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- W814087712 abstract "A flight control system analysis and synthesis method is presented that is intended to be especially suitable for application to vehicles exhibiting complex dynamic characteristics. For such vehicles quantitative handling qualities specifications are not usually available. Howver, handling qualities objectives are specifically introduced in this method via the hypothesis of correlation between pilot ratings and the objective function of an optimal control model of the human pilot. Further, since augmentation and pilot operate in parallel, simultaneous determination of the augmentation and pilot model gains is required. Desirable augmented dynamics are obtained for a variety of complex systems and the method is experimentally verified in the case of simple pilot damper gain selection for optimum pitch tracking performance." @default.
- W814087712 created "2016-06-24" @default.
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- W814087712 date "1981-12-01" @default.
- W814087712 modified "2023-09-27" @default.
- W814087712 title "Multivariable closed loop control analysis and synthesis for complex flight systems" @default.
- W814087712 hasPublicationYear "1981" @default.
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