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Design and Evaluation of a Constraint-Based Head-Up Display for Helicopter Obstacle Avoidance During Forward Flight

机译:基于约束的平视显示器在前向飞行中避免直升机障碍的设计和评估

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This paper aims to reveal the effect of different display design principles in the helicopter domain. Two different obstacle avoidance support displays are evaluated during low-altitude, forward helicopter flight: a baseline Head-Up Display (HUD) is complemented either by a conventional advisory display, or a constraint-based display inspired by Ecological Interface Design. The latter has only been sparsely applied in the helicopter domain. It is hypothesized that the advisory display reduces workload, increases situation awareness, and improves performance measures in nominal obstacle avoidance situations, while the constraint-based display increases the resilience of the pilot-vehicle system towards unexpected, off-nominal situations. Twelve helicopter pilots with varying flight experience participated in an experiment in the SIMONA Research Simulator at Delft University of Technology. Contrary to expectations, the experiment revealed no significant effects of the displays on any of the dependent measures. However, there was a trend of decreasing pilot workload and increasing situation awareness when employing any of the support displays, compared to the baseline HUD. Pilots preferred the advisory display in nominal and the constraint-based display in off-nominal situations, reproducing similar findings from research in the fixed-wing domain. The relatively short time-frame and monotony of the control-task, an already cue-rich baseline HUD condition, and similarity between the displays possibly prohibited revealing larger differences between conditions. Future research will analyze the obstacle avoidance trajectories of this experiment, possibly revealing changes in control strategy caused by the displays, even when the lumped performance measures are similar. A follow-up experiment will focus on a longer task time-frame, more variable situations, and a truly ecological display to investigate the effect of applying Ecological Interface Design and different automation systems in the helicopter domain.
机译:本文旨在揭示直升机领域中不同显示设计原理的影响。在低空向前的直升机飞行过程中,评估了两种不同的避障支持显示器:基线平视显示器(HUD)由常规的咨询显示器或受生态界面设计启发的基于约束的显示器来补充。后者仅被稀疏地应用于直升机领域。假设咨询显示器减少了工作量,提高了态势感知能力,并改善了在标称避障情况下的性能指标,而基于约束的显示器则提高了驾驶员车辆系统对意外,偏离标称情况的适应能力。十二名具有不同飞行经验的直升机飞行员参加了代尔夫特理工大学SIMONA研究模拟器的实验。与预期相反,该实验表明显示器对任何相关测量均无明显影响。但是,与基线HUD相比,采用任何支持显示器时都有减少飞行员工作量和增强态势意识的趋势。飞行员更喜欢名义上的咨询性展示和非名义上的基于约束的展示,从而再现了固定翼领域研究的类似发现。相对较短的时间范围和控制任务的单调性,已经很丰富的基线HUD条件以及显示器之间的相似性可能会禁止揭示条件之间的较大差异。未来的研究将分析该实验的避障轨迹,即使集总的性能指标相似,也可能揭示由显示器引起的控制策略的变化。后续实验将着重于更长的任务时间范围,更多的可变情况以及真正的生态展示,以研究在直升机领域应用生态界面设计和不同的自动化系统的效果。

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