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- W577827102 abstract "Results of fixed-base simulator tests for augmented aircraft are presented in order to distinguish characteristics of a rate-command system from those of an attitude command system. Regulating aircraft states is requested by manual control of a subject pilot with a major concern for pitch attitude, under various combi nations of simulated turbulence intensities and bandwidths. Pilot dynamics in the closed loop is identified by applying the autoregressive model analysis using the measured data. The obtained loop transfer functions are compared in the light of stability margins and crossover frequency as well as of bandwidths and the equivalent time delay. It is concluded that the rate-command system is inferior in disturbance regulation tasks to the attitude-command system in that it shows less robustness beyond the frequencies defining the pilotaircraft bandwidth." @default.
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- W577827102 date "1996-01-01" @default.
- W577827102 modified "2023-09-26" @default.
- W577827102 title "Rate-Command System, Revisited." @default.
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- W577827102 doi "https://doi.org/10.2322/jjsass1969.44.242" @default.
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