In-flight Simulation of the Lateral-directional Handling Qualities of Entry Vehicles
Author: Robert P. Harper (Jr.)
Publisher:
Published: 1961
Total Pages: 66
ISBN-13:
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Author: Robert P. Harper (Jr.)
Publisher:
Published: 1961
Total Pages: 66
ISBN-13:
DOWNLOAD EBOOKAuthor: Edwin A. Kidd
Publisher:
Published: 1964
Total Pages: 138
ISBN-13:
DOWNLOAD EBOOKLongitudinal and lateral directional flying qualities for the re-entry mission are reported. The program utilized primarily a high-fidelity fixed-base ground simulator with evaluations made by three pilots. One of the three pilots also made in-flight evaluations of longitudinal flying qualities in the same vehicle, a threeaxis variable stability airplane flown with a two-axis side controller and conventional rubber pedals. Control sensitivity evaluations were compared to center stick results of earlier work. The longitudinal flying qualities as evaluated both on the ground simulator and in flight are compared and related to earlier investigations. Pilot rating variability, both interpilot and intrapilot, are quantized and discussed for the ground and flight experiments. Performance measures are reported.
Author: Lawrence W. Taylor
Publisher:
Published: 1969
Total Pages: 122
ISBN-13:
DOWNLOAD EBOOKPilot ratings of lateral directional handling for wide range of aircraft characteristics - graphs.
Author: I. L. Ashkenas
Publisher:
Published: 1965
Total Pages: 40
ISBN-13:
DOWNLOAD EBOOKThis 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: Robert F. Stengel
Publisher: Princeton University Press
Published: 2022-11-01
Total Pages: 914
ISBN-13: 0691237042
DOWNLOAD EBOOKAn updated and expanded new edition of an authoritative book on flight dynamics and control system design for all types of current and future fixed-wing aircraft Since it was first published, Flight Dynamics has offered a new approach to the science and mathematics of aircraft flight, unifying principles of aeronautics with contemporary systems analysis. Now updated and expanded, this authoritative book by award-winning aeronautics engineer Robert Stengel presents traditional material in the context of modern computational tools and multivariable methods. Special attention is devoted to models and techniques for analysis, simulation, evaluation of flying qualities, and robust control system design. Using common notation and not assuming a strong background in aeronautics, Flight Dynamics will engage a wide variety of readers, including aircraft designers, flight test engineers, researchers, instructors, and students. It introduces principles, derivations, and equations of flight dynamics as well as methods of flight control design with frequent reference to MATLAB functions and examples. Topics include aerodynamics, propulsion, structures, flying qualities, flight control, and the atmospheric and gravitational environment. The second edition of Flight Dynamics features up-to-date examples; a new chapter on control law design for digital fly-by-wire systems; new material on propulsion, aerodynamics of control surfaces, and aeroelastic control; many more illustrations; and text boxes that introduce general mathematical concepts. Features a fluid, progressive presentation that aids informal and self-directed study Provides a clear, consistent notation that supports understanding, from elementary to complicated concepts Offers a comprehensive blend of aerodynamics, dynamics, and control Presents a unified introduction of control system design, from basics to complex methods Includes links to online MATLAB software written by the author that supports the material covered in the book
Author: Neville Moray
Publisher: Psychology Press
Published: 2005
Total Pages: 580
ISBN-13: 9780415322577
DOWNLOAD EBOOKBecause of the 'applied' nature of ergonomics there are many outstanding pieces of work that have never been published in the archival literature. These volumes collect some of those papers that have attained classical status.
Author:
Publisher:
Published: 1964
Total Pages: 1600
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. Wright Air Development Division
Publisher:
Published: 1961
Total Pages: 1246
ISBN-13:
DOWNLOAD EBOOKAuthor: Frederick D. Newell
Publisher:
Published: 1969
Total Pages: 84
ISBN-13:
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