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Analytical display design for flight tasks conducted under instrument meteorological conditionsA relatively straightforward, nearly algorithmic procedure for deriving model-based pilot-centered display requirements is presented. A pilot model based on modern control theory serves as the backbone of the design methodology, which is specifically directed toward the synthesis of head-down, electronic cockpit display formats. Some novel applications of the optimal pilot model are discussed, including the generation of vehicle-handling-qualities levels via numerical pilot-opinion ratings. An analytical design example is offered which aids in the definition of a format for the electronic display to be used in a UH-1H helicopter in a landing-approach task involving longitudinal and lateral degrees of freedom. It is proposed that the design procedure offers a systematic means for generating candidate display formats and flight-director laws for simulator evaluation.
Document ID
19770053066
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Hess, R. A.
(NASA Ames Research Center Aircraft Guidance and Navigation Branch, Moffett Field, Calif., United States)
Date Acquired
August 9, 2013
Publication Date
June 1, 1977
Subject Category
Aircraft Instrumentation
Accession Number
77A35918
Distribution Limits
Public
Copyright
Other

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