Aircraft Motion Sensitivity to Dynamic Stability Derivatives
Author : T. F. Langham
Publisher :
Page : 146 pages
File Size : 46,14 MB
Release : 1980
Category : Angle of attack (Aerodynamics)
ISBN :
Author : T. F. Langham
Publisher :
Page : 146 pages
File Size : 46,14 MB
Release : 1980
Category : Angle of attack (Aerodynamics)
ISBN :
Author : T. F. Langham
Publisher :
Page : 116 pages
File Size : 31,28 MB
Release : 1980
Category : Guided missiles
ISBN :
A dynamic derivative sensitivity study was conducted to demonstrate the importance of dynamic derivatives in missile motion simulation studies. Generalized bank-to-turn and yaw-to-turn missile configurations were used with a six-degree-of-freedom linearized stability program. The effects of various dynamic derivatives on missile stability were investigated in both level and turning flight for several Mach numbers and altitude conditions.
Author : Thomas R. Yechout
Publisher : AIAA
Page : 666 pages
File Size : 23,87 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 :
Page : 464 pages
File Size : 17,95 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 : Jan Roskam
Publisher : DARcorporation
Page : 612 pages
File Size : 49,37 MB
Release : 1998
Category : Science
ISBN : 9781884885174
Author : Bernard Etkin
Publisher : John Wiley & Sons
Page : 392 pages
File Size : 48,3 MB
Release : 1982
Category : Technology & Engineering
ISBN :
Author : R. W. Butler
Publisher :
Page : 60 pages
File Size : 42,60 MB
Release : 1976
Category : Damping (Mechanics).
ISBN :
An investigation was conducted to provide some insight into the importance of dynamic cross and cross-coupling derivatives in motion simulation studies of fighter aircraft in the maneuvering flight regime. The aircraft motion sensitivity to the various derivatives is ascertained in level and turning flight utilizing a 5 deg of freedom linearized stability program. The results are presented in a root locus format.
Author : Michael V. Cook
Publisher : Butterworth-Heinemann
Page : 608 pages
File Size : 36,85 MB
Release : 2012-10-03
Category : Technology & Engineering
ISBN : 008098276X
The study of flight dynamics requires a thorough understanding of the theory of the stability and control of aircraft, an appreciation of flight control systems and a grounding in the theory of automatic control. Flight Dynamics Principles is a student focused text and provides easy access to all three topics in an integrated modern systems context. Written for those coming to the subject for the first time, the book provides a secure foundation from which to move on to more advanced topics such as, non-linear flight dynamics, flight simulation, handling qualities and advanced flight control. - Additional examples to illustrate the application of computational procedures using tools such as MATLAB®, MathCad® and Program CC® - Improved compatibility with, and more expansive coverage of the North American notational style - Expanded coverage of lateral-directional static stability, manoeuvrability, command augmentation and flight in turbulence - An additional coursework study on flight control design for an unmanned air vehicle (UAV)
Author : David G. Hull
Publisher : Springer Science & Business Media
Page : 311 pages
File Size : 18,82 MB
Release : 2007-01-20
Category : Technology & Engineering
ISBN : 3540465731
Flight mechanics is the application of Newton's laws to the study of vehicle trajectories (performance), stability, and aerodynamic control. This volume details the derivation of analytical solutions of airplane flight mechanics problems associated with flight in a vertical plane. It covers trajectory analysis, stability, and control. In addition, the volume presents algorithms for calculating lift, drag, pitching moment, and stability derivatives. Throughout, a subsonic business jet is used as an example for the calculations presented in the book.
Author :
Publisher :
Page : 464 pages
File Size : 33,79 MB
Release : 1995
Category : Aeronautics
ISBN :