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Pilot-optimal augmentation synthesisAn augmentation synthesis method usable in the absence of quantitative handling qualities specifications, and yet explicitly including design objectives based on pilot-rating concepts, is presented. The algorithm involves the unique approach of simultaneously solving for the stability augmentation system (SAS) gains, pilot equalization and pilot rating prediction via optimal control techniques. Simultaneous solution is required in this case since the pilot model (gains, etc.) depends upon the augmented plant dynamics, and the augmentation is obviously not a priori known. Another special feature is the use of the pilot's objective function (from which the pilot model evolves) to design the SAS.
Document ID
19790007432
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Schmidt, D. K.
(Purdue Univ. West Lafayette, IN, United States)
Date Acquired
August 10, 2013
Publication Date
November 1, 1978
Publication Information
Publication: NASA. Ames Res. Center The 14th Ann. Conf. on Manual Control
Subject Category
Man/System Technology And Life Support
Accession Number
79N15603
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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