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Investigation of Feel System and Control Sensitivity Characteristics InfluencingP-I-O of Unmaneuverable Aircraft

机译:影响无人驾驶飞机p-I-O的感觉系统和控制灵敏度特性研究

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This report results from a contract tasking TsAGI, Central AerohydrodynamicInstitute as follows: Investigate the pilot-induced-oscillation (PIO) tendency depending upon control sensitivity characteristics, damping of lever loading, lever mass and loading gradient at different flight regimes and dynamic performance using flight simulators.

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