Author : Robert C. Nelson
Publisher :
Page : 464 pages
File Size : 43,97 MB
Release : 1998
Category : History
ISBN :
This edition of this this flight stability and controls guide features an unintimidating math level, full coverage of terminology, and expanded discussions of classical to modern control theory and autopilot designs. Extensive examples, problems, and historical notes, make this concise book a vital addition to the engineer's library.
Author : Thomas R. Yechout
Publisher : AIAA
Page : 666 pages
File Size : 20,61 MB
Release : 2003
Category : Aerodynamics
ISBN : 9781600860782
Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.
Author : United States. Federal Aviation Administration
Publisher :
Page : 10 pages
File Size : 45,15 MB
Release : 1983
Category : Airplanes
ISBN :
Author : Tom Proulx
Publisher : Springer Science & Business Media
Page : 362 pages
File Size : 46,80 MB
Release : 2011-04-02
Category : Technology & Engineering
ISBN : 1441993029
Advanced Aerospace Applications, Volume 1. Proceedings of the 29th IMAC, A Conference and Exposition on Structural Dynamics, 2011, the first volume of six from the Conference, brings together 32 contributions to this important area of research and engineering. The collection presents early findings and case studies on fundamental and applied aspects of Structural Dynamics, including papers on Aeroelasticity, Ground Testing, Dynamic Testing of Aerospace Structures, and Random Vibration.
Author : National Research Council
Publisher : National Academies Press
Page : 221 pages
File Size : 34,41 MB
Release : 1997-03-28
Category : Transportation
ISBN : 0309056888
Adverse aircraft-pilot coupling (APC) events include a broad set of undesirable and sometimes hazardous phenomena that originate in anomalous interactions between pilots and aircraft. As civil and military aircraft technologies advance, interactions between pilots and aircraft are becoming more complex. Recent accidents and other incidents have been attributed to adverse APC in military aircraft. In addition, APC has been implicated in some civilian incidents. This book evaluates the current state of knowledge about adverse APC and processes that may be used to eliminate it from military and commercial aircraft. It was written for technical, government, and administrative decisionmakers and their technical and administrative support staffs; key technical managers in the aircraft manufacturing and operational industries; stability and control engineers; aircraft flight control system designers; research specialists in flight control, flying qualities, human factors; and technically knowledgeable lay readers.
Author : Jan Robert Wright
Publisher : John Wiley & Sons
Page : 559 pages
File Size : 24,52 MB
Release : 2008-02-28
Category : Technology & Engineering
ISBN : 047085846X
Aeroelastic phenomena arising from the interaction of aerodynamic, elastic and inertia forces, and the loads resulting from flight / ground manoeuvres and gust / turbulence encounters, have a significant influence upon aircraft design. The prediction of aircraft aeroelastic stability, response and loads requires application of a range of interrelated engineering disciplines. This new textbook introduces the foundations of aeroelasticity and loads for the flexible aircraft, providing an understanding of the main concepts involved and relating them to aircraft behaviour and industrial practice. This book includes the use of simplified mathematical models to demonstrate key aeroelastic and loads phenomena including flutter, divergence, control effectiveness and the response and loads resulting from flight / ground manoeuvres and gust / turbulence encounters. It provides an introduction to some up-to-date methodologies for aeroelastics and loads modelling. It lays emphasis on the strong link between aeroelasticity and loads. It also includes provision of MATLAB and SIMULINK programs for the simplified analyses. It offers an overview of typical industrial practice in meeting certification requirements.
Author :
Publisher : AIAA (American Institute of Aeronautics & Astronautics)
Page : 760 pages
File Size : 45,15 MB
Release : 1995
Category : Technology & Engineering
ISBN :
Author :
Publisher :
Page : 602 pages
File Size : 36,51 MB
Release : 1977
Category : Aerodynamics
ISBN :
Author : Roger Pratt
Publisher : IET
Page : 416 pages
File Size : 42,36 MB
Release : 2000
Category : Technology & Engineering
ISBN : 9780852967669
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)
Author : Eric T. Falangas
Publisher : John Wiley & Sons
Page : 432 pages
File Size : 42,70 MB
Release : 2015-12-03
Category : Technology & Engineering
ISBN : 1119134870
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
