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Pilot Stick Input Estimates from Attitude Commands as Indicator of Systemic Changes

机译:来自姿态命令的飞行员操纵杆输入估计作为系统变化的指示

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Control-theoretic modeling of the human operator dynamic behavior in manual control tasks has a long and rich history. In the last two decades, there has been a renewed interest in modeling the human operator. There has also been significant work on techniques used to identify the pilot model of a given structure. The purpose of this research is to attempt to go beyond identification of a pilot model based on collected experimental data and to develop a predictor of pilot behavior. Two sets of experimental data were analyzed: 1) the effects of an adaptive controller on pilot compensation during control surface failures in cruise and 2) heads-up-display concepts during takeoff and landing. A general linear in-parameter model structure is used to represent a pilot Three different estimation methods are explored - a gradient descent estimator, a least squares estimator with exponential forgetting, and a least squares estimator with bounded gain forgetting. This paper discusses the accuracy of each of the three methods to estimate pilot longitudinal and lateral stick input from the flight director's commanded pitch and bank attitudes and the differences in piloting techniques during takeoff, cruise, and landing phases of flight.
机译:人工控制任务中操作员动态行为的控制理论建模历史悠久且丰富。在过去的二十年中,人们对操作员建模有了新的兴趣。在用于识别给定结构的试验模型的技术方面也进行了大量工作。这项研究的目的是尝试超越基于收集到的实验数据识别飞行员模型,并开发出飞行员行为的预测器。分析了两组实验数据:1)在巡航控制面故障期间自适应控制器对飞行员补偿的影响,以及2)在起飞和着陆期间的抬头显示概念。使用一般的线性参数内模型结构表示飞行员,探索了三种不同的估计方法-梯度下降估计器,具有指数遗忘的最小二乘估计器和具有边界增益遗忘的最小二乘估计器。本文讨论了三种方法的准确性,这些方法可根据飞行指挥员的俯仰和倾斜姿态估计飞行员的纵向和横向操纵杆输入,以及在起飞,巡航和着陆阶段飞行员技术的差异。

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