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Identification of Time-Varying Pilot Control Behavior in Multi-Axis Control Tasks

机译:多轴控制任务中随时间变化的先导控制行为的识别

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摘要

Recent developments in fly-by-wire control architectures for rotorcraft have introduced new interest in the identification of time-varying pilot control behavior in multi-axis control tasks. In this paper a maximum likelihood estimation method is used to estimate the parameters of a pilot model with time-dependent sigmoid functions to characterize time-varying human control behavior. An experiment was performed by 9 general aviation pilots who had to perform a simultaneous roll and pitch control task with time-varying aircraft dynamics. In 8 different conditions, the axis containing the time-varying dynamics and the growth factor of the dynamics were varied, allowing for an analysis of the performance of the estimation method when estimating time-dependent parameter functions. In addition, a detailed analysis of pilots adaptation to the time-varying aircraft dynamics in both the roll and pitch axes could be performed. Pilot control behavior in both axes was significantly affected by the time-varying aircraft dynamics in roll and pitch, and by the growth factor. The main effect was found in the axis that contained the time-varying dynamics. However, pilot control behavior also changed over time in the axis not containing the time-varying aircraft dynamics. This indicates that some cross coupling exists in the perception and control processes between the roll and pitch axes.
机译:旋翼飞机的线控飞行控制体系结构的最新发展引起了人们对多轴控制任务中随时间变化的飞行员控制行为的识别的新兴趣。在本文中,最大似然估计方法用于估计具有随时间变化的S形函数的飞行员模型的参数,以表征随时间变化的人类控制行为。 9名通用航空飞行员进行了一项实验,他们必须同时执行随时间变化的飞机动力学的侧倾和俯仰控制任务。在8种不同的条件下,包含时变动力学的轴和动力学的增长因子发生了变化,从而可以在估计与时间有关的参数函数时对估计方法的性能进行分析。此外,可以对飞行员在横滚轴和俯仰轴上适应时变飞机动力学的情况进行详细分析。飞机在侧倾和俯仰中的时变动力学以及增长因子都极大地影响了两个轴上的飞行员控制行为。在包含随时间变化的动力学的轴中发现了主要影响。但是,飞行员控制行为也会随着时间的推移在不包含随时间变化的飞机动力学的轴上发生变化。这表明在侧倾和俯仰轴之间的感知和控制过程中存在一些交叉耦合。

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