Dynamics, control, and flying qualities of V/STOL aircraft

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Bibliographic Details
Main Author: Franklin, James A.
Format: eBook
Language:English
Published: Reston, Va. : American Institute of Aeronautics and Astronautics, c2002.
Series:AIAA education series.
Subjects:
Online Access:Subscribed ebook (available only in University campus-wide network);click to view
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010 |z  2002015061 
020 |z 1563475758 (alk. paper) 
020 |z 9781563475757 
020 |z 9781600860478 (e-book) 
040 |a CaPaEBR  |c CaPaEBR 
035 |a (OCoLC)607774930 
050 1 4 |a TL685  |b .F73 2002eb 
082 0 4 |a 629.133/35  |2 21 
100 1 |a Franklin, James A. 
245 1 0 |a Dynamics, control, and flying qualities of V/STOL aircraft  |h [electronic resource] /  |c James A. Franklin. 
260 |a Reston, Va. :  |b American Institute of Aeronautics and Astronautics,  |c c2002. 
300 |a xvi, 210 p. :  |b ill. 
490 1 |a AIAA education series 
504 |a Includes bibliographical references (p. 203-205) and index. 
505 0 |a Representative operations of V/STOL aircraft -- Control strategy and desired control characteristics -- Equations of motion for Hover and forward flight -- Longitudinal flying qualities in Hover -- Lateral-directional flying qualities in Hover -- Longitudinal flying qualities in forward flight -- Lateral-directional flying qualities in forward flight -- Response to wind and turbulence -- Control augmentation and cockpit displays -- Aircraft stability derivatives. 
533 |a Electronic reproduction.  |b Palo Alto, Calif. :  |c ebrary,  |d 2013.  |n Available via World Wide Web.  |n Access may be limited to ebrary affiliated libraries. 
650 0 |a Vertically rising aircraft. 
650 0 |a Short take-off and landing aircraft. 
650 0 |a Short take-off and landing aircraft  |x Handling characteristics. 
650 0 |a Airplanes  |x Control systems. 
655 7 |a Electronic books.  |2 local 
830 0 |a AIAA education series. 
856 4 0 |u http://site.ebrary.com/lib/unicalicut/Doc?id=10516408  |z Subscribed ebook (available only in University campus-wide network);click to view 
952 |a ON  |c EBR  |y EB 
999 |c ebr10516408