Introduction to the design of fixed-wing micro air vehicles : including three case studies
Author(s)
Bibliographic Information
Introduction to the design of fixed-wing micro air vehicles : including three case studies
(AIAA education series)
American Institute of Aeronautics and Astronautics, c2007
Available at 13 libraries
  Aomori
  Iwate
  Miyagi
  Akita
  Yamagata
  Fukushima
  Ibaraki
  Tochigi
  Gunma
  Saitama
  Chiba
  Tokyo
  Kanagawa
  Niigata
  Toyama
  Ishikawa
  Fukui
  Yamanashi
  Nagano
  Gifu
  Shizuoka
  Aichi
  Mie
  Shiga
  Kyoto
  Osaka
  Hyogo
  Nara
  Wakayama
  Tottori
  Shimane
  Okayama
  Hiroshima
  Yamaguchi
  Tokushima
  Kagawa
  Ehime
  Kochi
  Fukuoka
  Saga
  Nagasaki
  Kumamoto
  Oita
  Miyazaki
  Kagoshima
  Okinawa
  Korea
  China
  Thailand
  United Kingdom
  Germany
  Switzerland
  France
  Belgium
  Netherlands
  Sweden
  Norway
  United States of America
Note
Includes bibliographical references and index
Other authors: James C. Kellogg, Peter G. Ifju, Sergey V. Shkarayev
Description and Table of Contents
Description
This intriguing book breaks new ground on an emerging subject that has attracted considerable attention: the use of unmanned Micro Air Vehicles (MAVs) to conduct special, limited duration missions. Significant advances in the miniaturization of electronics make it now possible to use vehicles of this type in a detection or surveillance role to carry visual, acoustic, chemical, or biological sensors. Interestingly, many of the advances in MAV technology can be traced directly to annual student competitions, begun in the late 1990s, that use relatively low cost model airplane equipment. The wide variety of configurations entered in these contests and their ongoing success has led to a serious interest in testing the performance of these vehicles for adaptation to practical applications. MAVs present aerodynamic issues unique to their size and the speeds at which they operate. Of particular concern is the aerodynamic efficiency of various fixed wing concepts. Very little information on the performance of low aspect ratio wing planforms existed for this flight regime until MAVs became of interest and the proliferation of fixed wing designs has since expanded.This book presents a brief history of unmanned air vehicles and offers elements of aerodynamics for low aspect ratio wings. Propulsion and the basic concepts for fixed wing MAV design are presented, as is a method for autopilot integration. Three different wing configurations are presented in a series of step-by-step case studies. The goal of the book is to assist both working professionals and students to design, build, and fly MAVs, and do so in a way that will advance the state of the art and lead to the development of even smaller aircraft.
Table of Contents
- * An Overview of Micro Air Vehicle Development
- * Elements of Aerodynamics, Propulsion, and Design
- * Autopilot Integration into Micro Air Vehicles
- * Case Study: The Micro Tactical Expendable (MITE) Rigid-Wing Micro Air Vehicle
- * Case Study: Flexible Wing Micro Air Vehicles
- * Case Study: Development of Micro Air Vehicles with In-Flight Adaptive Wing
- * Summary.
by "Nielsen BookData"