An Analytical Study Of V Stol Handling Qualities In Hover And Transition
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An Analytical Study of V STOL Handling Qualities in Hover and Transition
Author | : R. L. Stapleford |
Publsiher | : Unknown |
Total Pages | : 174 |
Release | : 1965 |
Genre | : Airplanes |
ISBN | : UOM:39015095310135 |
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The hover analysis considers pilot attitude and position control tasks in the presence of horizontal gusts. The effects of each of the stability derivatives on the difficulty of the control tasks and on the closed-loop gust responses are determined. It is clearly shown that the handling qualities studies of control sensitivity and angular damping must consider the influences of M sub u (or L sub v) and should include gust inputs. These conclusions are substantiated by previous variable-stability-helicopter experiments. The effects of vehicle size and geometry are investigated by several approaches. The key result of increasing size is found to be a reduction in M sub u and L sub v which can, in turn, lower the requirements for control power and damping. The handling qualities during transition of two vehicles, a tilt duct and a tilt wing, which were previously tested on a simulator are analyzed. It is shown that both trim control and perturbations about the trim conditions must be considered. In fact, part of the increased difficulty in landing transitions, in comparison with takeoff transitions, is due to more difficult trim control; the much more stringent position control requirements in landing are also a contributing factor.
Conference on V STOL and STOL Aircraft Ames Research Center Moffett Field California April 4 5 1966
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 486 |
Release | : 1966 |
Genre | : Short take-off and landing aircraft |
ISBN | : NASA:31769000653124 |
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Initial VTOL Flight Control Design Criteria Development Discussion of Selected Handling Qualities Topics
Author | : John Kroll (Jr.) |
Publsiher | : Unknown |
Total Pages | : 76 |
Release | : 1968 |
Genre | : Helicopters |
ISBN | : UOM:39015095298553 |
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"This report presents a series of discussions on selected topics related to the development of VTOL flying qualities criteria. The topics were chosen on the basis of their importance to flying qualities and the potential significance to the Air Force VTOL Integrated Flight Control System (VIFCS) program. The treatment given to the selected topics was aimed at identifying those areas that require further study and research within the scope of the VIFCS program. -- page iii.
Government wide Index to Federal Research Development Reports
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 1050 |
Release | : 1966-02 |
Genre | : Government publications |
ISBN | : UOM:39015058500342 |
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Technical Abstract Bulletin
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 760 |
Release | : 2024 |
Genre | : Science |
ISBN | : CORNELL:31924057185575 |
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Annual NASA University Conference on Manual Control
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 476 |
Release | : 1968 |
Genre | : Human engineering |
ISBN | : STANFORD:36105024706447 |
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Scientific and Technical Aerospace Reports
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 892 |
Release | : 1988 |
Genre | : Aeronautics |
ISBN | : UIUC:30112075701570 |
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Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Aircraft Dynamics and Automatic Control
Author | : Duane T. McRuer,Dunstan Graham,Irving Ashkenas |
Publsiher | : Princeton University Press |
Total Pages | : 809 |
Release | : 2014-07-14 |
Genre | : Technology & Engineering |
ISBN | : 9781400855988 |
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Aeronautical engineers concerned with the analysis of aircraft dynamics and the synthesis of aircraft flight control systems will find an indispensable tool in this analytical treatment of the subject. Approaching these two fields with the conviction that an understanding of either one can illuminate the other, the authors have summarized selected, interconnected techniques that facilitate a high level of insight into the essence of complex systems problems. These techniques are suitable for establishing nominal system designs, for forecasting off-nominal problems, and for diagnosing the root causes of problems that almost inevitably occur in the design process. A complete and self-contained work, the text discusses the early history of aircraft dynamics and control, mathematical models of linear system elements, feedback system analysis, vehicle equations of motion, longitudinal and lateral dynamics, and elementary longitudinal and lateral feedback control. The discussion concludes with such topics as the system design process, inputs and system performance assessment, and multi-loop flight control systems. Originally published in 1974. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.