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Investigation of limb-sidestick dynamic interaction with roll control

机译:侧倾控制与侧倾动力学相互作用的研究

摘要

A fixed-base simulation was performed to identify and quantify interactions between the pilot's hand/arm neuromuscular subsystem and such features of typical modern fighter aircraft roll rate command control system mechanization as: (1) force sensing side-stick type manipulator; (2) vehicle effective roll time constant; and (3) flight control system effective time delay. The simulation results provide insight to high frequency pilot induced oscillations (PIO) (roll ratchet), low frequency PIO, and roll-to-right control and handling problems previously observed in experimental and production fly-by-wire control systems. The simulation configurations encompass and/or duplicate several actual flight situations, reproduce control problems observed in flight, and validate the concept that the high frequency nuisance mode known as roll ratchet derives primarily from the pilot's neuromuscular subsystem. The simulations show that force-sensing side-stick manipulator force/displacement/command gradients, command prefilters, and flight control system time delays need to be carefully adjusted to minimize neuromuscular mode amplitude peaking (roll ratchet tendency) without restricting roll control bandwidth (with resulting sluggish or PIO prone control).
机译:进行了基于固定的仿真,以识别和量化飞行员的手/臂神经肌肉子系统与典型现代战斗机侧倾率指令控制系统机械化特征之间的相互作用:(1)力感测侧杆式操纵器; (2)车辆有效横滚时间常数; (3)飞行控制系统的有效时间延迟。仿真结果为洞悉高频飞行员感应振荡(PIO)(滚动棘齿),低频PIO以及从右到右的控制和处理问题提供了见识,这些问题以前是在实验和生产电传操纵系统中观察到的。仿真配置包含和/或复制了几种实际的飞行情况,重现了在飞行中观察到的控制问题,并验证了称为“滚动棘齿”的高频干扰模式主要源自飞行员的神经肌肉子系统的概念。仿真表明,需要仔细调整力感测侧操纵杆力/位移/指令梯度,指令预滤波器和飞行控制系统的时延,以在不限制侧倾控制带宽的情况下最小化神经肌肉模式振幅峰值(侧倾棘轮趋势)。导致速度缓慢或PIO控制容易)。

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