NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
V/STOL Dynamics, Control, and Flying QualitiesThis publication presents material that constituted the lectures presented by the author as part of Course AA 234, Dynamics, Control, and Flying Qualities of Vertical/Short Takeoff and Landing (V/STOL) Aircraft that was taught in the Department of Aeronautics and Astronautics at Stanford University. It covers representative operations of vertical and short takeoff and landing (V/STOL) aircraft, a discussion of the pilot's strategy in controlling these aircraft, the equations of motion pertinent to V/STOL tasks, and their application in the analysis of longitudinal and lateral-directional control in hover and forward flight. Following that development, which applies to the characteristics of the basic airframe and propulsion system, the text concludes with a discussion of the contributions of control augmentation in specific flight tasks and of the integration of modern electronic displays with these controls.
Document ID
20010038495
Acquisition Source
Ames Research Center
Document Type
Technical Publication (TP)
Authors
Franklin, James A.
(NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
September 7, 2013
Publication Date
October 1, 2000
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.60:209591
A-0003625
NASA/TP-2000-209591
Report Number: NAS 1.60:209591
Report Number: A-0003625
Report Number: NASA/TP-2000-209591
Funding Number(s)
PROJECT: RTOP 706-25-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available