Stability and Control of Maneuvering High-performance Aircraft
Author : Robert F. Stengel
Publisher :
Page : 212 pages
File Size : 33,95 MB
Release : 1977
Category : Airplanes
ISBN :
Author : Robert F. Stengel
Publisher :
Page : 212 pages
File Size : 33,95 MB
Release : 1977
Category : Airplanes
ISBN :
Author : Robert F. Stengel
Publisher :
Page : 212 pages
File Size : 15,60 MB
Release : 1977
Category : Airplanes
ISBN :
Author : Thomas R. Yechout
Publisher : AIAA
Page : 666 pages
File Size : 27,12 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 : Robert C. Nelson
Publisher : WCB/McGraw-Hill
Page : 441 pages
File Size : 34,46 MB
Release : 1998
Category : Aerodynamique / Aeronautique / Aerospatial / Automatique / Avion / Commande / Conception / Controle / Navigation / Stabilite
ISBN : 9780071158381
The second edition of Flight Stability and Automatic Control presents an organized introduction to the useful and relevant topics necessary for a flight stability and controls course. Not only is this text presented at the appropriate mathematical level, it also features standard terminology and nomenclature, along with expanded coverage of classical control theory, autopilot designs, and modern control theory. Through the use of extensive examples, problems, and historical notes, author Robert Nelson develops a concise and vital text for aircraft flight stability and control or flight dynamics courses.
Author : Edward Seckel
Publisher :
Page : 532 pages
File Size : 49,97 MB
Release : 1964
Category : Stability of airplanes
ISBN :
Stability and Control of Airplanes and Helicopters deals with aircraft flying qualities that determine the stability and control of airplanes and helicopters. It includes problems based on real aircraft, selected to represent the gamut from simple to complicated, and from conventional utility designs to futuristic research types. Many of these problems involve comparison of theory and experiment to demonstrate their mutual relationship.
Author : Robert F. Stengel
Publisher :
Page : 295 pages
File Size : 12,8 MB
Release : 1976
Category :
ISBN :
High-performance aircraft are susceptible to degraded flying qualities during maneuvering flight for a number of reasons, including aerodynamic nonlinearities, inertial coupling, and rapidly changing flight condition. Lateral-directional modes of motion coupled with longitudinal motions in asymmetric flight and high angle of attack can lead to instability and adverse control response. The pilot must adapt his control strategies to varying aircraft dynamics, and his work load is high; consequently, improper piloting procedures could occur, leading to inadvertent loss of control.
Author : Bandu N. Pamadi
Publisher : AIAA (American Institute of Aeronautics & Astronautics)
Page : 792 pages
File Size : 47,49 MB
Release : 1998
Category : Science
ISBN :
A textbook for a two-semester senior undergraduate or first-year graduate course in aerospace. Includes the necessary background material on basic aerodynamics, dynamics, and linear control. Assumes the airplane is a rigid body and therefore does not consider elastic deformations and their effects on an airplane's motion. Includes a number of solved examples to illustrate the theory and basic principles, and several exercise problems to help develop problem- solving skills. Annotation copyrighted by Book News, Inc., Portland, OR
Author : Edward Seckel
Publisher : Academic Press
Page : 523 pages
File Size : 45,95 MB
Release : 2014-05-10
Category : Technology & Engineering
ISBN : 148322015X
Stability and Control of Airplanes and Helicopters deals with aircraft flying qualities that determine the stability and control of airplanes and helicopters. It includes problems based on real aircraft, selected to represent the gamut from simple to complicated, and from conventional utility designs to futuristic research types. Many of these problems involve comparison of theory and experiment to demonstrate their mutual relationship. Comprised of 25 chapters, this book begins with a discussion on the aerodynamics of the component parts related to the lift and moment characteristics of an airplane, including wings and associated accessories; bodies such as fuselages, nacelles, and tip tanks; and control surfaces. The reader is then introduced to some mathematical techniques for linear differential equations; steady flight at different speeds; and stick force and control-free stability. Subsequent chapters focus on flaps and high-lift devices; power and compressibility effects; and the manner in which the aircraft responds to the application of control. Aeroelasticity and longitudinal equations of motion are also examined. This monograph is intended for undergraduate and graduate students taking modern engineering courses.
Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
Page : 70 pages
File Size : 32,49 MB
Release : 2018-07-10
Category :
ISBN : 9781722671129
This research should lead to the development of new nonlinear methodologies for the adaptive control and stability analysis of high angle-of-attack aircraft such as the F18 (HARV). The emphasis has been on nonlinear adaptive control, but associated model development, system identification, stability analysis and simulation is performed in some detail as well. Various models under investigation for different purposes are summarized in tabular form. Models and simulation for the longitudinal dynamics have been developed for all types except the nonlinear ordinary differential equation model. Briefly, studies completed indicate that nonlinear adaptive control can outperform linear adaptive control for rapid maneuvers with large changes in alpha. The transient responses are compared where the desired alpha varies from 5 degrees to 60 degrees to 30 degrees and back to 5 degrees in all about 16 sec. Here, the horizontal stabilator is the only control used with an assumed first-order linear actuator with a 1/30 sec time constant. Mohler, R. R. Unspecified Center...
Author : Angelo Miele
Publisher :
Page : 42 pages
File Size : 18,6 MB
Release : 1959
Category : Airplanes
ISBN :