A Study Of Conventional Airplane Handling Qualities Requirements
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Author | : I. L. Ashkenas |
Publisher | : |
Total Pages | : 86 |
Release | : 1965 |
Genre | : Airplanes |
ISBN | : |
The report uses as a point of departure the concept that control of bank angle is the primary piloting task in maintaining or changing heading. Regulation of the bank angle to maintain heading is a close-loop tracking task in which the pilot applies aileron control as a function of observed bank angle error. For large heading changes, the steady-state bank angle consistent with available or desired load factor is attained in an open-loop fashion; it is then regulated in a closed-loop fashion throughout the remainder of the turn. For the transient entry and exit from the turn, the pilot is not concerned with bank angle per se, but rather with attaining a mentally commanded bank angle with tolerable accuracy in a reasonable time, and with an easily learned and comfortable program of aileron movements.
Author | : I. L. Ashkenas |
Publisher | : |
Total Pages | : 40 |
Release | : 1965 |
Genre | : Airplanes |
ISBN | : |
This report is a codification in two parts of conventional aircraft handling qualities criteria. The results of this effort are to serve as an intermediate design guide in the areas of lateral-directional oscillatory and roll control. The roll handling qualities portion of this report uses as a point of departure the concept that control of bank angle is the primary piloting task in maintaining or changing heading. In the lateral oscillatory portion of this effort, in defining requirements for satisfactory Dutch roll characteristics, a fundamental consideration is the fact that the motions characterizing this mode are ordinarily not the pilot's chief objective. That is, he is not deliberately inducing Dutch roll motions in the sense that he induces rolling and longitudinal short-period motions. A worthwhile approach to establishment of Dutch roll damping requirements is to first establish the basic level, and then to study the varied influences of the disturbance parameters. This approach provides the basis for the material contained in this report.
Author | : Irving Louis Ashkenas |
Publisher | : |
Total Pages | : |
Release | : 1965 |
Genre | : Airplanes |
ISBN | : |
Author | : National Research Council |
Publisher | : National Academies Press |
Total Pages | : 221 |
Release | : 1997-03-28 |
Genre | : Transportation |
ISBN | : 0309056888 |
Adverse aircraft-pilot coupling (APC) events include a broad set of undesirable and sometimes hazardous phenomena that originate in anomalous interactions between pilots and aircraft. As civil and military aircraft technologies advance, interactions between pilots and aircraft are becoming more complex. Recent accidents and other incidents have been attributed to adverse APC in military aircraft. In addition, APC has been implicated in some civilian incidents. This book evaluates the current state of knowledge about adverse APC and processes that may be used to eliminate it from military and commercial aircraft. It was written for technical, government, and administrative decisionmakers and their technical and administrative support staffs; key technical managers in the aircraft manufacturing and operational industries; stability and control engineers; aircraft flight control system designers; research specialists in flight control, flying qualities, human factors; and technically knowledgeable lay readers.
Author | : |
Publisher | : |
Total Pages | : 776 |
Release | : |
Genre | : Science |
ISBN | : |
Author | : Thomas R. Yechout |
Publisher | : AIAA |
Total Pages | : 666 |
Release | : 2003 |
Genre | : Aerodynamics |
ISBN | : 9781600860782 |
Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.
Author | : |
Publisher | : |
Total Pages | : 490 |
Release | : 1990 |
Genre | : Aeronautics |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 236 |
Release | : 1979 |
Genre | : |
ISBN | : |
Author | : Edwin W. Aiken |
Publisher | : |
Total Pages | : 18 |
Release | : 1985 |
Genre | : |
ISBN | : |
Author | : Robert C. Nelson |
Publisher | : |
Total Pages | : 464 |
Release | : 1998 |
Genre | : History |
ISBN | : |
This edition of this this flight stability and controls guide features an unintimidating math level, full coverage of terminology, and expanded discussions of classical to modern control theory and autopilot designs. Extensive examples, problems, and historical notes, make this concise book a vital addition to the engineer's library.