Author: Charles R. ChalkPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 36
Book Description
Additional Flight Evaluations of Various Longitudinal Handling Qualities in a Variable-stability Jet Fighter
Author: Charles R. ChalkPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 36
Book Description
Additional Flight Evaluations of Various Longitudinal Handling Qualities in a Variable-stability Jet Fighter
Author: Charles R. ChalkPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 27
Book Description
Flight Stability and Automatic Control
Author: Robert C. NelsonPublisher:
ISBN:
Category : History
Languages : en
Pages : 464
Book Description
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.
Simulator Study of Stall/post-stall Characteristics of a Fighter Airplane with Relaxed Longitudinal Static Stability
Author: U.S. Government Research Reports
Author: Flight Dynamics Principles
Author: M. V. CookPublisher: Butterworth-Heinemann
ISBN: 0080982425
Category : Business & Economics
Languages : en
Pages : 609
Book Description
Previous ed.: 2007. - Includes index.
NASA Technical Note
Author: Fixed-base Simulator Investigation of the Effects of L [alpha] and True Speed on Pilot Opinion of Longitudinal Flying Qualities
![Fixed-base Simulator Investigation of the Effects of L [alpha] and True Speed on Pilot Opinion of Longitudinal Flying Qualities PDF](https://books.google.com/books/content/images/frontcover/mFoAp9wGVrQC?fife=w80-h100)
Author: Charles R. ChalkPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 174
Book Description
The study is directed toward investigating the effects on pilots rating of large variations (L alpha) in the relative amplitude and phase of the basic airplane responses to elevator control. The effects of L alpha and true speed on longitudinal flying qualities, optimum control gain, and normal acceleration response to turbulence were investigated in a ground simulator. The steady state ratio of normal acceleration to angle of attack was found to be of significance both to the flying qualities of an airplane and to the optimum longitudinal control gain. Normal acceleration response to rough air was demonstrated to be primarily a function of L alpha and the short period frequency and damping ratio.
Flight Dynamics Principles
Author: Michael V. CookPublisher: Elsevier
ISBN: 0080550363
Category : Technology & Engineering
Languages : en
Pages : 491
Book Description
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 comprehensive grounding in the theory of automatic control. Flight Dynamics Principles provides all three in an accessible and student focussed text. Written for those coming to the subject for the first time the book is suitable as a complete first course text. It provides a secure foundation from which to move on to more advanced topics such a non-linear flight dynamics, simulation and advanced flight control, and is ideal for those on course including flight mechanics, aircraft handling qualities, aircraft stability and control. Enhances by detailed worked examples, case studies and aircraft operating condition software, this complete course text, by a renowned flight dynamicist, is widely used on aircraft engineering courses - Suitable as a complete first course text, it provides a secure foundation from which to move on to more advanced topics such a non-linear flight dynamics, simulation and advanced flight control - End of chapter exercises, detailed worked examples, and case studies aid understanding and relate concepts to real world applications - Covers key contemporary topics including all aspects of optimization, emissions, regulation and automatic flight control and UAVs - Accompanying MathCAD software source code for performance model generation and optimization
Author: