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HANDLING QUALITIES STUDIES INTO THE INTERACTION BETWEEN ACTIVE SIDESTICK PARAMETERS AND HELICOPTER RESPONSE TYPES

机译:活动西迪克参量与直升机响应类型之间相互作用的处理质量研究

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Active inceptors offer great potential for improving the handling qualities of fly-by-wire rotorcraft. In a cooperative research, effort the DLR Institute of Flight Systems in Germany and the U.S. Army Aeroflightdynamics Directorate (AFDD) conducted several in-flight experiments to study the influence of the dynamic characteristics (natural frequency and damping) of the cyclic stick on the overall handling qualities of a rotorcraft. Experiments were performed looking at sidestick (DLR) and centerstick (AFDD) inceptors for Rate and Attitude Command response types. The results of two different experiments are presented in this paper. The first experiment evaluated the roll handling in forward flight and was only performed with a sidestick inceptor. The task used in this experiment was designed during exercises of the Empire Test Pilots' School (ETPS) on DLR's Flying Helicopter Simulator EC 135 ACT/FHS. ETPS also contributed to the optimization of the static sidestick characteristics that were used for the testing. The second, more comprehensive experiment, evaluating ADS-33 Hover and Slalom Mission Taks Elements, was performed both with a sidestick and a centerstick allowing a direct comparison of both types of inceptors. Regression analyses are performed on the collected pilot ratings to gain a systematic insight into the preferred stick characteristics for the different inceptor and response types. The test results consistently suggest that the preferred characteristics are best described by first order response model.
机译:主动感受器为改善电传旋翼飞机的操纵质量提供了巨大潜力。在一项合作研究中,德国DLR飞行系统研究所和美国陆军航空动力学局(AFDD)共同进行了几次飞行实验,以研究循环摇杆的动态特性(固有频率和阻尼)对整体飞行器的影响。处理旋翼飞机的质量。进行了实验,查看了“速率”和“姿态”命令响应类型的侧杆(DLR)和中杆(AFDD)感受器。本文介绍了两个不同的实验结果。第一个实验评估了向前飞行中的侧倾操纵,并且仅使用侧杆感受器进行了实验。本实验中使用的任务是在帝国测试飞行员学校(ETPS)在DLR的飞行直升机模拟器EC 135 ACT / FHS上进行的练习中设计的。 ETPS还有助于优化用于测试的静态侧杆特性。第二个更全面的实验是评估ADS-33悬停和激流回旋飞行任务元素,同时使用侧杆和中杆进行了实验,可以直接比较两种类型的感受器。对收集的飞行员评分进行回归分析,以系统地了解不同感受器和响应类型的首选摇杆特征。测试结果一致表明,首选特性最好由一阶响应模型来描述。

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