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MODEL OF HELICOPTER PILOT'S CONTROLS ACTIVITY FOR SHIPBOARD OPERATIONS

机译:直升机操作的直升机驾驶员控制模型

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The only approved means available to evaluate the dynamic behavior of the helicopter/pilot combination in the complex turbulent environment of the moving flight deck of a ship is the execution of actual at-sea flight tests. The development of an off-line simulation tool of helicopter shipboard operations for engineering and design purpose is desirable. The objective of this study is to identify the pilot's controls strategy in order to provide prediction of the controls' positions when flying typical on-shore representative shipboard maneuvers, namely, hover, "fore/aft" and "estern" approaches, into four different wind environment conditions. Operational pilots A, B, C and D performed a pilot-in-the-loop flight test simulation in the helicopter engineering flight simulator facility of ONERA Salon de Provence Center, so called PycsHel, in order to provide data to calibrate and validate the prediction of the basic SYCOS {SYnthesis through Constrained Simulation) pilot model. The optimization process for training the pilot model from the piloted simulations data is divided into hover task and approach tasks, and uses the DIMSS PM (Dynamic Interface Modeling and Simulation System Product Metric) as metrics for estimating the pilot's controls activity. Pilots A and B models are considered valid for the validation data set in hover. However, basic SYCOS model is not able to keep the predictions stable over 50 sec of flight of the approach tasks. Therefore, extensions to the basic SYCOS model are studied by implementing an attitude or an acceleration feedback parallel line, in order to provide stability strategy to the pilot's controls activity prediction. The attitude feedback strategy is the only able to restore the SYCOS model stability for the approach data set. The extended SYCOS model with attitude feedback strategy is used for training and allows the validation of pilot's activity model to approach type "estem" (pilot B). None pilot's controls activity model is valid for the "fore/aft" approach task. The pilots C ("estern" approach) and D ("fore/aft" approach) extended SYCOS models are able to provide satisfactory predictions only for collective and pedals activities.
机译:在船舶移动的飞行甲板的复杂湍流环境中,唯一可用于评估直升机/飞行员组合的动态行为的批准方法是执行实际的海上飞行测试。期望开发用于工程和设计目的的直升机船载离线仿真工具。这项研究的目的是确定飞行员的控制策略,以便在将典型的陆上有代表性的舰艇操纵飞行时,即将鼠标悬停,“前后”和“偏航”进近到四个不同状态时,可以预测控制位置。风环境条件。运营飞行员A,B,C和D在ONERA Salon de Provence中心的直升机工程飞行模拟器设施(称为PycsHel)中进行了飞行员在环飞行测试模拟,以便提供数据来校准和验证预测基本SYCOS(通过约束模拟合成)先导模型的模型。用于从飞行员模拟数据中训练飞行员模型的优化过程分为悬停任务和进近任务,并使用DIMSS PM(动态接口建模和仿真系统产品度量)作为评估飞行员控制活动的度量。飞行员A和B模型被认为对悬停中的验证数据集有效。但是,基本的SYCOS模型无法在进近任务飞行50秒内使预测保持稳定。因此,通过实施姿态或加速度反馈平行线来研究对基本SYCOS模型的扩展,以便为飞行员的控制活动预测提供稳定性策略。姿态反馈策略是唯一能够为进近数据集恢复SYCOS模型稳定性的方法。具有姿态反馈策略的扩展SYCOS模型用于训练,并允许验证飞行员的活动模型以接近“估计”类型(飞行员B)。对于“前/后”进近任务,没有飞行员的控制活动模型有效。飞行员SYCOS模型的C(“ estern”方法)和D(“ fore / aft”方法)能够仅针对集体和踏板活动提供令人满意的预测。

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