NASA NTRS ยท 19790007432
Pilot-optimal augmentation synthesis
Abstract
An 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.
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Schmidt, D. K.. 1978-11-01. Pilot-optimal augmentation synthesis. https://ntrs.nasa.gov/citations/19790007432
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