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- W2113649314 abstract "A pilot/vehicle analysis technique is offered which can provide predictions of handling qualities levels and pilot-induced oscillation rating levels in single-axis tracking tasks, with linear or nonlinear vehicle dynamics. The technique is applied to the three vehicle configurations evaluated hi the series of flight tests sponsored by the US Air Force, identified as HAVE LIMITS. The ability of the analysis technique to provide excellent quantitative predictions of the effects of actuator rate saturation on the handling qualities and pilot-induced oscillation susceptibility of the aircraft configurations is demonstrated. An interactive computer code is discussed which automates much of the pilot/vehicle analysis." @default.
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- W2113649314 date "1998-08-10" @default.
- W2113649314 modified "2023-09-25" @default.
- W2113649314 title "Analysis of aircraft handling qualities and pilot-induced oscillation tendencies with actuator saturation" @default.
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- W2113649314 doi "https://doi.org/10.2514/6.1998-4334" @default.
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