term enhancements, and future considerations for the data link should the Archytas concept be adapted for use in an operational combat environment.

Book Unmanned Aircraft Design

Download or read book Unmanned Aircraft Design written by Mohammad Sadraey and published by Morgan & Claypool Publishers. This book was released on 2017-09-19 with total page 211 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book provides fundamental principles, design procedures, and design tools for unmanned aerial vehicles (UAVs) with three sections focusing on vehicle design, autopilot design, and ground system design. The design of manned aircraft and the design of UAVs have some similarities and some differences. They include the design process, constraints (e.g., g-load, pressurization), and UAV main components (autopilot, ground station, communication, sensors, and payload). A UAV designer must be aware of the latest UAV developments; current technologies; know lessons learned from past failures; and they should appreciate the breadth of UAV design options. The contribution of unmanned aircraft continues to expand every day and over 20 countries are developing and employing UAVs for both military and scientific purposes. A UAV system is much more than a reusable air vehicle or vehicles. UAVs are air vehicles, they fly like airplanes and operate in an airplane environment. They are designed like air vehicles; they have to meet flight critical air vehicle requirements. A designer needs to know how to integrate complex, multi-disciplinary systems, and to understand the environment, the requirements and the design challenges and this book is an excellent overview of the fundamentals from an engineering perspective. This book is meant to meet the needs of newcomers into the world of UAVs. The materials are intended to provide enough information in each area and illustrate how they all play together to support the design of a complete UAV. Therefore, this book can be used both as a reference for engineers entering the field or as a supplementary text for a UAV design course to provide system-level context for each specialized topic.

Book Tipjet VTOL UAV  Vertical Takeoff and Landing Unmanned Aerial Vehicle  Summary  Volume 1  1200 Pound Tipjet VTOL Unmanned Aerial Vehicle  Part 1  Conceptual Design Study of a 1200 Pound Vehicle

Download or read book Tipjet VTOL UAV Vertical Takeoff and Landing Unmanned Aerial Vehicle Summary Volume 1 1200 Pound Tipjet VTOL Unmanned Aerial Vehicle Part 1 Conceptual Design Study of a 1200 Pound Vehicle written by and published by . This book was released on 1989 with total page 79 pages. Available in PDF, EPUB and Kindle. Book excerpt: A new concept is developed for an unmanned aerial vehicle (UAV) configured with a tip-jet driven, two-bladed, stoppable rotor and circulation control airfoils. The conceptual design of the Tipjet Vertical Takeoff and Landing (VTOL) UAV is presented, and vehicle performance is evaluated for three mid-range UAV Navy missions: Tactical Reconnaissance, Over-the-Horizon Targeting, and Combat Support Reconnaissance. Vehicle performance predictions are presented for hover and low-speed, rotary-wing flight, for conversion between rotary-wing and fixed-wing flight, and for fixed-wing flight. Requirements for shipboard support of the vehicle are outlined. Mission specific equipment is described including size, weight, and power requirements. Standard design methods are applied to conduct a detailed mission performance analysis for the conceptual design. The analysis results indicate that the 1200-1b Tipjet VTOL UAV is a viable candidate vehicle for the specified missions. Moreover, the concept is directly applicable to much larger UAVs that will greatly enhance naval warfare capabilities. Part 1 of Volume I presents the conceptual design for the Tipjet VTOL UAV along with vehicle performance analysis for the designed missions. Part 2 of Volume I presents the detailed engine and vehicle performance data. This proprietary information is available upon request to qualified agencies.

Book Embedded Platforms for UAS Landing Path and Obstacle Detection

Download or read book Embedded Platforms for UAS Landing Path and Obstacle Detection written by Umberto Papa and published by Springer. This book was released on 2018-01-05 with total page 115 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book reports on the design and development of a system that assists remote pilots during the landing procedure. In particular, it covers a previously neglected topic, namely the search for the best pathway and landing site. It describes the system’s components, such as the ultrasonic sensor, infrared sensor and optical sensor, in detail, and discusses the experimental tests carried out in both controlled laboratory and real-world environments. Providing a fascinating survey of the state of the art in the field of unmanned aircraft system electronics design and development, the book also presents recent advances in and cutting-edge methodologies for the development of acquisition systems and inexpensive sensor design for navigation data.

Book American Military Helicopters and Vertical Short Landing and Takeoff Aircraft Since 1941

Download or read book American Military Helicopters and Vertical Short Landing and Takeoff Aircraft Since 1941 written by E.R. Johnson and published by McFarland. This book was released on 2021-11-01 with total page 495 pages. Available in PDF, EPUB and Kindle. Book excerpt: Over the past eight decades, developments in vertical lift aircraft--both helicopters and vertical/short takeoff and landing (V/STOL) planes--have given the American military unparalleled capabilities on the modern battlefield. The U.S. has led the world in vertical lift technologies with the help of some of the brightest minds in this field--Igor I. Sikorsky, Arthur M. Young, Frank N. Piasecki, Charles H. Kaman and Stanley Hiller, Jr., to name a few--and by having the industrial prowess to make their concepts reality. This book provides a concise historical survey, including technical specifications, drawings, and photographs of every type of helicopter and V/STOL aircraft developed for the U.S. military, from the earliest examples tested in 1941 and 1942, up to the newest prototypes.

Book Three Tier Unmanned Areial Vehicle

Download or read book Three Tier Unmanned Areial Vehicle written by Alankar Chhabra and published by . This book was released on 1999 with total page 170 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Conceptual Design  Development  and Simulation of a Tilt duct Unmanned Aerial Vehicle with Vertical Takeoff and Landing Capabilities

Download or read book Conceptual Design Development and Simulation of a Tilt duct Unmanned Aerial Vehicle with Vertical Takeoff and Landing Capabilities written by Peter Gabriel Cross and published by . This book was released on 2006 with total page 530 pages. Available in PDF, EPUB and Kindle. Book excerpt: "Unmanned aerial vehicles possessing vertical takeoff and landing capabilities are receiving growing interest within the aerospace industry, as these aircraft can be operated in areas and on missions that preclude the use of conventional aircraft. This thesis presents the development and analysis of the triple tilt-duct aircraft configuration, an aircraft design suited for future generations of VTOL UAVs. The development of a conceptual design for a small-scale, "proof of concept" tilt-duct UAV is presented, culminating in a description of the final conceptual design. The methodology for a detailed analysis of the performance and the stability and control characteristics of the tilt-duct UAV design is outlined, along with the results from these analyses. The tilt-duct UAV has good stability and handling characteristics when in horizontal flight mode, but is highly unstable when hovering or in vertical flight mode. A study of the motion of the tilt-duct aircraft during transition maneuvers between horizontal and vertical flight modes is also presented; schemes for performing optimal transition maneuvers and maintaining adequate pitch control during the transitions are given as well. A flight simulation model was utilized to test the performance and stability and control of the tilt-duct UAV. Though it was not possible to accurately simulate transition maneuvers with the software package used, it was possible to obtain reasonable measurements of the aircraft's performance and response to control inputs. An outlook for the triple tilt-duct configuration is given, along with suggestions for future research. It is felt that the triple tilt-duct configuration is a viable design for future VTOL aircraft"--Abstract, leaf iii.

Book Unmanned Aerial Vehicle Design and Technology

Download or read book Unmanned Aerial Vehicle Design and Technology written by T. Hikmet Karakoc and published by Springer Nature. This book was released on 2023-12-19 with total page 197 pages. Available in PDF, EPUB and Kindle. Book excerpt: Unmanned Aerial Vehicle Design and Technology provides readers with a comprehensive introduction to unmanned aerial systems (UAS) technology basics. The book presents clear, concise guidance on UAS system design, components, control, and operations fundamentals. Additional chapters look at unmanned aerial regulations and ethics and the historical background of UAS technology. This textbook offers a well-rounded look at unmanned flight technology, making it an ideal primer for aviation and aerospace students and anyone interested in learning more about unmanned aerial systems, including engineers, technicians, drone and flight hobbyists, and civil aviation organization officials.