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- W1980417351 abstract "Analyses of design variations on a pitch axis stabilization and command augmentation system (SCAS) for a STOVL fighter aircraft are performed in a moving base simulation experiment. The primary goal of this study is to determine if turbulence-induced control activity could be reduced by modifying SCAS parameters while keeping the response-to-command characteristics of the baseline system that provide Level 1 flying qualities. Pilot ratings and control utilization statistics for the baseline system are in agreement with similar data gathered in a prior simulation test involving the same aircraft and control system." @default.
- W1980417351 created "2016-06-24" @default.
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- W1980417351 date "1992-08-10" @default.
- W1980417351 modified "2023-09-26" @default.
- W1980417351 title "Piloted simulation evaluation of pitch control designs for highly augmented STOVL aircraft" @default.
- W1980417351 doi "https://doi.org/10.2514/6.1992-4234" @default.
- W1980417351 hasPublicationYear "1992" @default.
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