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Improvements in Hover Display Dynamics for A Combat HelicopterThis paper describes a piloted simulation conducted on the NASA Ames Vertical Motion Simulator. The objective of the experiment was to investigate the handling qualities benefits attainable using new display law design methods for hover displays. The new display laws provide improved methods to specify the behavior of the display symbol that predicts the vehicle's ground velocity in the horizontal plane; it is the primary symbol that the pilot uses to control aircraft horizontal position. The display law design was applied to the Apache helmet-mounted display format, using the Apache vehicle dynamics to tailor the dynamics of the velocity predictor symbol. The representations of the Apache vehicle used in the display design process and in the simulation were derived from flight data. During the simulation, the new symbol dynamics were seen to improve the pilots' ability to maneuver about hover in poor visual cuing environments. The improvements were manifested in pilot handling qualities ratings and in measured task performance. The paper details the display design techniques, the experiment design and conduct, and the results.
Document ID
19940008837
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Jeffery A Schroeder
(Ames Research Center Mountain View, United States)
Michelle M Eshow
(Army Aviation Systems Command Edwards AFB, CA, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1993
Publication Information
Publication: Piloting Vertical Flight Aircraft: A Conference on Flying Qualities and Human Factors
Publisher: National Aeronautics and Space Administration
Subject Category
Aircraft Stability and Control
Report/Patent Number
NASA/CP-3220
Meeting Information
Meeting: Piloting Vertical Flight Aircraft: A Conference on Flying Qualities and Human Factors
Location: San Francisco, CA
Country: US
Start Date: January 20, 1993
End Date: January 22, 1993
Sponsors: American Helicopter Society, National Aeronautics and Space Administration
Accession Number
94N13310
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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