NDLI: V/stol maneuverability and control

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V/stol maneuverability and control

Content Provider	NASA Technical Reports Server (NTRS)
Author	Anderson, S. B. Franklin, J. A.
Copyright Year	1984
Description	Maneuverability and control of V/STOL aircraft in powered-lift flight is studied with specific considerations of maneuvering in forward flight. A review of maneuverability for representative operational mission tasks is presented and covers takeoff, transition, hover, and landing flight phases. Maneuverability is described in terms of the ability to rotate and translate the aircraft and is specified in terms of angular and translational accelerations imposed on the aircraft. Characteristics of representative configurations are reviewed, including experience from past programs and expectations for future designs. The review of control covers the characteristics inherent in the basic airframe and propulsion system and the behavior associated with ontrol augmentation systems. Demands for augmented stability and control response to meet certain mission operational requirements are discussed. Experience from ground-based simulation and flight experiments that illustrates the impact of augmented stability and control on aircraft design is related by example.
File Size	4917493
Page Count	56
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19840014516
Archival Resource Key	ark:/13960/t2b903m77
Language	English
Publisher Date	1984-04-01
Access Restriction	Open
Subject Keyword	Aircraft Stability And Control Horizontal Flight V/stol Aircraft Airframes Stability Augmentation Aircraft Maneuvers Aircraft Design Powered Lift Aircraft Aircraft Configurations Propulsion System Configurations Aircraft Control Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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