V/STOL Maneuverability and Control
Author :
Publisher :
Page : 54 pages
File Size : 19,14 MB
Release : 1984
Category :
ISBN :
Author :
Publisher :
Page : 54 pages
File Size : 19,14 MB
Release : 1984
Category :
ISBN :
Author : James A. Franklin
Publisher : AIAA
Page : 240 pages
File Size : 21,70 MB
Release : 2002
Category : Airplanes
ISBN : 9781600860478
Annotation This text presents the principles of dynamics and control for vertical, short take-off landing (V/STOL) aircraft. It is the first book of its kind. It is intended for graduate students and professionals in aeronautics who have knowledge of linear systems analysis, aircraft static, dynamic stability, and control. The text begins with a discussion of V/STOL aircraft operations. Control strategies, equations of motion, longitudinal and lateral-directional flying qualities in both hover and forward flight, wind and turbulence responses, and control augmentation and cockpit displays are covered. Specific examples of the YAV-8B Harrier and XV-15 Tilt Rotor aircraft are used to illustrate actual V/STOL dynamic and control characteristics.
Author : Frank R. Niessen
Publisher :
Page : 20 pages
File Size : 19,51 MB
Release : 1969
Category : Airplanes
ISBN :
In-flight simulation to evaluate simultaneous use of attitude control for jet VTOL maneuvering.
Author :
Publisher :
Page : 52 pages
File Size : 40,15 MB
Release : 1984
Category :
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Author :
Publisher :
Page : 996 pages
File Size : 19,5 MB
Release : 1990
Category : Aeronautics
ISBN :
Author : Walter Z. Collings
Publisher :
Page : 212 pages
File Size : 16,80 MB
Release : 1979
Category : Aeronautics, Military
ISBN :
Author : Terrell W. Feistel
Publisher :
Page : 18 pages
File Size : 41,28 MB
Release : 1969
Category : Aeronautical instruments
ISBN :
Author : Benjamin Gal-Or
Publisher : Springer Science & Business Media
Page : 277 pages
File Size : 47,43 MB
Release : 2013-11-09
Category : Technology & Engineering
ISBN : 1461389615
This book is designed to fill a professional vacuum in the new field of advance, high-angle, vectored stealth aircraft. The subject matter presented in the volume has never before been investigated and presented as a unified field of study because it covers entirely new fields and because specialized fragments of this unified field are scattered throughout literature in specific problems. The book is of interest to aeronautical and mechanical engineers, electrical and control engineers, aerospace industry, USAF, US Navy, NASA, pilots and instructors.
Author : Seth B. Anderson
Publisher :
Page : 56 pages
File Size : 28,63 MB
Release : 1960
Category : Flight control
ISBN :
A study has been undertaken to define hand-ling qualities criteria for V/STOL aircraft. With the current military requirements for helicopters and airplanes as a framework, modifications and additions were made for conversion to a preliminary set of V/STOL requirements using a broad background of flight experience and pilots' comments from VTOL and STOL aircraft, BLC (boundary-layer-control) equipped aircraft, variable stability aircraft, flight simulators and landing approach studies. The report contains a discussion of the reasoning behind and the sources of information leading to suggested requirements. The results of the study indicate that the majority of V/STOL requirements can be defined by modifications to the helicopter and/or airplane requirements by appropriate definition of reference speeds. Areas where a requirement is included but where the information is felt to be inadequate to establish a firm quantitative requirement include the following: Control power and damping relationships about all axes for various sizes and types of aircraft; control power, sensitivity, d-amping and response for height control; dynamic longitudinal and dynamic lateral- directional stability in the transition region, including emergency operation; hovering steadiness; acceleration and deceleration in transition; descent rates and flight-path angles in steep approaches, and thrust margin for approach.
Author :
Publisher :
Page : 116 pages
File Size : 23,3 MB
Release : 1974
Category : Fan-in-wing aircraft
ISBN :